BR112014024197B1 - ES Fastener Cartridge Assembly for a Surgical Instrument and End Actuator Assembly for a Surgical Instrument - Google Patents

Abstract

FABRIC THICKNESS COMPENSATOR COMPRISING FIBERS TO PRODUCE A RESILIENT LOAD. The present invention relates to a non-woven compensator (20020) for an end actuator of a surgical instrument which may comprise a plurality of spring fibers (20082) dispersed by the non-woven compensator. The non-woven compensator may be positioned on the end actuator, for example adjacent to a platform surface of a fastener cartridge which is positioned on the end actuator. When a fastener of the fastener cartridge is moved from a home position to a fired position, the fastener can be configured to engage the non-woven compensator. The fastener may compress a portion of the non-woven compensator in a staple gripping area defined by the fired staple. The spring fibers in the non-woven compensator may comprise a resilient material and may be deformed when the fastener compresses a portion of the non-woven compensator. Additionally, the non-woven compensator may comprise non-spring fibers, a hemostatic material and/or a homogeneous absorbable polymeric matrix.

Description

CROSS REFERENCE TO RELATED ORDERS

[0001] This provisional patent application is a continuation-in-part patent application under 35 U.S.C. §120 of the U.S. Patent Application No. 13/097,891 entitled "Tissue Thickness Compensator For A Surgical Stapler Comprising An Adjustable Anvil, which was filed April 29, 2011, which is a continuation-in-part application under 35 U.S.C. §120 of U.S. Patent Application No. Serial No. 12/894,377, entitled "Selectively Orientable Implantable Fastener Cartridge", which was filed September 30, 2010, the disclosure of which is incorporated herein by reference.

BACKGROUND

[0002] The present invention relates to surgical instruments and, in various embodiments, to surgical cutting and stapling instruments and staple cartridges thereof that are designed to cut and staple tissue.

SUMMARY

[0003] The following is a non-exhaustive list of embodiments of the present invention that are or can be claimed.,

[0004] 1. Fastener cartridge assembly for a surgical instrument, the fastener cartridge assembly comprising:

[0005] a support portion comprising a fastener cavity;

[0006] a non-woven compensator positioned with respect to the support portion, the non-woven compensator comprising a plurality of spring fibers dispersed therein; and

[0007] a fastener movable between a home position and a fired position, wherein the fastener is at least partially positioned in the fastener cavity when the fastener is in its home position, and wherein the fastener is configured to compress the non-woven compensator when the fastener is moved between its home position and its fired position.

[0008] 2. Fastener cartridge assembly, according to embodiment 1, wherein at least one spring fiber comprises a resilient material, and wherein the spring fiber is deformed when the fastener compresses the non-woven compensator.

[0009] 3. Fastener cartridge set, according to modality 1 or modality 2, in which the fastener comprises:

[00010] a base;

[00011] a first leg extending from the base; and

[00012] a second leg extending from the base, the first leg and second leg being configured to bend towards the base when the fastener is moved to its triggered position;

[00013] wherein the fastener captures a portion of the non-woven compensator between the base and at least one of the first leg and second leg when the fastener is moved to its triggered position.

[00014] 4. Fastener cartridge set, according to modality 3, which additionally comprises:

[00015] a slit that extends through at least a portion of the support portion; and

[00016] a trigger member configured to translate within the slot, wherein the trigger member is configured to engage the base of the clamp when the trigger member translates so that the clamp is ejected from the clamp cavity.

[00017] 5. A fastener cartridge assembly, according to any of the foregoing embodiments, wherein the non-woven compensator is releasably secured to a platform of the support portion by an adhesive.

[00018] 6. Fastener cartridge assembly, according to any of the foregoing embodiments, wherein the spring fibers are randomly dispersed and randomly oriented in the non-woven compensator.

[00019] 7. A fastener cartridge assembly according to any of the foregoing embodiments, wherein the non-woven compensator comprises a plurality of non-spring fibers.

[00020] 8. A fastener cartridge assembly according to any of the foregoing embodiments, wherein the spring fibers comprise a bioabsorbable synthetic material.

[00021] 9. Fastener cartridge assembly according to any of the foregoing embodiments, wherein the spring fibers comprise a material selected from a group comprising poly(dioxanone) (PDO), polylactides (APL), polyglycolides (PGA) , polycaprolactones (PCL), polycarbonates, and their copolymers.

[00022] 10. A fastener cartridge assembly according to any of the foregoing embodiments, wherein the spring fibers are heat formed to maintain a substantially coiled shape.

[00023] 11. A fastener cartridge assembly according to any of the foregoing embodiments, wherein the non-woven compensator is needle-punched and comprises a hemostatic material.

[00024] 12. Fastener cartridge for a surgical instrument, the fastener cartridge comprising:

[00025] a body comprising a first body portion and a second body portion, the first body portion comprising fastener cavities, the second body portion comprising a compressible portion, the compressible portion comprising a plurality of spring fibers dispersed therein, the spring fibers being at least partially resilient; and

[00026] fasteners, each fastener being aligned with a fastener cavity of the first body portion.

[00027] 13. A fastener cartridge according to embodiment 12, wherein at least one fastener is movable between an initial position and a triggered position, and wherein the fastener is configured to compress a portion of the compressible portion when the fastener is moved to the fired position.

[00028] 14. A fastener cartridge according to embodiment 13, wherein the compressible portion comprises an absorbable homogeneous polymeric matrix.

[00029] 15. Fastener cartridge according to any one of modalities 12 to 14 which additionally comprises:

[00030] a slit that extends through at least a portion of the first body portion; and

[00031] A trigger member configured to translate within the slot, wherein the trigger member is configured to engage at least one fastener when the trigger member translates such that the trigger member ejects the at least one fastener from the first body part.

[00032] 16. End actuator assembly for a surgical instrument, comprising:

[00033] an anvil;

[00034] a fastener cartridge comprising:

[00035] a cartridge body comprising a fastener cavity; and

[00036] a fastener that is at least partially positioned in a fastener cavity when the fastener is in an initial position; and

[00037] a non-woven compensator positioned intermediate the fastener cartridge and the anvil, the non-woven compensator comprising a plurality of spring fibers dispersed therein, and the spring fibers being at least partially resilient.

[00038] 17. End actuator assembly according to embodiment 16, wherein the non-woven compensator is releasably attached to at least one of the fastener cartridge and the anvil, and wherein the non-woven compensator comprises a non-woven material.

[00039] 18. End actuator assembly according to embodiment 17, wherein the fastener is movable from its initial position to a triggered position, and wherein the fastener is configured to compress a portion of the non-woven compensator when the fastener is moved to its fired position.

[00040] 19. End actuator assembly according to embodiment 18, wherein the anvil comprises a forming pocket in a tissue contacting surface, and wherein the forming pocket deforms the fastener when the fastener is moved from your starting position to your firing position.

[00041] 20. End actuator assembly according to embodiment 18 or embodiment 19, wherein the non-woven compensator is configured to disengage from the end actuator assembly when the fastener compresses said portion of the non-woven compensator.

BRIEF DESCRIPTION OF THE DRAWINGS

[00042] The features and advantages of this invention, and the manner of achieving them, will become more apparent and the invention itself will be better understood by referring to the following description of embodiments of the invention, obtained in conjunction with the accompanying drawings , being that:

[00043] Figure 1 is a cross-sectional view of a surgical instrument modality;

[00044] Figure 1A is a perspective view of an embodiment of an implantable staple cartridge;

[00045] Figures 1B to 1E illustrate portions of an end actuator that grips and staples tissue with an implantable staple cartridge;

[00046] Figure 2 is a partial cross-sectional side view of another end actuator coupled to a portion of a surgical instrument with the end actuator supporting a surgical staple cartridge and with its anvil in an open position;

[00047] Figure 3 is another side view in partial cross-section of the end actuator of Figure 2 in a closed position;

[00048] Figure 4 is another partial cross-sectional side view of the end actuator of Figures 2 and 3 as the knife bar begins to advance through the end actuator;

[00049] Figure 5 is another side view in partial cross-section of the end actuator of Figures 2 to 4 with the knife bar partially advanced therethrough;

[00050] Figures 6A to 6D show a diagram of the deformation of a surgical staple positioned in the body of a retractable staple cartridge according to at least one embodiment;

[00051] Figure 7A is a diagram illustrating a staple positioned in the body of a collapsible staple cartridge;

[00052] Figure 7B is a diagram illustrating the deformable staple cartridge body 7A of Figure being deformed by an anvil;

[00053] Figure 7C is a diagram illustrating the deformable staple cartridge body 7A of Figure being further deformed by the anvil;

[00054] Figure 7D is a diagram illustrating the staple of Figure 7A in a fully formed configuration and the collapsible staple cartridge of Figure 7A in a fully deformed condition;

[00055] Figure 8 is a top view of a staple cartridge according to at least one embodiment comprising staples inserted into the body of the retractable staple cartridge;

[00056] Figure 9 is an elevation view of the staple cartridge of Figure 8;

[00057] Figure 10 is an exploded perspective view of an alternative embodiment of a compressible staple cartridge comprising staples therein and a system for driving the staples against an anvil;

[00058] Figure 10A is a partial cutaway view of an alternative embodiment of the staple cartridge of Figure 10;

[00059] Figure 11 is a cross-sectional view of the staple cartridge of Figure 10.

[00060] Figure 12 is an elevation view of a slider configured to traverse the staple cartridge of Figure 10 and move the staples toward the anvil;

[00061] Figure 13 is a diagram of a clamp driver that can be lifted towards the anvil by the slider of Figure 12;

[00062] Figure 14 is a perspective view of a staple cartridge comprising a rigid support portion and a compressible tissue thickness compensator for use with a surgical stapling instrument in accordance with at least one embodiment of the invention;

[00063] Figure 15 is a partially exploded view of the staple cartridge of Figure 14;

[00064] Figure 16 is a fully exploded view of the staple cartridge of Figure 14;

[00065] Figure 17 is another exploded view of the staple cartridge of Figure 14 without a warp covering the fabric thickness compensator;

[00066] Figure 18 is a perspective view of a cartridge body, or support portion, of the staple cartridge of Figure 14;

[00067] Figure 19 is a top perspective view of a movable slider within the staple cartridge of Figure 14 for positioning staple cartridge staples;

[00068] Figure 20 is a bottom perspective view of the slider of Figure 19;

[00069] Figure 21 is an elevation view of the slider of Figure 19;

[00070] Figure 22 is a top perspective view of a driver configured to support one or more staples and to be lifted upwards by the slider of Figure 19 to eject the staples from the staple cartridge;

[00071] Figure 23 is a bottom perspective view of the actuator of Figure 22;

[00072] Figure 24 is a housing configured to at least partially surround a compressible tissue thickness compensator of a staple cartridge;

[00073] Figure 25 is a partial cutaway view of a staple cartridge comprising a rigid support portion and a compressible tissue thickness compensator illustrated with staples being moved from a non-fired position to a fired position during a first sequence;

[00074] Figure 26 is an elevation view of the staple cartridge of Figure 25;

[00075] Figure 27 is a detailed elevational view of the staple cartridge of Figure 25;

[00076] Figure 28 is an end cross-sectional view of the staple cartridge of Figure 25;

[00077] Figure 29 is a bottom view of the staple cartridge of Figure 25;

[00078] Figure 30 is a detailed bottom view of the staple cartridge of Figure 25;

[00079] Figure 31 is a longitudinal cross-sectional view of an anvil in a closed position and a staple cartridge comprising a rigid support portion and a compressible tissue thickness compensator illustrated with staples being moved from an unfired to a non-fired position. a position triggered during a first sequence;

[00080] Figure 32 is another cross-sectional view of the anvil and staple cartridge of Figure 31 illustrating the anvil in an open position after the firing sequence has been completed;

[00081] Figure 33 is a partial detail view of the staple cartridge of Figure 31 illustrating the staples in an unfired position;

[00082] Figure 34 is an elevational cross-sectional view of a staple cartridge comprising a rigid support portion and a compressible fabric thickness compensator illustrating the staples in an unfired position;

[00083] Figure 35 is a detail view of the staple cartridge of Figure 34;

[00084] Figure 36 is an elevational view of an anvil in an open position and a staple cartridge comprising a rigid support portion and a compressible tissue thickness compensator illustrating the staples in an unfired position;

[00085] Figure 37 is an elevational view of an anvil in a closed position and a staple cartridge comprising a rigid support portion and a compressible tissue thickness compensator illustrating the staples in an unfired position and tissue captured between the anvil and fabric thickness compensator;

[00086] Figure 38 is a detail view of the anvil and staple cartridge of Figure 37;

[00087] Figure 39 is an elevational view of an anvil in a closed position and a staple cartridge comprising a rigid support portion and a compressible tissue thickness compensator illustrating the staples in an unfired position illustrating thicker tissue positioned between the anvil and the staple cartridge;

[00088] Figure 40 is a detail view of the anvil and staple cartridge of Figure 39;

[00089] Figure 41 is an elevational view of the anvil and staple cartridge of Figure 39 illustrating tissue having different thicknesses positioned between the anvil and staple cartridge;

[00090] Figure 42 is a detail view of the anvil and staple cartridge of Figure 39, as illustrated in Figure 41;

[00091] Figure 43 is a diagram illustrating a fabric thickness compensator that is compensating for different thicknesses of fabric captured by different staples;

[00092] Figure 44 is a diagram illustrating a tissue thickness compensator applying compressive pressure to one or more vessels that have been transected by a row of staples;

[00093] Figure 45 is a diagram illustrating a circumstance in which one or more clamps were improperly formed.

[00094] Figure 46 is a diagram illustrating a fabric thickness compensator that could compensate for improperly formed staples;

[00095] Figure 47 is a diagram illustrating a fabric thickness compensator positioned in a region of fabric cut by multiple rows of staples;

[00096] Figure 48 is a diagram illustrating tissue captured by a staple;

[00097] Figure 49 is a diagram illustrating fabric and a fabric thickness compensator captured by a staple;

[00098] Figure 50 is a diagram illustrating tissue captured by a staple;

[00099] Figure 51 is a diagram illustrating thick fabric and a fabric thickness compensator captured by a staple;

[000100] Figure 52 is a diagram illustrating thin tissue and a tissue thickness compensator captured by a staple;

[000101] Figure 53 is a diagram illustrating fabric having an intermediate thickness and a fabric thickness compensator captured by a staple;

[000102] Figure 54 is a diagram illustrating fabric having another intermediate thickness and a fabric thickness compensator captured by a staple;

[000103] Figure 55 is a diagram illustrating thick fabric and a fabric thickness compensator captured by a staple;

[000104] Figure 56 is a partial cross-sectional view of an end actuator of a surgical stapling instrument illustrating a firing bar and a staple firing slider in a retracted and unfired position;

[000105] Figure 57 is another partial cross-sectional view of the end actuator of Figure 56 illustrating the trigger bar and staple trigger slider in a partially advanced position;

[000106] Figure 58 is a cross-sectional view of the end actuator of Figure 56 illustrating the firing bar in a fully advanced or fired position;

[000107] Figure 59 is a cross-sectional view of the end actuator of Figure 56 illustrating the firing bar in a retracted position after being fired and the staple firing slider left in its fully fired position;

[000108] Figure 60 is a detail view of the firing bar in the retracted position of Figure 59;

[000109] Figure 61 is a perspective view of a tissue thickness compensator in an end actuator of a surgical instrument according to at least one embodiment;

[000110] Figure 62 is a non-woven detail view of the fabric thickness compensator of Figure 61;

[000111] Figure 63 is an elevation view depicting the tissue thickness compensator of Figure 61 deployed against tissue and released from the end actuator;

[000112] Figure 64 is a detail view of a non-woven material of a fabric thickness compensator according to at least one embodiment;

[000113] Figure 65 is a schematic view depicting randomly oriented clusters of crimped fibers according to at least one embodiment;

[000114] Figure 66 is a schematic view depicting an array of randomly oriented crimped fibers according to at least one embodiment;

[000115] Figure 67 is a schematic view depicting an arrangement of crimped fibers according to at least one embodiment;

[000116] Figure 68 is a schematic view depicting an arrangement of crimped fibers according to at least one embodiment;

[000117] Figure 69 is a schematic view depicting an arrangement of crimped fibers according to at least one embodiment;

[000118] Figure 70 is a cross-sectional plan view of spirally wound fibers in a fabric thickness compensator according to at least one embodiment;

[000119] Figure 70A is a cross-sectional plan view of the spiral wound fibers of Figure 70;

[000120] Figure 70B is a cross-sectional detail view of the fabric thickness compensator of Figure 70;

[000121] Figure 71 is a perspective view of a tissue thickness compensator in an end actuator of a surgical instrument according to at least one embodiment;

[000122] Figure 72 is a diagram depicting the deformation of the fabric thickness compensator of Figure 71;

[000123] Figure 73 is a schematic view of woven suture for a tissue thickness compensator depicting woven suture in a loaded configuration in accordance with at least one embodiment;

[000124] Figure 74 is a schematic view of the woven suture of Figure 73 depicting the woven suture in a released configuration;

[000125] Figure 75 is a plan view of a tissue thickness compensator having the woven suture of Figure 73 into an end actuator of a surgical instrument;

[000126] Figure 76 is a perspective view of a tissue thickness compensator in an end actuator of a surgical instrument according to at least one embodiment;

[000127] Figure 77 is a partial plan view of the fabric thickness compensator of Figure 76;

[000128] Figure 78 is an exploded view of the end actuator fastener cartridge assembly and fabric thickness compensator of Figure 61;

[000129] Figure 79 is a partial cross-sectional view of the cartridge fastener assembly of Figure 78 depicting unfired, partially fired and fired fasteners;

[000130] Figure 80 is an elevational view of the cartridge fastener assembly of Figure 78 depicting an actuator that fires fasteners from staple cavities of the cartridge fastener assembly into the fabric thickness compensator;

[000131] Figure 81 is a detail view of the fastener cartridge assembly of Figure 80;

[000132] Figure 82 is an elevation view of the fabric thickness compensator of Figure 61 and the fabric captured by the fired fasteners;

[000133] Figure 83 is an elevation view of the fabric thickness compensator of Figure 61 and the fabric captured by the fired fasteners;

[000134] Figure 84 is a perspective view of a tissue thickness compensator in an end actuator of a surgical instrument according to at least one embodiment;

[000135] Figure 85 is a diagram depicting deformation of a deformable tube of the fabric thickness compensator of Figure 84;

[000136] Figure 86 is a detail view of the deformable tube of the fabric thickness compensator of Figure 84;

[000137] Figure 87 is a diagram depicting deformation of a deformable tube of a fabric thickness compensator according to at least one embodiment;

[000138] Figure 88 is an elevational view of a fabric thickness compensator comprising a tubular member implanted against fabric according to at least one embodiment;

[000139] Figure 89 is an elevation view of a fabric thickness compensator comprising tubular elements implanted against fabric according to at least one embodiment;

[000140] Figure 90 is a partial perspective view of a deformable tube comprising a tubular reticle according to at least one embodiment;

[000141] Figure 91 is an elevation view of a tubular wire of the deformable tube of Figure 90.

[000142] Figure 92 is an elevation view of the collapsible tube of Figure 90;

[000143] Figure 93 is an elevational view of multiple tubular strands for the collapsible tube of Figure 90 according to various embodiments;

[000144] Figure 94 is an elevation view of the tubular lattice of Figure 90 implanted against tissue;

[000145] Figure 95 is a partial perspective view of a deformable tube according to at least one embodiment;

[000146] Figure 96 is a partial perspective view of a deformable tube according to at least one embodiment;

[000147] Figure 97 is a partial perspective view of a deformable tube according to at least one embodiment;

[000148] Figure 98 is an elevation view of the collapsible tube of Figure 97;

[000149] Figure 99 is a partial perspective view of a deformable tube according to at least one embodiment;

[000150] Figure 100 is a partial perspective view of a deformable tube according to at least one embodiment;

[000151] Figure 101 is a partial perspective view of a deformable tube according to at least one embodiment;

[000152] Figure 102 is a perspective view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000153] Figure 103 is an elevation view of a collapsible tube of the fabric thickness compensator of Figure 102;

[000154] Figure 104 is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 102 representing the end actuator in a non-tight configuration;

[000155] Figure 105 is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 102 depicting the end actuator in a tight and fired configuration;

[000156] Figure 106 is an elevational cross-sectional view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000157] Figure 107 is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 106 depicting the end actuator in a tight and fired configuration;

[000158] Figure 108 is an elevational cross-sectional view of a tissue thickness compensator in the end actuator of a surgical instrument according to at least one embodiment;

[000159] Figure 109 is a cross-sectional elevation view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000160] Figure 110 is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 109 representing the end actuator in a tight and fired configuration;

[000161] Figure 111 is a perspective view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000162] Figure 112 is an elevational cross-sectional view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000163] Figure 113 is an elevational cross-sectional view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000164] Figure 114 is an elevational cross-sectional view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000165] Figure 115 is an elevational cross-sectional view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000166] Figure 116 is a partial plan view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000167] Figure 117 is a partial plan view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000168] Figure 118 is a partial elevation cross-sectional view of the fabric thickness compensator and end actuator of Figure 116 representing the end actuator in a non-tight configuration;

[000169] Figure 119 is a partial elevation cross-sectional view of the fabric thickness compensator and end actuator of Figure 116 representing the end actuator in a tight configuration;

[000170] Figure 120 is a perspective view of a tissue thickness compensator in an end actuator of a surgical instrument according to at least one embodiment;

[000171] Figure 121 is an elevation view of the fabric thickness compensator and end actuator of Figure 120;

[000172] Figure 122 is a perspective view of the fabric thickness compensator and end actuator of Figure 120 depicting the end actuator anvil moving towards a tight configuration;

[000173] Figure 123 is an elevation view of the fabric thickness compensator and end actuator of Figure 120 representing the end actuator in a tight configuration;

[000174] Figure 124 is an elevational cross-sectional view of tubular elements of the fabric thickness compensator of Figure 120 in an undeformed configuration;

[000175] Figure 125 is an elevational cross-sectional view of tubular elements of the fabric thickness compensator of Figure 120 in a deformed configuration;

[000176] Figure 126 is a perspective view of a tissue thickness compensator in an end actuator of a surgical instrument according to at least one embodiment;

[000177] Figure 127 is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 126 representing the end actuator in a tight configuration;

[000178] Figure 128 is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 126 depicting the end actuator in a partially unclamped and fired configuration;

[000179] Figure 129 is a perspective view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000180] Figure 130 is an elevational cross-sectional view of a tissue thickness compensator attached to an anvil of an end actuator of a surgical instrument according to at least one embodiment;

[000181] Figure 131 is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 130 representing the end actuator in a tight configuration;

[000182] Figure 132 is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 130 depicting the end actuator in the fired and partially untightened configuration;

[000183] Figure 133 is a detail view of the fabric thickness compensator and end actuator of Figure 132;

[000184] Figure 134 is an elevational cross-sectional view of a tissue thickness compensator clamped on an end actuator of a surgical instrument representing the positioning of staples by means of a slide-firing bracket. clip according to at least one embodiment;

[000185] Figure 135 is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 134 representing the end actuator in a tight configuration;

[000186] Figure 136 is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 134 representing the end actuator in the fired configuration;

[000187] Figure 137 is a perspective view of a tissue thickness compensator in an end actuator of a surgical instrument according to at least one embodiment;

[000188] Figure 138 is a perspective view of a collapsible tube of the fabric thickness compensator of Figure 137;

[000189] Figure 139 is a perspective view of the tubular element of Figure 138 separated between a first and a second ends;

[000190] Figure 140 is a perspective view of the fabric thickness compensator of Figure 137 showing a cutting element that separates the fabric thickness compensator and the clips that engage the fabric thickness compensator;

[000191] Figure 141 is a perspective view of a frame configured to produce the fabric thickness compensator of Figure 137 according to at least one embodiment;

[000192] Figure 142 is an elevational cross-sectional view of the frame of Figure 141 depicting the fabric thickness compensator of Figure 137 curing in the frame;

[000193] Figure 143 is an elevational cross-sectional view of the fabric thickness compensator removed from the frame of Figure 142 and prepared for trimming by at least one cutting instrument;

[000194] Figure 144 is an elevational cross-sectional view of the fabric thickness compensator of Figure 143 after at least one cutting instrument has trimmed the fabric thickness compensator;

[000195] Figure 145 is an elevational cross-sectional view of the fabric thickness compensator formed in the frame of Figure 142 representing separable tubes having various geometries in cross section;

[000196] Figure 146 is a perspective view of a tissue thickness compensator in an end actuator of a surgical instrument according to at least one embodiment;

[000197] Figure 147 is a detail view of the fabric thickness compensator of Figure 146 according to at least one embodiment;

[000198] Figure 148 is a partial perspective view of a fabric thickness compensator according to at least one embodiment;

[000199] Figure 149 is a partial perspective view of a fabric thickness compensator according to at least one embodiment;

[000200] Figure 150A is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 146 depicting the end actuator in a non-tight configuration;

[000201] Figure 150B is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 146 representing the end actuator in a tight configuration;

[000202] Figure 150C is an elevational cross-sectional view of the fabric thickness compensator and end actuator of Figure 146 depicting the end actuator in a tight and fired configuration;

[000203] Figure 150D is an elevational cross-sectional view of the fabric thickness compensator of Figure 146 captured on fired staples;

[000204] Figure 150E is an elevational cross-sectional view of the fabric thickness compensator of Figure 146 captured in fired staples representing further expansion of the fabric thickness compensator;

[000205] Figure 151 is a perspective cross-sectional view of a tissue thickness compensator in an end actuator of a surgical instrument according to at least one embodiment;

[000206] Figure 152 is a partial elevation view of the fabric thickness compensator of Figure 151 captured in a fired staple;

[000207] Figure 153 is an elevation view of a collapsible tube of the fabric thickness compensator of Figure 151;

[000208] Figure 154 is an elevation view of a deformable tube according to at least one embodiment;

[000209] Figure 155 is a perspective cross-sectional view of the fabric thickness compensator of Figure 151;

[000210] Figure 156 is a perspective cross-sectional view of a tissue thickness compensator in an end actuator of a surgical instrument according to at least one embodiment;

[000211] Figure 157 is a perspective view of a fabric thickness compensator according to at least one embodiment;

[000212] Figure 158 is a partial elevation cross-sectional view of the fabric thickness compensator of Figure 157 depicting a fastener engaged with the fabric and fabric thickness compensator;

[000213] Figure 159 is a perspective cross-sectional view of a fabric thickness compensator according to at least one embodiment;

[000214] Figure 160 is an elevation view of a fabric thickness compensator according to at least one embodiment;

[000215] Figure 161 is an elevational view of a fabric thickness compensator according to at least one embodiment;

[000216] Figure 162 is an elevation view of a tissue thickness compensator positioned on a circular end actuator of a surgical instrument according to at least one embodiment;

[000217] Figure 163 is an elevational view of a fabric thickness compensator according to at least one embodiment;

[000218] Figure 164 is an elevation view of a fabric thickness compensator according to at least one embodiment;

[000219] Figure 165 is an elevational view of a fabric thickness compensator according to at least one embodiment;

[000220] Figure 166 is an elevation view of a fabric thickness compensator according to at least one embodiment;

[000221] Figure 167 is an elevational view of a fabric thickness compensator according to at least one embodiment;

[000222] Figure 168 is a partial perspective view of a fabric thickness compensator according to at least one embodiment;

[000223] Figure 169 is a partial perspective view of a tissue thickness compensator positioned on an end actuator of a surgical instrument according to at least one embodiment;

[000224] Figure 170 is a partial perspective view of a fabric thickness compensator with a fastener positioned in the openings thereof according to at least one embodiment;

[000225] Figure 171 is a partial perspective view of the fabric thickness compensator of Figure 169 depicting the fabric thickness compensator in an undeformed configuration;

[000226] Figure 172 is a partial perspective view of the fabric thickness compensator of Figure 169 depicting the fabric thickness compensator in a partially deformed configuration;

[000227] Figure 173 is a partial perspective view of the fabric thickness compensator of Figure 169 depicting the fabric thickness compensator in a deformed configuration;

[000228] Figure 174 is a perspective view of a fabric thickness compensator according to at least one embodiment;

[000229] Figure 175 is a perspective view of an end actuator of a stapling instrument comprising an anvil and a staple cartridge according to at least one embodiment;

[000230] Figure 176 is a cross-sectional view of the end actuator of Figure 175 illustrating staples positioned within the staple cartridge in an unfired state and a tissue thickness compensator comprising a sealed vessel in an unfired state. unperforated, wherein the vessel is shown with portions thereof removed for purposes of illustration;

[000231] Figure 177 is a cross-sectional view of the end actuator of Figure 175 illustrating the clamps of Figure 176 in an at least partially fired state and the vessel in an at least partially pierced state;

[000232] Figure 178 is a perspective view of an end actuator of a stapling instrument comprising an anvil and a staple cartridge according to at least one embodiment;

[000233] Figure 179 is a cross-sectional view of the end actuator of Figure 178 illustrating staples positioned within the staple cartridge in an unfired state and sealed vessels positioned within a tissue thickness compensator of the staple cartridge. staples in an unperforated state, wherein the vessels are shown with portions thereof removed for purposes of illustration;

[000234] Figure 180 is a cross-sectional view of the end actuator of Figure 178 illustrating the staples of Figure 179 in an at least partially fired state and the vessels in the staple cartridge in an at least partially pierced state;

[000235] Figure 181 is a perspective view of an end actuator of a stapling instrument comprising an anvil and a sealed vessel secured to the anvil in accordance with at least one alternative embodiment, wherein the vessel is shown with portions of the anvil. even removed for illustration purposes;

[000236] Figure 182 is a cross-sectional view of the end actuator of Figure 181 illustrating staples at least partially fired from a staple cartridge and the vessels attached to the anvil in an at least partially punctured state;

[000237] Figure 183 is a cross-sectional view of the vessel attached to the anvil of Figure 181 illustrated in an expanded state;

[000238] Figure 184 is a detail view of the vessel attached to the anvil of Figure 183 illustrated in an expanded state;

[000239] Figure 185 illustrates a vessel extending in a direction transverse to a row of staples;

[000240] Figure 186 illustrates a plurality of vessels extending in directions that are transverse to a row of staples;

[000241] Figure 187 is a cross-sectional view of a staple cartridge according to various embodiments;

[000242] Figure 188 is a partial cross-sectional view of Figure 187 in an implanted condition;

[000243] Figure 189A is a partial perspective view of a fabric thickness compensator before expansion;

[000244] Figure 189B is a partial perspective view of a fabric thickness compensator of Figure 189 during expansion;

[000245] Figure 190 is a partial perspective view of a fabric thickness compensator comprising a fluid swellable composition in accordance with various embodiments;

[000246] Figure 191 is a cross-sectional view of fabric positioned adjacent a fabric thickness compensator in accordance with various embodiments;

[000247] Figure 192 is a partial cross-sectional view of Figure 191 after the staple cartridge has been fired;

[000248] Figure 193 is a diagram illustrating the tissue thickness compensator of Figure 191 implanted adjacent to tissue;

[000249] Figure 194 is a partial perspective view of a fabric thickness compensator in accordance with various embodiments;

[000250] Figure 195 is a perspective view of a jaw configured to receive the fabric thickness compensator of Figure 194;

[000251] Figure 196 is a partial cross-sectional view of a staple cartridge illustrating staples being installed from the staple cartridge;

[000252] Figure 197 is a perspective view of an upper fabric thickness compensator and a lower fabric thickness compensator positioned within an actuator of a disposable loading unit;

[000253] Figure 198A is a cross-sectional view of the lower fabric thickness compensator of Figure 197 being manufactured in a mold according to various embodiments;

[000254] Figure 198B is a cross-sectional view of a three-layer fabric thickness compensator being manufactured in a mold according to various embodiments;

[000255] Figure 199 is a cross-sectional view of an anvil comprising a fabric thickness compensator comprising reinforcing material in accordance with various embodiments;

[000256] Figure 200 is a cross-sectional view of a fabric positioned intermediate the upper fabric thickness compensator and the lower fabric thickness compensator in accordance with various embodiments;

[000257] Figure 201 is a cross-sectional view of Figure 200 illustrating staples being installed from the staple cartridge;

[000258] Figure 202 is a cross-sectional view of Figure 200 after the staple cartridge has been fired;

[000259] Figure 203A illustrates a needle configured to supply fluid to a tissue thickness compensator attached to a staple cartridge in accordance with various embodiments;

[000260] Figure 203B is a cross-sectional view of a staple cartridge comprising a fabric thickness compensator configured to receive the needle of Figure 203A;

[000261] Figure 204 illustrates a method of manufacturing a fabric thickness compensator according to various embodiments;

[000262] Fig. 205 is a diagram and method of forming an expanding thickness compensator according to various embodiments;

[000263] Figure 206 illustrates a micelle comprising a hydrogel precursor; and

[000264] Figure 207 is a diagram of a surgical instrument comprising a tissue thickness compensator and fluids that can be supplied to the tissue thickness compensator in accordance with various embodiments.

[000265] Figure 208 is a partial perspective view of a tissue thickness compensator attached to an anvil of an end actuator of a surgical instrument according to at least one embodiment.

[000266] Figure 209 is a perspective view of a deformable tube of the fabric thickness compensator of Figure 208.

[000267] Figure 210 is a perspective view of the tubular element of Figure 209 representing the tubular element separated into two halves and in fluid contact with the hydrophilic substance within each half.

[000268] Figure 211 is a perspective view of a half of the detached tubular element of Figure 210 representing the expansion of the detached tubular element.

[000269] Matching reference characters indicate matching parts in all the various views. The exemplifications described herein illustrate certain embodiments of the invention, in one form, and such exemplifications are not to be considered as limiting the scope of the invention in any way.

DETAILED DESCRIPTION

[000270] The applicant of the present application also owns the rights to the US patent applications identified below which are each incorporated herein by reference in their respective entireties: US Patent Application Serial No. 12/894,311 entitled SURGICAL INSTRUMENTS WITH RECONFIGURABLE SHAFT SEGMENTS (attorney's document number END6734USNP/100058); US Patent Application Serial No. 12/894,340 entitled SURGICAL STAPLE CARTRIDGES SUPPORTING NON-LINEARLY ARRANGED STAPLES AND SURGICAL STAPLING INSTRUMENTS WITH COMMON STAPLE-FORMING POCKETS (Attorney's Document No. END6735USNP/100059); US Patent Application Serial No. 12/894,327 entitled JAW CLOSURE ARRANGEMENTS FOR SURGICAL INSTRUMENTS (Attorney's Document No. END6736USNP/100060); US Patent Application Serial No. 12/894,351 entitled SURGICAL CUTTING AND FASTENING INSTRUMENTS WITH SEPARATE AND DISTINCT FASTENER DEPLOYMENT AND TISSUE CUTTING SYSTEMS (Attorney's Document No. END6839USNP/100524); US Patent Application Serial No. 12/894,338 entitled IMPLANTABLE FASTENER CARTRIDGE HAVING A NON-UNIFORM ARRANGEMENT (Attorney's Document No. END6840USNP/100525); US Patent Application Serial No. 12/894,369 entitled IMPLANTABLE FASTENER CARTRIDGE COMPRISING A SUPPORT RETAINER (Attorney's Document No. END6841USNP/100526); US Patent Application Serial No. 12/894,312 entitled IMPLANTABLE FASTENER CARTRIDGE COMPRISING MULTIPLE LAYERS (Attorney's Document No. END6842USNP/100527); US Patent Application Serial No. 12/894,377 entitled SELECTIVELY ORIENTABLE IMPLANTABLE FASTENER CARTRIDGE (Attorney's Document No. END6843USNP/100528); US Patent Application Serial No. 12/894,339 entitled SURGICAL STAPLING INSTRUMENT WITH COMPACT ARTICULATION CONTROL ARRANGEMENT (Attorney's Document No. END6847USNP/100532); US Patent Application Serial No. 12/894,360 entitled SURGICAL STAPLING INSTRUMENT WITH A VARIABLE STAPLE FORMING SYSTEM (Attorney's Document No. END6848USNP/100533); US Patent Application Serial No. 12/894,322 entitled SURGICAL STAPLING INSTRUMENT WITH INTERCHANGEABLE STAPLE CARTRIDGE ARRANGEMENTS (Attorney's Document No. END6849USNP/100534); US Patent Application Serial No. 12/894,350 entitled SURGICAL STAPLE CARTRIDGES WITH DETACHABLE SUPPORT STRUCTURES AND SURGICAL STAPLING INSTRUMENTS WITH SYSTEMS FOR PREVENTING ACTUATION MOTIONS WHEN A CARTRIDGE IS NOT PRESENT (attorney's document no. END6855USNP/100540); US Patent Application Serial No. 12/894,383 entitled IMPLANTABLE FASTENER CARTRIDGE COMPRISING BIOABSORBABLE LAYERS (Attorney's Document No. END6856USNP/100541); US Patent Application Serial No. 12/894,389 entitled COMPRESSIBLE FASTENER CARTRIDGE (Attorney's Document No. END6857USNP/100542); US Patent Application Serial No. 12/894,345 entitled FASTENERS SUPPORTED BY A FASTENER CARTRIDGE SUPPORT (Attorney's Document No. END6858USNP/100543); US Patent Application Serial No. 12/894,306 entitled COLLAPSIBLE FASTENER CARTRIDGE (Attorney's Document No. END6859USNP/100544); US Patent Application Serial No. 12/894,318 entitled FASTENER SYSTEM COMPRISING A PLURALITY OF CONNECTED RETENTION MATRIX ELEMENTS (Attorney's Document No. END6860USNP/100546); US Patent Application Serial No. 12/894,330 entitled FASTENER SYSTEM COMPRISING A RETENTION MATRIX AND AN ALIGNMENT MATRIX (Attorney's Document No. END6861USNP/100547); US Patent Application Serial No. 12/894,361 entitled FASTENER SYSTEM COMPRISING A RETENTION MATRIX (Attorney's Document No. END6862USNP/100548); US Patent Application Serial No. 12/894,367 entitled FASTENING INSTRUMENT FOR DEPLOYING A FASTENER SYSTEM COMPRISING A RETENTION MATRIX (Attorney's Document No. END6863USNP/100549); US Patent Application Serial No. 12/894,388 entitled FASTENER SYSTEM COMPRISING A RETENTION MATRIX AND A COVER (Attorney's Document No. END6864USNP/100550); US Patent Application Serial No. 12/894,376 entitled FASTENER SYSTEM COMPRISING A PLURALITY OF FASTENER CARTRIDGES (Attorney's Document No. END6865USNP/100551); US Patent Application Serial No. 13/097,865 entitled SURGICAL STAPLER ANVIL COMPRISING A PLURALITY OF FORMING POCKETS (Attorney's Document No. END6735USCIP1/100059CIP1); US Patent Application Serial No. 13/097,936 entitled TISSUE THICKNESS COMPENSATOR FOR A SURGICAL STAPLER (Attorney's Document No. END6736USCIP1/100060CIP1); US Patent Application Serial No. 13/097,954 entitled STAPLE CARTRIDGE COMPRISING A VARIABLE THICKNESS COMPRESSIBLE PORTION (Attorney's Document No. END6840USCIP1/100525CIP1); US Patent Application Serial No. 13/097,856 entitled STAPLE CARTRIDGE COMPRISING STAPLES POSITIONED WITHIN A COMPRESSIBLE PORTION THEREOF (Attorney's Document No. END6841USCIP1/100526CIP1); US Patent Application Serial No. 13/097,928 entitled TISSUE THICKNESS COMPENSATOR COMPRISING DETACHABLE PORTIONS (Attorney's Document No. END6842USCIP1/100527CIP1); US Patent Application Serial No. 13/097,891 entitled TISSUE THICKNESS COMPENSATOR FOR A SURGICAL STAPLER COMPRISING AN ADJUSTABLE ANVIL (Attorney Document No. END6843USCIP1/100528CIP1); US Patent Application Serial No. 13/097,948 entitled STAPLE CARTRIDGE COMPRISING AN ADJUSTABLE DISTAL PORTION (Attorney's Document No. END6847USCIP1/100532CIP1); US Patent Application Serial No. 13/097,907 entitled COMPRESSIBLE STAPLE CARTRIDGE ASSEMBLY (Attorney's Document No. END6848USCIP1/100533CIP1); US Patent Application Serial No. 13/097,861 entitled TISSUE THICKNESS COMPENSATOR COMPRISING PORTIONS HAVING DIFFERENT PROPERTIES (Attorney's Document No. END6849USCIP1/100534CIP1); US Patent Application Serial No. 13/097,869 entitled STAPLE CARTRIDGE LOADING ASSEMBLY (Attorney's Document No. END6855USCIP1/100540CIP1); US Patent Application Serial No. 13/097,917 entitled COMPRESSIBLE STAPLE CARTRIDGE COMPRISING ALIGNMENT MEMBERS (Attorney's Document No. END6856USCIP1/100541CIP1); US Patent Application Serial No. 13/097,873 entitled STAPLE CARTRIDGE COMPRISING A RELEASABLE PORTION (Attorney's Document No. END6857USCIP1/100542CIP1); US Patent Application Serial No. 13/097,938 entitled STAPLE CARTRIDGE COMPRISING COMPRESSIBLE DISTORTION RESISTANT COMPONENTS (Attorney's Document No. END6858USCIP1/100543CIP1); US Patent Application Serial No. 13/097,924 entitled STAPLE CARTRIDGE COMPRISING A TISSUE THICKNESS COMPENSATOR (Attorney's Document No. END6859USCIP1/100544CIP1); US Patent Application Serial No. 13/242,029 entitled SURGICAL STAPLER WITH FLOATING ANVIL (Attorney's Document No. END6841USCIP2/100526CIP2); US Patent Application Serial No. 13/242,066 entitled CURVED END EFFECTOR FOR A STAPLING INSTRUMENT (Attorney's Document No. END6841USCIP3/100526CIP3); US Patent Application Serial No. 13/242,086 entitled STAPLE CARTRIDGE INCLUDING COLLAPSIBLE DECK (Attorney's Document No. END7020USNP/110374); US Patent Application Serial No. 13/241,912 entitled STAPLE CARTRIDGE INCLUDING COLLAPSIBLE DECK ARRANGEMENT (Attorney's Document No. END7019USNP/110375); US Patent Application Serial No. 13/241,922 entitled SURGICAL STAPLER WITH STATIONARY STAPLE DRIVERS (Attorney's Document No. END7013USNP/110377); US Patent Application Serial No. 13/241,637 entitled SURGICAL INSTRUMENT WITH TRIGGER ASSEMBLY FOR GENERATING MULTIPLE ACTUATION MOTIONS (Attorney Document No. END6888USNP3/110378); and US Patent Application Serial No. 13/241,629 entitled SURGICAL INSTRUMENT WITH SELECTIVELY ARTICULATABLE END EFFECTOR (Attorney's Document No. END6888USNP2/110379). The Applicant of the present application also owns the US patent applications identified below which were filed on the same date as the present application and which are each incorporated herein by reference in their entirety, respectively: US Application Serial No. , entitled TIS SUE THICKNESS COMPENSATOR COMPRISING A PLURALITY OF CAPSULES, (attorney's document number END6864USCIP1/100550CIP1); US Application Serial No., entitled TIS SUE THICKNESS COMPENSATOR COMPRISING A PLURALITY OF LAYERS, (Attorney's Document No. END6864USCIP2/100550CIP2); US Application Serial No., entitled EX PANDABLE TISSUE THICKNESS COMPENSATOR, (Attorney's Document No. END6843USCIP2/100528CIP2). US Application Serial No., entitled TIS SUE THICKNESS COMPENSATOR COMPRISING A RESERVOIR, (Attorney Document No. END6843USCIP3/100528CIP3); US Application Serial No., entitled RETAINER ASSEMBLY INCLUDING A TISSUE THICKNESS COMPENSATOR, (Attorney Document No. END6843USCIP4/100528CIP4); US Application Serial No., entitled TIS SUE THICKNESS COMPENSATOR COMPRISING AT LEAST ONE MEDICAMENT, (Attorney's Document No. END6843USCIP5/100528CIP5); US Application Serial No., entitled TIS SUE THICKNESS COMPENSATOR COMPRISING CONTROLLED RELEASE AND EXPANSION, (Attorney Document No. END6843USCIP6/100528CIP6); US Application Serial No., entitled TIS SUE THICKNESS COMPENSATOR COMPRISING STRUCTURE TO PRODUCE A RESILIENT LOAD, (attorney's document no. END6843USCIP8/100528CIP8); US Application Serial No., entitled TIS SUE THICKNESS COMPENSATOR COMPRISING RESILIENT MEMBERS, (Attorney Document No. END6843USCIP9/100528CIP9); US Application Serial No., entitled ME THODS FOR FORMING TISSUE THICKNESS COMPENSATOR AR-RANGEMENTS FOR SURGICAL STAPLERS, (Attorney's Document No. END6843USCIP10/100528CP10); US Application Serial No., entitled TIS SUE THICKNESS COMPENSATORS, (Attorney's Document No. END6843USCIP11/100528CP11); US Application Serial No., entitled LAYE RED TISSUE THICKNESS COMPENSATOR, (Attorney's Document No. END6843USCIP12/100528CP12); US Application Serial No., entitled TISSUE THICKNESS COMPENSATORS FOR CIRCULAR SURGICAL STAPLERS, (Attorney's Document No. END6843USCIP13/100528CP13); US application serial no., entitled TIS SUE THICKNESS COMPENSATOR COMPRISING CAPSULES DEFINING A LOW PRESSURE ENVIRONMENT, (attorney's document no. END7100USNP/110601); US application serial no., entitled TIS SUE THICKNESS COMPENSATOR COMPRISED OF A PLURALITY OF MATERIALS, (attorney's document no. END7101USNP/110602); US Application Serial No., entitled MO VABLE MEMBER FOR USE WITH A TISSUE THICKNESS COMPENSATOR, (Attorney's Document No. END7107USNP/110603); US application serial no., entitled TIS SUE THICKNESS COMPENSATOR COMPRISING A PLURALITY OF MEDICAMENTS, (attorney's document no. END7102USNP/110604); US Application Serial No., entitled TIS SUE THICKNESS COMPENSATOR AND METHOD FOR MAKING THE SAME, (Attorney's Document No. END7103USNP/110605); US Application Serial No., entitled TIS SUE THICKNESS COMPENSATOR COMPRISING CHANNELS, (Attorney's Document No. END7104USNP/110606); US Application Serial No., entitled TISSUE THICKNESS COMPENSATOR COMPRISING TISSUE INGROWTH FEATURES, (Attorney Document No. END7105USNP/110607); and US Application Serial No., entitled DEVI CES AND METHODS FOR ATTACHING TISSUE THICKNESS COMPENSATING MATERIALS TO SURGICAL STAPLING INSTRUMENTS, (attorney's document no. END7106USNP/110608).

[000271] Certain exemplary embodiments will now be described to provide a general understanding of the principles of structure, function, fabrication and use of the devices and methods of the present invention presented. One or more examples of these embodiments are illustrated in the accompanying drawings. Those skilled in the art will understand that the devices and methods specifically described herein and illustrated in the accompanying drawings are exemplary, non-limiting embodiments. Features illustrated or described in conjunction with one exemplary embodiment may be combined with features of other embodiments. Such modifications and variations are included within the scope of the present invention.

[000272] Any of the methods disclosed or claimed herein for manufacturing, forming or otherwise producing an article or product, may be used to manufacture, form or otherwise produce all or part of the article or product in question, and provided that such method is used to manufacture, form or otherwise produce part of the article or product in question, the remainder of the article or product may be produced in any way, including by means of the use of any of the other methods disclosed and claimed herein for manufacturing, forming or otherwise producing the article or product, and the various parts so produced may be combined in any way. Similarly, any article or product disclosed or claimed herein may exist alone or in combination with, or as an integral part of, any other article or product disclosed in that form with which it is compatible. In this way, the particular features, structures or characteristics illustrated or described in conjunction with an article, product or method may be combined, in whole or in part, with the features, structures or characteristics of one or more other compatible articles, products or methods. , without limitation. Such modifications and variations are included within the scope of the present invention.

[000273] Where it is disclosed herein, with reference to a particular figure or otherwise, that a certain embodiment of the invention or a certain article, product or method may comprise certain structures, features or features, it will be understood by the reader that this means that those structures, characteristics or features may be incorporated into the article, product or method in question in any compatible combination. In particular, such disclosure of numerous ideal structures, features or features shall be understood to also reveal all such structures, features or features in combination, except in the case of structures, features or features which are revealed as alternatives to one another. Where such structures, features or resources are revealed as alternatives to one another, it must be understood that this reveals these alternatives as being replacements for another.

[000274] The terms "proximal" and "distal" are used in the present invention with reference to a clinician's manipulation of the handle portion of the surgical instrument. The term "proximal" refers to the portion closest to the clinician, and the term "distal" refers to the portion located furthest from the clinician. It will also be understood that, for the sake of convenience and clarity, spatial terms such as "vertical", "horizontal", "upward" and "downward" may be used in the present invention in connection with the drawings. However, surgical instruments can be used in many orientations and positions, and these terms are not intended to be limiting and/or absolute.

[000275] Various exemplary devices and methods are provided for performing laparoscopic and minimally invasive surgical procedures. However, the reader will readily understand that the various methods and devices disclosed in the present invention can be used in numerous surgical procedures and applications, including in connection with open surgical procedures. As the present detailed description proceeds, the reader will further appreciate that the various instruments disclosed in the present invention can be inserted into a body in any manner, such as through a natural orifice, through an incision or perforation hole formed in tissue. , etc. The working portions or end actuator portions of instruments may be inserted directly into the patient's body or may be inserted through an access device which has a working channel through which the end actuator and elongated stem of an instrument surgery can be advanced.

[000276] Turning to drawings where numbers indicate similar components across the various views, Figure 1 shows a surgical instrument 10 that is capable of performing several unique benefits. Surgical stapling instrument 10 is designed to handle and/or actuate end actuators 12 of various shapes and sizes that are operatively attached to the instrument. In Figures 1 to 1E, for example, the end actuator 12 includes an elongate channel 14 which forms a lower jaw 13 of the end actuator 12. The elongate channel 14 is configured to support an "implantable" clamp cartridge 30 and also support movably an anvil 20 which acts as an upper grip 15 of the end actuator 12.

[000277] The elongated channel 14 can be manufactured from, for example, stainless steel, titanium, etc. series 300 & 400, 17-4 & 17-7 and be formed with spaced side walls 16. The anvil 20 can be manufactured, for example, from stainless steel series 300 & 400, 17-4, 17-7, titanium , etc., & and have a lower staple-forming surface generally identified as 22 which has a plurality of staple-forming pockets 23 formed therein. See Figures 1B to 1E. In addition, the anvil 20 has a bifurcated ramp assembly 24 that protrudes proximally from the anvil. An anvil pin 26 projects from each side of the ramp assembly 24 to be received in a corresponding slot or opening 18 in the side walls 16 of the elongate channel 14 to facilitate its movable or pivoting attachment thereto.

[000278] Various forms of implantable staple cartridges may be employed with the surgical instruments disclosed herein. Specific staple cartridge configurations and constructions will be discussed in more detail below. However, in Figure 1A, an implantable staple cartridge 30 is shown. The staple cartridge 30 has a body portion 31 consisting of a compressible hemostatic material, for example oxidized regenerated cellulose ("ORC") or an oxidized regenerated cellulose ("ORC"). bioabsorbable foam on which rows of unformed metal staples are supported 32. To prevent the staple from being affected and the hemostatic material being activated during the insertion and placement process, the entire cartridge can be coated or wrapped in a biodegradable film 38, as a polydioxanone film sold under the trademark PDS®, or with a film of polyglycerol sebacate (PGS) or other biodegradable films formed from PGA (polyglycolic acid, marketed under the trademark Vicryl), PCL (polycaprolactone), PLA or PLLA (polylactic acid), PHA (polyhydroxyalkanoate), PGCL (polyglecapron 25, sold under the tradename Monocryl) or a compound of PGA, PCL, PLA, PDS that will be used waterproof until broken. The body 31 of the staple cartridge 30 is sized to be removably supported in the elongated groove 14 as shown, so that each staple 32 therein aligns with the corresponding staple forming pockets 23 on the anvil when the anvil 20 is actuated to form contact with the staple cartridge 30.

[000279] In use, after the end actuator 12 is positioned adjacent to the target tissue, the end actuator 12 is manipulated to capture or clamp the target tissue between an upper face 36 of the staple cartridge 30 and the surface of Staple forming 22 of anvil 20. Staples 32 are formed by moving anvil 20 in a path that is substantially parallel to elongated groove 14 to bring out staple forming surface 22 and, more particularly, staple forming pockets 23 in substantially simultaneous contact with the top face 36 of the staple cartridge 30. As the anvil 20 continues to move in the staple cartridge 30, the legs 34 of the staples 32 contact a corresponding staple forming the pocket 23 in the anvil 20 which serves to fold the legs of the clamps 34 over each other to form the clamps 32 in a "B-shape". Further movement of the anvil 20 towards the elongated groove 14 will further compress and form the clamps 32 into a height formed by the final "FF".

[000280] The staple formation process described above is generally represented in figures 1B to 1E. For example, Figure 1B illustrates the end actuator 12 with the target tissue "T" between the anvil 20 and the top face 36 of the implantable staple cartridge 30. Figure 1C illustrates the initial clamping position of the anvil 20 in which the anvil 20 was closed over the target tissue "T" to secure the target tissue "T" between the anvil 20 and the top face 36 of the staple cartridge 30. Figure 1D illustrates the initial formation of the staple in which the anvil 20 has begun to compress the staple cartridge 30 so that the legs 34 of the staples 32 are beginning to be formed by the staple forming pockets 23 in the anvil 20. Figure 1E illustrates the staple 32 in its final state formed through the fabric. "T" target with anvil 20 removed for clarity. After the clips 32 are formed and secured to the target tissue "T", the surgeon moves the anvil 20 to the open position to allow the cartridge body 31 and clips 32 to remain attached to the target tissue while the end actuator 12 is taken from the patient. End actuator 12 forms all clamps simultaneously as the two jaws 13 and 15 are pressed. The remaining "crumpled" body materials 31 act as a hemostatic material (the ORC) and staple line reinforcement (PGA, PDS or any of the other film compositions mentioned above 38). Furthermore, as the staples 32 never need to leave the cartridge body 31 during formation, the probability of defective formation of the staples 32 during this process is minimized. For use in the present invention, the term "implantable" means that, in addition to the clips, the cartridge body materials that support the clips will also remain in the patient and may eventually be absorbed into the patient's body. Such implantable staple cartridges are distinguishable from previous cartridge arrangements which remain positioned within the end actuator in its entirety after they have been fired.

[000281] In various implementations, the end actuator 12 is configured to be coupled to an elongate stem assembly 40 that projects from a cable assembly 100. The end actuator 12 (when closed) and the elongate stem assembly 40 may have similar cross-sectional shapes and be sized to pass operatively through a trocar tube or working channel in another form of access instrument. For use in the present invention, the term "operationally pass" means that the end actuator and at least a portion of the elongate stem assembly can be introduced through or passed through the opening of the channel or tube and can be manipulated therein. as needed to complete the surgical stapling procedure. When in a closed position, jaws 13 and 15 of end actuator 12 can provide the end actuator with a superficially circular cross-sectional shape that facilitates its passage through a circular passage/opening. However, the end actuators of the present invention, as well as the elongated stem assemblies, could conceivably be provided with other shapes in cross section that could otherwise pass through passages and access openings which are non-circular shapes in cross section. In this way, an overall size of a closed-end actuator cross-section will be related to the size of the passage or opening through which it is intended to pass. Thus, an end actuator for example can be called a "5mm end actuator", meaning it can operatively pass through an opening that is at least approximately 5 mm in diameter.

[000282] The elongated stem assembly 40 may have an outside diameter that is substantially equal to the outside diameter of the end actuator 12 when in a closed position. For example, a 5mm end actuator can be coupled to an elongated rod assembly 40 whose cross-sectional diameter is 5mm. However, as the present detailed description progresses, it will become apparent that the present invention can be effectively used in connection with different sizes of end actuators. For example, a 10mm end actuator can be attached to an elongated rod that has a cross diameter of 5mm. Conversely, for applications where a 10mm or greater opening or access passage is provided, the elongated rod assembly 40 may have a 10mm (or greater) transverse diameter, but may also be capable of actuating an actuator. 5mm or 10mm end. Accordingly, the outer stem 40 may have an outer diameter that is the same as or different from the outer diameter of a closed-end actuator 12 attached thereto.

[000283] As shown, the elongated rod assembly 40 extends distally from the handle assembly 100 in a generally straight line to define a longitudinal axis A-A. For example, the elongate rod assembly 40 may have a length of approximately 229 to 406 mm (9 to 16 inches). However, the elongate stem assembly 40 may be supplied in other lengths or may contain unions or be otherwise configured to facilitate articulation of the end actuator 12 with respect to other portions of the stem or cable assembly as will be discussed in more detail. below. The elongate rod assembly 40 includes a back member 50 that extends from the handle assembly 100 to the end actuator 12. The proximal end of the elongate channel 14 of the end actuator 12 has a pair of detent swivel pins 17. protruding therefrom, which are sized to be received within corresponding swivel pin openings or cradles 52 which are provided at a distal end of the back element 50 to allow the end actuator 12 to be removably coupled to the assembly of elongated shank 40. Back element 50 may be manufactured from, for example, 6061 or 7075 aluminum, stainless steel, titanium, and the like.

[000284] The cable assembly 100 comprises a pistol grip housing which can be manufactured in two or more pieces for assembly purposes. For example, the cable assembly 100, as shown, comprises a right-hand housing element 102 and a left-hand housing element (not shown) that are molded or otherwise manufactured from a polymer or plastic material and are designed to fit together. to fit in. These housing elements may be secured together by snapping means, dowels and sockets molded or otherwise formed within the elements and/or by means of adhesive, screws, etc. Back element 50 has a proximal end 54 which has a flange 56 formed thereon. The flange 56 is configured to be pivotally supported in a groove 106 formed by paired ribs 108 that project inwardly from each of the housing elements 102, 104. Such an arrangement facilitates the attachment of the back element 50 to the assembly. cable assembly 100 and further allows the back element 50 to be rotated relative to the cable assembly 100 about the longitudinal axis A-A in a 360° trajectory.

[000285] As can be seen in Figure 1, the back element 50 passes through and is supported by a mounting pad 60 which is pivotally secured to the cable assembly 100. The mounting pad 60 has a proximal flange 62 and a distal flange 64 defining a rotational groove 65 that is configured to rotatably receive a nose portion 101 of the cable assembly 100. Such an arrangement allows the mounting pad 60 to pivot about the longitudinal axis A-A with respect to the cable assembly 100. handle 100. The back element 50 is non-rotatably pinned to the mounting pad 60 by a back pin 66. In addition, a rotary knob 70 is secured to the mounting pad 60. For example, the rotary knob 70 has a hollow mounting flange portion 72 which is sized to receive a mounting pad portion 60 therein. The knob 70 can be made of, for example, glass or carbon filled nylon, polycarbonate, Ultem®, etc., and is secured to the mounting pad 60 by the back stud 66 as well. In addition, an inwardly projecting retaining flange 74 is formed over the mounting flange portion 72 and is configured to extend into a radial groove 68 formed in the mounting pad 60. In this way, the surgeon can rotating the back element 50 (and the end actuator 12 attached thereto) about the longitudinal axis A-A in a 360° trajectory by holding the knob 70 and rotating it with respect to the cable assembly 100.

[000286] The anvil 20 is held in an open position by an anvil spring 21 and/or other limiting arrangement. The anvil 20 is selectively movable from the open position to various closed or clamping and firing positions by a firing system, generally designated as 109. The firing system 109 includes a "firing element" 110 comprising a hollow tube of trigger 110. The hollow trigger tube 110 is axially movable over the back element 50 and thereby forms the outer portion of the elongate rod assembly 40. The trigger tube 110 may be manufactured from a polymer or other suitable material and having a proximal end which is attached to a firing yoke 114 of the firing system 109. For example, the firing yoke 114 may be overmolded to the proximal end of the firing tube 110. However, other fastener arrangements may be employed.

[000287] As can be seen in Figure 1, the firing fork 114 is pivotally supported on a support collar 120 which is configured to move axially on the cable assembly 100. The support collar 120 has a pair of laterally extending fins which are sized to be slidably received in fin slots formed in the right and left housing elements. In that way, the support collar 120 can slide axially in the cable compartment 100 and still allow the firing fork 114 and the firing tube 110 to rotate with respect thereto about the longitudinal axis A-A. In accordance with the invention, a longitudinal slot is provided through the firing tube 110 to allow the dorsum pin 66 to extend therethrough into the dorsum element 50 while facilitating axial displacement of the firing tube 110 over the back element 50.

[000288] The firing system 109 further comprises a firing actuator 130 which serves to control the axial displacement of the firing tube 110 over the back element 50. See Figure 1. Such axial movement in the distal direction of the firing tube 110 in firing interaction with anvil 20 is referred to in this document as "firing motion". As can be seen in Figure 1, the trigger 130 is movably or pivotally coupled to the cable assembly 100 by means of a pivot pin 132. A torsion spring 135 is employed to move the trigger 130 away from the triggering portion. grip the pistol 107 of the handle assembly 100 to a non-actuated or initial "open" position. As can be seen in Figure 1, the firing trigger 130 has an upper portion 134 which is movably (pinned) attached to firing links 136 which are movably attached (pinned) to the support collar 120. Accordingly, movement of the trigger 130 from the initial position (FIG. 1) toward an end position adjacent to the pistol grip portion 107 of the handle assembly 100 will cause the trigger fork 114 and trigger tube 110 to collapse. move in the distal "DD" direction. Movement of firing trigger 130 in the opposite direction to pistol grip portion 107 of handle assembly 100 (under the action of torsion spring 135) will cause firing hook 114 and firing tube 110 to move in the same direction. proximal direction "PD" over the back element 50.

[000289] The present invention can be employed with different sizes and configurations of implantable staple cartridges. For example, the surgical instrument 10, when used in conjunction with a first trigger adapter 140, can be used with a 5 mm end actuator 12 that has a length of approximately 20 mm (or other lengths) that supports an implantable staple cartridge 30. This size end actuator may be particularly well suited, for example, to complete dissection and relatively fine vascular transactions. However, as will be discussed in more detail below, the surgical instrument 10 can also be employed, for example, in conjunction with other sizes of end actuators and staple cartridges by replacing the first firing adapter 140 with a second firing adapter. . As a further alternative, the elongated stem assembly 40 may be configured to be attached to only one end actuator shape or size.

[000290] A method of detachably coupling the end actuator 12 to the back element 50 will be explained below. The coupling process is initiated by inserting the swivel retaining pins 17 in the elongated channel 14 into the swivel pin cradles 52 in the back element 50. Thereafter, the surgeon advances the triggering trigger 130 towards the handle of the gun 107 of housing assembly 100 to distally advance firing tube 110 and first firing adapter 140 over a proximal end portion 47 of elongate channel 14 to thereby retain trunnions 17 in their respective cradles 52. first firing adapter 140 over swivel pins 17 is referred to in this document as the "coupled position". The present invention may also have an end actuator lock assembly to lock the trigger trigger 130 in position after an end actuator 12 has been attached to the back element 50.

[000291] More specifically, one embodiment of the end actuator locking assembly 160 includes a retaining pin 162 that is movably supported on the upper portion 134 of the trigger actuator 130. As discussed earlier, the trigger tube 162 trigger 110 should initially be advanced distally to the engaged position where the first trigger adapter 140 retains the rotating retaining pins 17 of the end actuator 12 in the rotating pin cradles 52 on the dorsum member 50. The surgeon advances the trigger adapter 140 distally to the engaged position by pulling the trigger 130 from the home position to the pistol grip 107. As the trigger 130 is initially actuated, the retaining pin 162 is moved distally until the tube trigger 110 has advanced the first trigger adapter 140 to the engaged position, at which point the retaining pin 162 is forced into a latch cavity 164 formed in the carcass item. Optionally, when detent pin 162 enters latch cavity 164, pin 162 may produce a latching or other sound, as well as providing a tactile indication to the surgeon that end actuator 12 has "locked" into the element. 50. Furthermore, the surgeon cannot inadvertently continue to actuate the trigger driver 130 to begin forming the clamps 32 on the end actuator 12 without intentionally forcing the retaining pin 162 out of the latch cavity 164. Similarly, if the surgeon releases the trigger 130 when it is in the engaged position, it will be held in that position by the retaining pin 162 to prevent the trigger trigger 130 from returning to the home position and thereby releasing the end actuator. 12 of the back element 50.

[000292] The present invention may also include a trigger lock button 137 that is pivotally secured to the cable assembly 100. In one form, the trigger lock button 137 has a lock 138 formed over a distal end thereof which is oriented to engage the firing yoke 114 when the firing release button is in a first latched position. As can be seen in Figure 1, the lock spring 139 serves to force the firing system lock button 137 into the first locked position. In various circumstances, the latch 138 serves to engage the firing fork 114 at a point where the position of the firing fork 114 on the back element 50 corresponds to a point at which the first firing adapter 140 is about to advance distally towards up on the nip ramp 28 over the anvil 20. One skilled in the art will understand that as the first trigger adapter 140 advances axially up the nip ramp 28, the anvil 20 will move in a path such that its portion of staple forming surface 22 will be substantially parallel to the top face 36 of staple cartridge 30.

[000293] After the end actuator 12 is coupled to the back element 50, the staple forming process is initiated by first pressing the firing system lock button 137 to allow the firing fork 114 to be moved additionally in a distal position on the dorsum element 50 and, finally, compressing the anvil 20 into the staple cartridge 30. After pressing the trigger lock button 137, the surgeon continues to actuate the trigger 130 in the pistol grip 107, thereby driving the first staple collar 140 upwards on the corresponding staple forming chute 29 to force the anvil 20 into forming contact with the staples 32 in the staple cartridge 30. trigger system lock 137 prevents accidental formation of staples 32 until the surgeon is ready to begin this process. In this embodiment, the surgeon must press the trigger lock button 137 before the trigger trigger 130 can be further actuated to begin the staple formation process.

[000294] The surgical instrument 10 can be used exclusively as a tissue stapling device if desired. However, the present invention may also include a fabric cutting system, generically designated 170. In at least one form, the fabric cutting system 170 comprises a knife element 172 that can be selectively advanced from an adjacent non-actuated position. to the proximal end of the end actuator 12 to a position actuated by actuation of a knife advance driver 200. The knife element 172 is movably supported on the back element 50 and is secured or otherwise projects from there. knife shank 180. Knife member 172 may be manufactured from, for example, 420 or 440 stainless steel with a hardness greater than 38 HRC (Rockwell Hardness C scale) and have a fabric cutting edge 176 formed over the distal end 174 thereof and configured to slidably extend through a slot in the anvil 20 and a centrally arranged slot 33 in the staple cartridge 30 to cut through tissue that is tightened. The knife shaft 180 extends through the back element 50 and has a proximal end portion that actionably interfaces with a knife drive that is functionally attached to the knife advance driver. 200. The knife advance driver 200 is attached to the pivot pin 132 so that it can be pivoted or otherwise actuated without actuating the trigger driver 130. In accordance with the invention, a first knife gear 192 is also attached. to pivot pin 132 so that actuation of knife advance driver 200 also pivots first knife gear 192. A trigger return spring 202 is secured between first knife gear 192 and cable housing 100 to force knife feed driver 200 to a home or non-actuated position.

[000295] The knife drive also includes a second knife gear 194 which is pivotally supported on a second gear spindle and in mesh with the first knife gear 192. The second knife gear 194 is in engagement meshed with a third knife gear 196 which is supported on a third gear spindle. Also supported on the third gear spindle 195 is a fourth knife gear 198. The fourth knife gear 198 is adapted to drively engage a series of annular gear teeth or rings on a proximal end of the knife shank 180. Des In this form, such an arrangement allows the fourth knife gear 198 to axially drive the knife shank 180 in the distal "DD" or proximal "PD" direction and further allows the firing shaft 180 to rotate about the longitudinal axis. A-A with respect to the fourth knife gear 198. Accordingly, the surgeon can axially advance the firing rod 180 and ultimately the knife element 172 in a distal position by pulling the knife advance driver 200 in the gripping direction of the knife. pistol 107 of cable assembly 100.

[000296] The present invention further includes a knife lock system 210 that prevents advancement of knife element 172 unless firing trigger 130 has been pulled to the fully fired position. This feature will therefore prevent activation of the knife advance system 170 unless they have first been fired or formed into the fabric. As can be seen in Figure 1, various implementations of the knife blocking system 210 comprise a knife blocking bar 211 that is pivotally supported on the pistol grip portion 107 of the handle assembly 100. The blocking bar knife blade 211 has an activation end 212 which is adapted to be engaged by the trigger trigger 130 when the trigger trigger 130 is in the full-fire position. In addition, the knife lock bar 211 has a retaining hook 214 at its other end which is adapted to fixedly engage a lock rod 216 over the first cutting gear 192. A knife lock spring 218 is employed to force the knife lock bar 211 to a "locked" position in which the retaining hook 214 is retained in engagement with the locking rod 216 to thereby prevent actuation of the knife advance driver 200 unless the trigger 130 is in full trigger position.

[000297] After the staples are "fired" (formed) in the target tissue, the surgeon can press the fire trigger release button 167 so that the trigger trigger 130 returns to the initial position under traction of the torsion spring 135 which in turn causes the anvil 20 to be forced into an open position under the action of the spring 21. When in the open position, the surgeon can withdraw the end actuator 12 leaving the implantable staple cartridge 30 and clamps 32 in place. In applications where the end actuator is inserted through a passage, working channel, etc., the surgeon returns the anvil 20 to the closed position activating the trigger trigger 130 to allow the end actuator 12 to be removed. through the passage or working channel. If, however, the surgeon wishes to cut the target tissue after firing the staples, the surgeon must activate the knife advance driver 200 in the manner described above to drive the knife bar 172 through the target tissue to the end of the actuator. end. Thereafter, the surgeon may release the knife advance driver 200 to allow the trigger return spring 202 to cause the trigger drive to return the knife bar 172 to the home (non-actuated) position. After the knife bar 172 is returned to the home position, the surgeon can open the end actuator grips 13 and 15 to release the implantable cartridge 30 in the patient and then withdraw the end actuator 12 from the patient. In this way, surgical instruments facilitate the use of small cartridges of implantable staples that can be inserted through relatively small working channels and passageways, while at the same time providing the surgeon with the option of firing the staples without cutting the tissue or, if desired, also cut the fabric after firing the staples.

[000298] Several unique and innovative embodiments of the present invention employ a compressible staple cartridge that supports staples in a substantially stationary position for anvil contact formation. The anvil is directed into the unformed staples where, for example, the degree of formation of the staple depends on how far the anvil is directed into the staples. Such an arrangement provides the surgeon with the ability to adjust the amount of forming or triggering pressure applied to the staples and thereby altering the final formed height of the staples. In the present invention, surgical stapling arrangements may employ staple drive elements that can lift the staples toward the anvil. This is described in more detail below.

[000299] Optionally, with respect to the above, the amount of trigger movement that is applied to the movable anvil depends on the degree of triggering of the trigger. For example, if the surgeon wishes to obtain only partially formed staples, then the firing trigger is only partially pressed inwards in the pistol grip direction 107. To obtain more staple formation, the surgeon simply presses the firing trigger further, the which results in the anvil being driven further into forming contact with the clamps. As used herein, the term "contact forming" means that the staple forming surface or staple forming pockets contact the ends of the legs of the staples and begin to form or flex the legs into a formed position. The degree of cleat formation refers to the amount of bending suffered by the legs of the cleats and finally refers to the cleat formation height as mentioned above. Those of ordinary skill in the art will further understand that because the anvil 20 moves in a substantially parallel relationship with the staple cartridge as firing motions are applied thereto, the staples are formed substantially simultaneously. with substantially equal formed heights.

[000300] Figures 2 and 3 illustrate a 12" reciprocating end actuator that is similar to the 12' end actuator described above, with the exception of the following differences which are configured to accommodate a knife bar 172'. The knife bar 172 ' is coupled to or protrudes from a knife shank 180 and is otherwise operated in the manner described above with respect to knife bar 172. However, in this embodiment, knife bar 172' is long enough for traverse the entire length of the end actuator 12" and therefore a separate distal knife element is not employed on the end actuator 12". The knife bar 172' has an upper cross member 173' and a lower cross member 175' formed thereon. Upper cross member 173' is oriented to slide across a corresponding elongated slot 250 in anvil 20" and lower cross member 175' is oriented to cross elongate slot 252 in groove elongated 14" from the 12" end actuator. A release slot (not shown) is also provided in the anvil 20" so that when the knife bar 172' is driven to an end position with the thin end actuator 12", the upper cross member 173' drops through the corresponding slot to allow the anvil 20" to move into the open position to disengage from the clamp and cut the tissue. The anvil 20" may otherwise be identical to the anvil 20 described above and the elongated groove 14" may be otherwise identically to the elongated channel 14 described above.

[000301] In these embodiments, the anvil 20" is forced into a fully open position (figure 2) by a spring or other opening arrangement (not shown). The anvil 20" is moved between the open and fully tightened positions by axial displacement. of the trigger adapter 150 in the manner described above. When the trigger adapter 150 is advanced to the fully tightened position (Figure 3), the surgeon can then advance the knife bar 172" distally, in the manner described above. If the surgeon wishes to use the end actuator as a handle device to manipulate the tissue, the trigger adapter can be moved proximally to allow the anvil 20" to move away from the elongated channel 14", as shown in Figure 4 in dashed lines. In this embodiment, when the knife bar 172" moves distally, upper cross member 173' and lower cross member 175' pull the anvil 20" and elongated groove 14" together to achieve the desired staple formation when knife bar 172" is advanced in distal position via the 12" end actuator. See Figure 5. Thus, in this embodiment, staple formation occurs simultaneously with tissue cutting, but staples can be formed sequentially as knife bar 172" is driven distally.

[000302] The unique and innovative features of the various surgical staple cartridges and surgical instruments of the present invention allow the staples in these cartridges to be arranged in one or more rows of linear or non-linear staples. A plurality of such rows of staples may be provided on each side of an elongate slot which is arranged centrally in the staple cartridge to receive the fabric cutting element therethrough. In one arrangement, for example, staples in one row may be substantially parallel to staples in adjacent rows of staples, but offset therefrom. As a further alternative, one or more rows of staples may be non-linear in nature. That is, the base of at least one staple in a row of staples may extend along an axis that is substantially transverse to the bases of other staples in the same row of staples. For example, the rows of staples on either side of the elongated slit may have a zigzag appearance.

[000303] According to the invention, a staple cartridge may comprise a cartridge body and a plurality of staples stored in the cartridge body. In use, the staple cartridge can be introduced into a surgical site and positioned on one side of the tissue being treated. In addition, the staple forming anvil can be positioned on the opposite side of the fabric. The anvil may be carried by a first jaw and the staple cartridge may be carried by a second jaw, whereby the first jaw and/or the second jaw may be moved towards each other. After the staple cartridge and anvil are positioned relative to the tissue, the staples can be ejected from the staple cartridge body so that the staples can pierce the tissue and contact the staple forming anvil. After the staples are applied from the staple cartridge body, the staple cartridge body can then be removed from the surgical site. The staple cartridge, or at least a portion of a staple cartridge, can be deployed with the staples. For example, as described in more detail below, a staple cartridge may comprise a cartridge body that can be compressed, crushed and/or flattened by the anvil when the anvil is moved from an open position to a closed position. When the cartridge body is compressed, crushed and/or flattened, the clamps positioned in the cartridge body can be deformed by the anvil. Alternatively, the jaw supporting the staple cartridge can be moved towards the anvil to a closed position. In either case, the clips can be deformed while still at least partially positioned in the cartridge body. In some cases, staples may not be ejected from the staple cartridge, while in other cases, staples may be ejected from the staple cartridge along with a portion of the cartridge body.

[000304] Now referring to Figures 6A to 6D, a compressible staple cartridge, such as the staple cartridge 1000, for example, may comprise an implantable compressible cartridge body 1010 and, in addition, a plurality of positioned staples 1020 in the body of the compressible cartridge 1010, although only one clip 1020 is shown in Figures 6A to 6D. Figure 6A illustrates the staple cartridge 1000 supported by a staple cartridge holder, or staple cartridge channel, 1030, with the staple cartridge 1000 being illustrated in an uncompressed condition. In such an uncompressed condition, the anvil 1040 may or may not be in contact with the tissue T. In use, the anvil 1040 can be moved from an open position in contact with the tissue T, as illustrated in Figure 6B, and position the tissue T against the cartridge body 1010. Although the anvil 1040 may position the fabric T against a tissue-contacting surface 1019 of the staple cartridge body 1010, again with reference to Figure 6B, the staple cartridge body 1010 may be subjected to little or no compressive force or pressure at such a point and the clamps 1020 may remain in an unformed or unfired condition. As illustrated in Figures 6A and 6B, the staple cartridge body 1010 may comprise one or more layers, and the staple legs 1021 of the staples 1020 may extend upwardly through these layers. The cartridge body 1010 may comprise a first layer 1011, a second layer 1012, a third layer 1013, with the second layer 1012 being disposed in an intermediate position between the first layer 1011 and the third layer 1013, and a fourth layer 1014, wherein the third layer 1013 may be disposed in an intermediate position between the second layer 1012 and the fourth layer 1014. The bases 1022 of the clips 1020 may be positioned in recesses 1015 in the fourth layer 1014 and the legs of the clips 1021 may be extending upwards from bases 1022 and through fourth layer 1014, third layer 1013 and second layer 1012, for example. Optionally, each deformable leg 1021 may comprise a point, such as the sharp point 1023, for example, which can be positioned on the second layer 1012, for example, when the staple cartridge 1000 is in an uncompressed condition. For example, prongs 1023 may not extend into and/or through first layer 1011, prongs 1023 may not protrude through tissue-contacting surface 1019 when staple cartridge 1000 is in a poor condition. not compressed. The sharp points 1023 may be positioned on the third layer 1013, and/or any other suitable layer, when the staple cartridge is in an uncompressed condition. Alternatively, the body of a staple cartridge can have any suitable number of layers such as less than four layers or more than four layers, for example.

[000305] Optionally, as described in more detail below, the first layer 1011 can be comprised of a reinforcing material and/or a plastic material, such as polydioxanone (PDS) and/or poly(glycolic acid) (PGA), for example for example, and the second layer 1012 may be comprised of a bioabsorbable foam material and/or a compressible hemostatic material, such as oxidized regenerated cellulose (ORC), for example. Optionally, one or more of the first layer 1011, the second layer 1012, the third layer 1013 and the fourth layer 1014 may hold the staples 1020 in the staple cartridge body 1010 and further maintain the staples 1020 in alignment with each other. the others. The third layer 1013 may be comprised of a reinforcing material, or a reasonably incompressible or inelastic material, which may be configured to maintain the clamp legs 1021 of the clamps 1020 in a position relative to one another. In addition, second layer 1012 and fourth layer 1014, which are positioned on opposite sides of third layer 1013, may stabilize, or reduce the movement of staples 1020 although second layer 1012 and fourth layer 1014 may be comprised of a material of compressible or elastic foam. The ends 1023 of the legs of the staples 1021 may be, at least partially, incorporated into the first layer 1011. For example, the first layer 1011 and the third layer 1013 may be configured to cooperatively and firmly hold the legs of the staples 1021 in position. . The first layer 1011 and the third layer 1013 may each be comprised of a sheet of bioabsorbable plastic such as poly(glycolic acid) (PGA) which is available under the tradename Vicryl, poly(lactic acid) (PLA or PLLA ), polydioxanone (PDS), poly(hydroxyalkanoate) (PHA), polyglecaprone 25 (PGCL) which is available under the tradename Monocryl, polycaprolactone (PCL) and/or a composite of PGA, PLA, PDS, PHA, PGCL and/or PCL, for example, and second layer 1012 and fourth layer 1014 can each be comprised of at least one hemostatic material or agent.

[000306] While the first layer 1011 may be compressible, the second layer 1012 may be substantially more compressible than the first layer 1011. For example, the second layer 1012 may be about twice as compressible, about three times as compressible, about four times as compressible, about five times as compressible, and/or about ten times as compressible, for example, as the first layer 1011. Said another way, the second layer 1012 can compress about twice, about three times, about four times, about five times, and/or about ten times more than the first layer 1011, for a given applied force. The second layer 1012 may be about twice as compressible and about ten times as compressible, for example, as the first layer 1011. The second layer 1012 may comprise a plurality of air voids defined therein, being that the amount and/or size of air voids in the second layer 1012 can be controlled to provide a desired compressibility of the second layer 1012. Similar to the above embodiment, although the third layer 1013 may be compressible, the fourth layer 1014 may be substantially more compressible than third layer 1013. For example, fourth layer 1014 may be about twice as compressible, about three times as compressible, about four times as compressible, about five times as compressible. compressible, and/or about ten times as compressible, for example, as the third layer 1013. Put another way, the fourth layer 1014 can compress about twice, about t three times, about four times, about five times, and/or about ten times more than the third layer 1013, for a given applied force. The fourth layer 1014 may be about twice as compressible and about ten times as compressible, for example, as the third layer 1013. The fourth layer 1014 may comprise a plurality of air voids defined therein, the The amount and/or size of the air voids in the fourth layer 1014 can be controlled to provide a desired compressibility of the fourth layer 1014. In various circumstances, the compressibility of a cartridge body, or cartridge body layer, can be expressed in terms of a compression ratio, that is, a distance over which a layer is compressed for a given amount of force. For example, a layer that has a high compression ratio will compress a greater distance for a given amount of compression force applied to the layer compared to a layer that has a lower compression ratio. That said, the second layer 1012 may have a higher compression ratio than the first layer 1011, and similarly, the fourth layer 1014 may have a higher compression ratio than the third layer 1013. The second layer 1012 and fourth layer 1014 may be comprised of the same material and may comprise the same compression ratio. The second layer 1012 and the fourth layer 1014 may be comprised of materials that have different compression ratios. Similarly, the first layer 1011 and the third layer 1013 may be comprised of the same material and may comprise the same compression ratio. First layer 1011 and third layer 1013 may be comprised of materials having different compression ratios.

[000307] As the anvil 1040 is moved toward its closed position, the anvil 1040 can contact the tissue T and apply a compressive force to the tissue T and staple cartridge 1000, as illustrated in Figure 6C . In such circumstances, the anvil 1040 may force the top surface, or the tissue-contacting surface 1019, of the cartridge body 1010 down towards the staple cartridge holder 1030. The staple cartridge holder 1030 may comprise a cartridge supporting surface 1031 which can be configured to support the staple cartridge 1000 as the staple cartridge 1000 is compressed between the cartridge supporting surface 1031 and the tissue contacting surface 1041 of the anvil 1040. to the pressure applied by the anvil 1040, the cartridge body 1010 can be compressed and the anvil 1040 can contact the clamps 1020. More particularly, the compression of the cartridge body 1010 and the downward movement of the tissue contact surface 1019 can cause the ends 1023 of the legs of the staples 1021 to pierce the first layer 1011 of the cartridge body 1010, pierce the fabric T, and enter the forming pockets 1042 in the bigo 1040. As the cartridge body 1010 is further compressed by the anvil 1040, the prongs 1023 may contact the walls defining the forming pockets 1042 and, as a result, the legs 1021 may be deformed or bent inwardly, for example, as illustrated in Figure 6C. As the legs of the staples 1021 are deformed, as also illustrated in Figure 6C, the bases 1022 of the staples 1020 may contact or be supported by the staple cartridge holder 1030. Optionally, as described in more detail below, the staple cartridge holder 1030 may comprise a plurality of support features, such as grooves, slots or staple holder recesses 1032, for example, which may be configured to support the staples 1020, or at least the bases 1022 of the staples 1020 , as the clamps 1020 are deformed. As also illustrated in Figure 6C, the cavities 1015 in the fourth layer 1014 can flatten as a result of the compressive force applied to the staple cartridge body 1010. In addition to cavities 1015, the staple cartridge body 1010 may additionally comprise one or more voids, such as voids 1016, for example, which may or may not comprise a portion of a staple positioned therein, which may be configured to allow the 1010 cartridge body to be flattened. Cavities 1015 and/or voids 1016 may be configured to flatten so that the walls defining the cavities and/or walls are deflected downwardly and contact the platform surface of the cartridge 1031 and/or contact a layer of the cartridge body 1010 positioned under the cavities and/or voids.

[000308] Comparing Figure 6B and Figure 6C, it is evident that the second layer 1012 and the fourth layer 1014 were substantially compressed by the compressive pressure applied by the anvil 1040. It can also be seen that the first layer 1011 and the third layer 1013 were also compressed. As the anvil 1040 is moved to its closed position, the anvil 1040 may continue to further compress the cartridge body 1010 by forcing the tissue-contacting surface 1019 down toward the staple cartridge holder 1030. cartridge body 1010 is further compressed, anvil 1040 can deform clamps 1020 into their fully formed shape, as illustrated in Figure 6D. Referring to Figure 6D, the legs 1021 of each staple 1020 may be deformed downwardly toward the base 1022 of each staple 1020 to capture at least a portion of the T fabric, of the first layer 1011, of the second layer 1012, of the third layer. 1013, and fourth layer 1014 between deformable legs 1021 and base 1022. Comparing Figures 6C and 6D, it is further evident that second layer 1012 and fourth layer 1014 were substantially further compressed by the compressive pressure applied by the anvil 1040. It can also be seen after comparing Figures 6C and 6D that the first layer 1011 and the third layer 1013 were also further compressed. After the staples 1020 are completely, or at least sufficiently, formed, the anvil 1040 can be lifted away from the tissue T and the staple cartridge holder 1030 can be removed from, and/or detached from, the staple cartridge 1000. shown in Figure 6D, and as a result of the foregoing, cartridge body 1010 can be implanted with staples 1020. In various circumstances, implanted cartridge body 1010 can support tissue along the row of staples. In some circumstances, a hemostatic agent and/or any other suitable therapeutic drug contained in the body of the implanted cartridge 1010 can treat tissue over time. A hemostatic agent, as mentioned above, can reduce the bleeding of stapled and/or cut tissue while a binding agent or tissue adhesive can provide strength to the tissue over time. The 1010 implanted cartridge body can be comprised of materials such as ORC (oxidized regenerated cellulose), extracellular proteins such as collagen, poly(glycolic acid) (PGA) which is available under the trade name Vicryl, poly(lactic acid) (PLA or PLLA) ), polydioxanone (PDS), poly(hydroxyalkanoate) (PHA), polyglecaprone 25 (PGCL) which is available under the tradename Monocryl, polycaprolactone (PCL) and/or a composite of PGA, PLA, PDS, PHA, PGCL and/or or PCL, for example. In certain circumstances, the cartridge body 1010 may comprise an antibiotic and/or antimicrobial material, such as colloidal silver and/or triclosan, for example, which may reduce the possibility of infection at the surgical site.

[000309] The 1010 cartridge body layers can be connected to each other. Second layer 1012 can be adhered to first layer 1011, third layer 1013 can be adhered to second layer 1012 and fourth layer 1014 can be adhered to third layer 1013 using at least one adhesive such as fibrin and/or hydrogel of protein, for example. Although this is not illustrated, the layers of the cartridge body 1010 can be connected together by mechanical interlocking feature. For example, the first layer 1011 and the second layer 1012 may each comprise corresponding interlocking features, such as a tongue and groove arrangement and/or a mortise joint arrangement, for example. Similarly, second layer 1012 and third layer 1013 may each comprise corresponding interlocking features, while third layer 1013 and fourth layer 1014 may each comprise corresponding interlocking features. Although not illustrated, staple cartridge 1000 may comprise one or more rivets, for example, which may extend through one or more layers of cartridge body 1010. For example, each rivet may comprise a first end, or head. , positioned adjacent the first layer 1011 and a second head positioned adjacent the fourth layer 1014 which may be mounted on or formed by a second end of the rivet. Due to the compressible nature of the cartridge body 1010, the rivets may compress the cartridge body 1010 so that the rivet heads can be recessed relative to the fabric contacting surface 1019 and/or the bottom surface 1018 of the cartridge body. 1010 cartridge, for example. For example, rivets may consist of a bioabsorbable material such as polyglycolic acid (PGA), available under the tradename Vicryl, polylactic acid (PLA or PLLA), polydioxanone (PDS), polyhydroxyalkanoate (PHA), polyglecaprone 25 (PGCL), available under the tradename Monocryl, polycaprolactone (PCL), and/or a compound of PGA, PLA, PDS, PHA, PGCL and/or PCL, for example. The layers of the cartridge body 1010 may not be connected to each other, apart from clips 1020 contained therein. For example, frictional engagement between the legs of the clamps 1021 and the cartridge body 1010, for example, can hold the layers of the cartridge body 1010 together, and after the clamps are formed, the layers can be captured in the clamps 1020. At least a portion of the legs of the clamps 1021 may comprise a roughened surface or a rough coating which can increase the frictional forces between the clamps 1020 and the cartridge body 1010.

[000310] As described above, a surgical instrument may comprise a first jaw that includes the staple cartridge holder 1030 and a second jaw that includes the anvil 1040. Optionally, as described in more detail below, the staple cartridge 1000 may comprising one or more retaining features that can be configured to engage the staple cartridge holder 1030 and, as a result, releasably retain the staple cartridge 1000 in the staple cartridge holder 1030. The staple cartridge 1000 is clampable to the staple cartridge holder 1030 by at least one adhesive, such as fibrin and/or protein hydrogel, for example. In use, in at least one circumstance, specifically in laparoscopic and/or endoscopic surgery, the second jaw can be moved to a closed position opposite the first jaw, for example, so that the first and second jaws can be inserted through a trocar in a surgical site. For example, the trocar may define an opening, or cannula, of approximately 5 mm, through which the first and second jaws can be inserted. The second jaw can be moved into a partially closed position intermediate between the open position and the closed position which can allow the first and second jaws to be inserted through the trocar without deforming the staples 1020 contained in the staple cartridge body 1010. For example, the anvil 1040 may not apply a compressive force to the staple cartridge body 1010 when the second jaw is in its partially closed intermediate position while the anvil 1040 may compress the staple cartridge body 1010 when the second jaw is in its partially closed intermediate position. Although the anvil 1040 may compress the staple cartridge body 1010 when in such an intermediate position, the anvil 1040 may not sufficiently compress the staple cartridge body 1010 such that the anvil 1040 contacts the staples 1020 and/or or so that staples 1020 are deformed by anvil 1040. After the first and second jaws are inserted through the trocar into the surgical site, the second jaw can be opened again and the anvil 1040 and staple cartridge 1000 can be positioned relative to the target tissue as described above.

[000311] Now referring to Figures 7A to 7D, an end actuator of a surgical stapler may comprise an implantable staple cartridge 1100 placed in an intermediate position between an anvil 1140 and a staple cartridge holder 1130. In the above embodiment, the anvil 1140 may comprise a tissue-contacting surface 1141, the staple cartridge 1100 may comprise a tissue-contacting surface 1119, and the staple cartridge holder 1130 may comprise a platform surface 1131 that can be configured to support the staple cartridge 1100. Referring to Figure 7A, the anvil 1140 may be used to position the fabric T against the tissue contacting surface 1119 of the staple cartridge 1100 without deforming the staple cartridge 1100, and when the anvil 1140 is in such a position, the tissue contacting surface 1141 may be positioned a distance 1101a from the support surface of the cartridge staples 1131 and tissue contacting surface 1119 can be positioned a distance 1102a from staple cartridge support surface 1131. Thereafter, as anvil 1140 is moved towards staple cartridge support 1130, now with Referring to Figure 7B, the anvil 1140 can force the top surface, or the tissue-contacting surface 1119, of the staple cartridge 1100 downwards and compress the first layer 1111 and the second layer 1112 of the cartridge body 1110. As layers 1111 and 1112 are compressed, again with reference to Figure 7B, the second layer 1112 can be crushed and the legs 1121 of the staples 1120 can pierce the first layer 1111 and enter the fabric T. For example, the staples 1120 can be at least partially positioned in the staple cavities, or voids, 1115 in the second layer 1112, and when the second layer 1112 is compressed, the staple cavities 1115 may flatten and, as a result, remain The second layer 1112 may be flattened around the clips 1120. The second layer 1112 may comprise covering portions 1116 which may extend over the clip recesses 1115 and enclose, or at least partially enclose, the clip recesses 1115. Figure 7B illustrates cover portions 1116 being crushed down into staple cavities 1115. Second layer 1112 may comprise one or more weakened portions which may facilitate flattening of second layer 1112. Optionally, such weakened portions may comprise markings, perforations and/or thin cross-sections, for example, that can facilitate a controlled flattening of the cartridge body 1110. The first layer 1111 can comprise one or more weakened portions that can facilitate penetration of the legs of the staples 1121 through the first layer. 1111. Optionally, these weakened portions may comprise markings, perforations and/or cross-sections. thin salts, for example, which may be aligned, or at least substantially aligned, with the legs of the clamps 1121.

[000312] When the anvil 1140 is in a partially closed unfired position, again with reference to Figure 7A, the anvil 1140 can be positioned a distance 1101a from the support surface of the cartridge 1131 so that a gap is defined in that region. This gap can be filled by the staple cartridge 1100, which has a height of the staple cartridge 1102a, and the fabric T. As the anvil 1140 is moved downward to compress the staple cartridge 1100, again with reference to Figure 7B , the distance between the fabric contact surface 1141 and the cartridge support surface 1131 can be defined by a distance 1101b which is shorter than the distance 1101a. In various circumstances, the gap between the tissue-contacting surface 1141 of the anvil 1140 and the platform surface of the cartridge 1131, defined by the distance 1101b, may be greater than the original, undeformed height of the staple cartridge 1102a. As the anvil 1140 is moved closer to the cartridge support surface 1131, now referring to Figure 7C, the second layer 1112 can continue to be flattened and the distance between the legs of the clamps 1121 and the forming pockets 1142 can decrease. Similarly, the distance between the tissue-contacting surface 1141 and the platform surface of the cartridge 1131 may decrease to a distance 1101c which may be greater than, equal to, or less than the original, undeformed height of the cartridge 1102a. . Referring now to Figure 7D, the anvil 1140 can be moved to a final firing position in which the clamps 1120 have been fully formed, or at least formed to a desired height. In this position, the tissue contacting surface 1141 of the anvil 1140 may be a distance 1101d from the platform surface of the cartridge 1131, with the distance 1101d being shorter than the original, undeformed height of the cartridge 1102a. As also illustrated in Figure 7D, clamp cavities 1115 may be completely, or at least substantially, flattened and clamps 1120 may be completely, or at least substantially, surrounded by second flattened layer 1112. In various circumstances, anvil 1140 may thereafter be moved away from the staple cartridge 1100. After the anvil 1140 is disengaged from the staple cartridge 1100, the cartridge body 1110 can at least partially re-expand at various locations, i.e., intermediate locations of adjacent staples 1120 , for example. The crushed cartridge body 1110 may not resiliently re-expand. The formed clips 1120 and, in addition, the cartridge body clips 1110 placed in an adjacent intermediate position 1120 may apply pressure, or compressive forces, to the T-tissue, which may provide various therapeutic benefits.

[000313] As discussed earlier, again with reference to Figure 7A, each clamp 1120 may comprise clamp legs 1121 extending therefrom. While staples 1120 are shown as comprising two staple legs 1121, multiple staples may be used which may comprise one staple leg or, alternatively, more than two staple legs, such as three staple legs or four staple legs, for example . As illustrated in Figure 7A, each clamp leg 1121 can be incorporated into the second layer 1112 of the cartridge body 1110 so that the clamps 1120 are secured to the second layer 1112. The clamps 1120 can be inserted into the clamp cavities 1115 in the cartridge body. cartridge 1110 so that the prongs 1123 of the legs of the clamps 1121 enter the cavities 1115 before the bases 1122. After the prongs 1123 are inserted into the cavities 1115, the prongs 1123 can be pressed against the cover portions 1116 and cut the second layer 1112. Clips 1120 may be seated deep enough in second layer 1112 so that clips 1120 do not move, or at least substantially move, relative to second layer 1112. Clips 1120 may be seated deep enough in the second layer 1112 so that the bases 1122 are positioned or incorporated into the staple cavities 1115. Alternatively, the bases 1122 may not be positioned. or incorporated into the second layer 1112. Again referring to Figure 7A, the bases 1122 may extend below the bottom surface 1118 of the cartridge body 1110. The bases 1122 may rest on, or may be positioned directly against, the surface of cartridge platform 1130. Cartridge platform surface 1130 may comprise support features extending therefrom and/or defined therein whereby, for example, bases 1122 of clamps 1120 may be positioned on and supported by one or more support grooves, slots or recesses 1132, for example in the staple cartridge holder 1130, as described in more detail below.

[000314] Now referring to Figures 8 and 9, a staple cartridge, such as staple cartridge 1200, for example, may comprise a compressible implantable cartridge body 1210 comprising an outer layer 1211 and an inner layer 1212. Similar to the above embodiment, staple cartridge 1200 may comprise a plurality of staples 1220 positioned in cartridge body 1210. Optionally, each staple 1220 may comprise a base 1222 and one or more staple legs 1221 extending from the same. For example, the legs of the staples 1221 may be inserted into the inner layer 1212 and seated at a depth at which the bases 1222 of the staples 1220 are bordering and/or disposed adjacent to the bottom surface 1218 of the inner layer 1212. , for example. In Figures 8 and 9, inner layer 1212 does not comprise staple cavities configured to receive a portion of staples 1220 while, alternatively, inner layer 1212 may comprise such staple cavities. In addition to the above, the inner layer 1212 may consist of a compressible material, such as bioabsorbable foam and/or oxidized regenerated cellulose (ORC), for example, which may be configured to allow the cartridge body 1210 to be flattened when a compressive load is applied to it. The inner layer 1212 may consist of a lyophilized foam comprising polylactic acid (PLA) and/or polyglycolic acid (PGA), for example. The ORC may be commercially available under the tradename Surgicel and may comprise a loose woven cloth (such as a surgical sponge), loose fibers (such as a cotton ball) and/or a foam. The inner layer 1212 may be comprised of a material that includes drugs such as thrombin and/or freeze-dried fibrin, e.g. contained therein and/or coated on top of the layer, which may be activated by water and/or activated by fluids in the patient's body, for example. For example, freeze-dried thrombin and/or fibrin can be maintained in a Vicryl matrix (PGA), for example. In certain circumstances, however, activatable drugs may be unintentionally activated when the staple cartridge 1200 is inserted into a surgical site on the patient, for example. Referring again to Figures 8 and 9, the outer layer 1211 may be comprised of a material impermeable to water, or at least substantially impermeable to water, so that liquids do not come into contact with, or at least substantially contact with, the surface. inner layer 1212 until the cartridge body 1210 has been compressed and the legs of the staples have penetrated the outer layer 1211 and/or until the outer layer 1211 has been cut in some way. The outer layer 1211 may consist of a reinforcing material and/or plastic material, such as polydioxanone (PDS) and/or polyglycolic acid (PGA), for example. Outer layer 1211 may comprise a wrapper that surrounds inner layer 1212 and clips 1220. More particularly, clips 1220 may be inserted into inner layer 1212 and outer layer 1211 may be wrapped around the subassembly comprising inner layer 1212 and clamps 1220 and then sealed.

[000315] As described herein, the staples of a staple cartridge can be formed entirely by an anvil when the anvil is moved to a closed position. Alternatively, now referring to Figures 10 to 13, the staples of a staple cartridge, such as the staple cartridge 4100, for example, can be deformed by an anvil when the anvil is moved to a closed position and, additionally, by a clamp drive system that moves the clamps towards the closed anvil. The staple cartridge 4100 may comprise a compressible body 4110 which may consist of a foam material, for example, and a plurality of staples 4120 positioned, at least partially, in the compressible body 4110. The staple drive system may comprise a staple drivers 4160, a plurality of staple drivers 4162 positioned on driver holders 4160, and a staple cartridge housing 4180 that can be configured to retain staple drivers 4162 in driver holder 4160. - Clamp drivers 4162 can be positioned in one or more slots 4163 in driver support 4160, so that the side walls of the slits 4163 can help guide clamp drivers 4162 upward toward the anvil. Clamps 4120 can be held in slots 4163 by clamp drivers 4162, with clamps 4120 being fully positioned in slots 4163 when clamps 4120 and clamp drivers 4162 are in the unfired position. Alternatively, at least a portion of the clamps 4120 may extend upwardly through the open ends 4161 of the slots 4163 when the clamps 4120 and the clamp drivers 4162 are in the unfired position. For example, with reference primarily to Figure 11, the bases of the clamps 4120 may be positioned on the actuator support 4160 and the tips of the clamps 4120 may be immersed in the compressible body 4110. Approximately one third of the height of the clamps 4120 may be positioned on the support of drivers 4160 and approximately two-thirds of the height of the 4120 clamps can be positioned on the cartridge body 4110.

[000316] Referring to Figure 10A, the staple cartridge 4100 may additionally comprise a water-impermeable wrapper or membrane 4111 surrounding the cartridge body 4110 and driver support 4160, for example.

[000317] In use, the staple cartridge 4100 can be placed in a staple cartridge groove, for example, and the anvil can be moved towards the staple cartridge 4100 to a closed position. The anvil may contact and compress the compressible body 4110 when the anvil is moved to its closed position. The anvil may not contact the 4120 clamps when it is in the closed position. The anvil may contact the legs of the clamps 4120 and at least partially deform the clamps 4120 when the anvil is moved to the closed position. In any of these cases, the staple cartridge 4100 may additionally comprise one or more sliders 4170 that can be advanced longitudinally on the staple cartridge 4100 so that the sliders 4170 can sequentially engage the staple drivers 4162 and move the staple drivers 4162. clamps 4162 and clamps 4120 towards the anvil. Sliders 4170 can slide between the staple cartridge compartment 4180 and staple drivers 4162. When closing the anvil has started the process of forming the staples 4120, the upward movement of the staples 4120 towards the anvil can complete the process of forming the staples 4120. forming and deforming the clamps 4120 to their fully formed, or at least desired, height. When closing the anvil has not deformed the clamps 4120, upward movement of the clamps 4120 towards the anvil can initiate and complete the forming process and deform the clamps 4120 to their fully formed, or at least desired, height. Sliders 4170 may be advanced from a proximal end of the staple cartridge 4100 to a distal end of the staple cartridge 4100 so that the staples 4120 positioned at the proximal end of the staple cartridge 4100 are formed completely before the staples 4120 positioned at the distal end of the staple cartridge 4100 are fully formed. Referring to Figure 12, the sliders 4170 may each comprise at least one angled or sloped surface 4711 that can be configured to slide under the staple drivers 4162 and lift the staple drivers 4162 as illustrated in Fig. Figure 13.

[000318] In addition to the above description, the staples 4120 may be formed to capture at least a portion of the T-tissue and at least a portion of the compressible body 4110 of the staple cartridge 4100. After the staples 4120 are formed, the anvil and staple cartridge channel 4130 of the surgical stapler may be spaced away from the implanted staple cartridge 4100. In various circumstances, the cartridge housing 4180 may be fixedly engaged with the staple cartridge channel 4130 so that, as a result, the cartridge housing 4180 can be separated from compressible body 4110 as staple cartridge groove 4130 is spaced away from implanted cartridge body 4110. Referring again to Figure 10, cartridge housing 4180 may comprise opposing side walls 4181 between which cartridge body 4110 may be removably positioned. For example, the compressible cartridge body 4110 can be compressed between the side walls 4181 so that the cartridge body 4110 can be removably retained in that region during use and releasably disengaged from the cartridge housing 4180 as the 4180 cartridge compartment is removed. For example, the 4160 Trigger Holder can be attached to the 4180 Cartridge Slot so that the 4160 Trigger Holder, 4162 Triggers and/or 4170 Slides can remain in the 4180 Cartridge Slot when the 4180 Cartridge Slot is removed from the surgical site. The 4162 Triggers can be ejected from the 4160 Trigger Holder and left in the surgical site. For example, 4162 triggers can be comprised of a bioabsorbable material such as polyglycolic acid (PGA), available under the tradename Vicryl, polylactic acid (PLA or PLLA), polydioxanone (PDS), polyhydroxyalkanoate (PHA), polyglecaprone 25 (PGCL), available under the tradename Monocryl, polycaprolactone (PCL), and/or a compound of PGA, PLA, PDS, PHA, PGCL and/or PCL, for example. Drivers 4162 may be attached to clamps 4120 such that drivers 4162 are deployed with clamps 4120. For example, each driver 4162 may comprise a recess configured to receive the bases of clamps 4120, for example, the recesses being able to be configured to hold the bases of the clamps by pressure and/or by snapping.

[000319] In addition to the above, driver holder 4160 and/or sliders 4170 can be ejected from cartridge housing 4180. For example, sliders 4170 can slide between cartridge housing 4180 and driver holder. sliders 4160 so that as sliders 4170 are advanced to drive staple drivers 4162 and staple drivers 4120 upward, sliders 4170 can also move driver support 4160 up and out of cartridge compartment 4180. For example, the 4160 Driver Holder and/or the 4170 Slider may consist of a bioabsorbable material such as polyglycolic acid (PGA), available under the tradename Vicryl, polylactic acid (PLA or PLLA), polydioxanone (PDS), poly- hydroxyalkanoate (PHA), polyglecaprone 25 (PGCL), available under the tradename Monocryl, polycaprolactone (PCL), and/or a compound of PGA, PLA, PDS, PHA, PGCL and/or PCL, for example. Sliders 4170 may be integrally formed and/or attached to a drive bar, or cutting element, which pushes slides 4170 through staple cartridge 4100. In such cases, slides 4170 may not be ejected from the cartridge housing. 4180 and may remain with the surgical stapler whereas, in other cases where the slides 4170 are not attached to the drive bar, the slides 4170 may be left in the surgical site. In any case, in addition to the above, the compressibility of the cartridge body 4110 may allow the use of thicker staple cartridges in the end actuator of a surgical stapler, since the cartridge body 4110 may compress, or retract. , when the stapler anvil is closed. As a result of at least partial deformation of the staples upon closing the anvil, taller staples could be used, such as staples that have a height of approximately 4.6 mm (0.18 inches), for example, with a height of approximately 3.0 mm (0.12 inch) from the height of the clip may be positioned on the compressible layer 4110 and wherein the compressible layer 4110 may have an uncompressed height of approximately 3.6 mm (0 .14 inch), for example.

[000320] As described herein, a staple cartridge may comprise a plurality of staples therein. Optionally, such staples may consist of a metal wire deformed into a substantially U-shaped configuration having two staple legs. Alternatives are envisaged in which the clips may comprise different configurations such as two or more strands which have been joined together and having three or more clip legs. The yarn or yarns used to form the staples may comprise a round, or at least substantially round, cross-section. The staple wires may comprise any other suitable cross-section, such as square and/or rectangular cross-sections, for example. Staples may consist of plastic threads. Staples may consist of plastic coated metal wires. In accordance with the invention, a cartridge may comprise any suitable type of fastener in addition to or in place of staples. For example, such a fastener may comprise pivoting arms which are bent when engaged by an anvil. Two-piece fasteners could be used. For example, a staple cartridge may comprise a plurality of first fastener portions and an anvil may comprise a plurality of second fastener portions which are connected to the first fastener portions when the anvil is pressed against the staple cartridge. As described above, a slider or driver can be advanced into a staple cartridge to complete the staple forming process. A slider or driver may be advanced within an anvil to move downwardly one or more forming elements in engagement with the staple cartridge and the opposing staples, or fasteners, positioned therein.

[000321] A staple cartridge may comprise four rows of staples stored therein. The four rows of staples can be arranged into two rows of inner staples and two rows of outer staples. For example, an inner row of staples and an outer row of staples can be positioned on a first side of a cutting element, or knife, slot in the staple cartridge, and similarly, an inner row of staples and a row of staples. of external staples can be positioned on a second side of the cutting element slot, or knife. A staple cartridge may not comprise a cutting element slot; however, such a staple cartridge may comprise a designated portion configured to be cut by a cutting element instead of a staple cartridge slot. The inner staple rows may be arranged in the staple cartridge so that they are equally, or at least substantially equally, spaced from the cutting element slot. Similarly, rows of outer staples may be arranged on the staple cartridge so that they are equally, or at least substantially equally, spaced from the cutting element slot. In accordance with the invention, a staple cartridge may comprise more or less than four rows of staples. A staple cartridge may comprise six rows of staples. For example, the staple cartridge may comprise three rows of staples on a first side of a cutting element slot and three rows of staples on a second side of the cutting element slot. A staple cartridge may comprise an odd number of rows of staples. For example, a staple cartridge may comprise two rows of staples on a first side of a cutting element slot and three rows of staples on a second side of the cutting element slot. The rows of staples may comprise staples that have the same, or at least substantially the same, unformed staple height. Alternatively, one or more of the rows of staples may comprise staples that have an unformed staple height different from the height of other staples. For example, staples on a first side of a cutting element slot can have a first unformed height and staples on a second side of a cutting element slot can have a second unformed height that is different from the first height. , for example.

[000322] Optionally, as described above, a staple cartridge may comprise a cartridge body that includes a plurality of staple cavities defined therein. The cartridge body may comprise a support and an upper support surface, where each staple cavity may define an opening in the support surface. As also described above, a staple can be positioned within each staple cavity so that the staples are stored within the cartridge body until they are ejected. Prior to being ejected from the cartridge body, the staples may be contained with the cartridge body so that the staples do not protrude above the platform surface. When the staples are positioned below the platform surface, in such cases the possibility of the staples becoming damaged and/or prematurely contacting the target tissue can be reduced. In various circumstances, clips can be moved between an unfired position in which they do not protrude from the cartridge body and a fired position in which they emerge from the cartridge body and can contact an anvil positioned opposite the cartridge. of staples. The anvil and/or forming pockets defined within the anvil may be positioned a predetermined distance above the platform surface so that when the staples are being dispensed from the cartridge body they are deformed to a predetermined formed height. In some cases, the thickness of tissue captured between the anvil and staple cartridge may vary and as a result, thicker tissue may be captured within certain staples while thinner tissue may be captured within certain other staples. In any case, the pinching pressure, or force, applied to the tissue by the staples may vary from staple to staple or can vary between a staple at one end of a row of staples and a staple at the other end of the row of staples, for example. . Under certain circumstances, the gap between the anvil and the staple cartridge holder can be controlled so that the staples apply a certain minimum pinch pressure within each staple. In some such circumstances, however, there may still be significant variation in pinch pressure within different clamps. Similar surgical stapling instruments are disclosed in US Patent No. 7,380,696, which was issued June 3, 2008, the disclosure of which is incorporated herein by reference. An illustrative multi-stroke handle for the surgical stapling and cutting instrument is described in greater detail in the co-pending US patent application by the same holder entitled SURGICAL STAPLING INSTRUMENT INCORPORATING A MULTITROKE FIRING POSITION INDICATOR AND RETRACTION MECHANISM, Serial No. 10/374,026), the contents of which are incorporated herein by reference in their entirety. Other applications compatible with the present invention may incorporate a single firing stroke, as described in the co-pending and co-pending US patent application SURGICAL STAPLING INSTRUMENT HAVING SEPARATE DISTINCT CLOSING AND FIRING SYSTEMS, Serial No. 10/441,632), the contents of which are is incorporated herein by reference in its entirety.

[000323] As described herein, a staple cartridge may comprise means for compensating for the thickness of tissue captured within staples dispensed from the staple cartridge. Referring to Figure 14, a staple cartridge, such as the staple cartridge 10000, for example, may include a rigid first portion, such as the support portion 10010, for example, and a second compressible portion, such as the 10020 fabric, for example. Referring primarily to Figure 16, the support portion 10010 may comprise a cartridge body, an upper platform surface 10011, and a plurality of staple cavities 10012 wherein, similarly to the above, each staple cavity 10012 may define an opening in the platform surface 10011. A clamp 10030, for example, may be removably positioned in each clamp cavity 10012. For example, each clamp 10030 may comprise a base 10031 and one or more legs 10032 extending therefrom. starting from base 10031. Before staples 10030 are dispensed, as also described in more detail below, bases 10031 of staples 10030 may be supported by staple drivers positioned within support portion 10010 and, simultaneously, legs 10032 of the clips 10030 may be at least partially contained within the clip cavities 10012. The clips 10030 may be dispensed between a position not fired and a fired position such that legs 10032 move through fabric thickness compensator 10020, penetrate through a top surface of fabric thickness compensator 10020, penetrate fabric T, and contact an anvil positioned opposite the staple cartridge 10000. When the legs 10032 are deformed against the anvil, the legs 10032 of each staple 10030 can capture a portion of the fabric thickness compensator 10020 and a portion of the fabric T within each staple 10030 and apply a compressive force to the fabric. In addition to the above, the legs 10032 of each staple 10030 can be deformed downwardly towards the base 10031 of the staple to form a staple gripping area 10039 in which the fabric T and the fabric thickness compensator 10020 can be captured. In various circumstances, the clamp gripping area 10039 can be defined between the inner surfaces of the deformed legs 10032 and the inner surface of the base 10031. The size of the gripping area for a staple can depend on various factors, such as the length of the legs. , the diameter of the legs, the width of the base, and/or the extent to which the legs are deformed, for example.

[000324] In the past, it was often necessary for the surgeon to select the proper staples with the proper staple height for the tissue being stapled. For example, a surgeon might select tall staples for use with thick tissue and short staples for use with thin tissue. In some circumstances, however, the fabric being stapled did not have a consistent thickness, and therefore some staples were unable to achieve the desired fired configuration. For example, Figure 48 illustrates a high staple used in thin fabric. Referring now to Figure 49, when a fabric thickness compensator, such as the fabric thickness compensator 10020, for example, is used with thin fabric, for example, the larger staple can be formed to a desired fired configuration.

[000325] Due to the compressibility of the fabric thickness compensator, the fabric thickness compensator can compensate for the thickness of the fabric captured inside each staple. More particularly, now referring to Figures 43 and 44, a fabric thickness compensator, such as the fabric thickness compensator 10020, for example, may consume larger and/or smaller portions of the staple gripping area 10039 of each staple 10030 depending on the thickness and/or type of fabric contained within the staple gripping area 10039. For example, if thinner tissue T is captured within a staple 10030, the fabric thickness compensator 10020 may consume a larger portion of the area 10039 compared to cases where thicker tissue T is captured inside the staple 10030. Correspondingly, if thicker tissue T is captured inside a staple 10030, the tissue thickness compensator 10020 may consume a portion smaller 10039 staple entrapment area compared to cases where thinner tissue T is captured within the 10030 staple. In this way, the tec thickness compensator This method can compensate for thinner tissue and/or thicker tissue and ensure that compressive pressure is applied to the tissue independently, or at least substantially independent, of the thickness of the tissue captured within the staples. In addition to the above, the fabric thickness compensator 10020 can compensate for different types, or compressibilities of fabrics captured within different staples 10030. Now, referring to Figure 44, the fabric thickness compensator 10020 can apply a force of compression to vascular tissue T which may include vessels V and, as a result, restrict blood flow through less compressible vessels V, while also applying a desired compressive pressure to surrounding tissue T. In many circumstances, in addition to above, the 10020 Fabric Thickness Compensator can also compensate for malformed staples. Referring to Figure 45, malformation of multiple staples 10030 can result in larger staple entrapment areas 10039 being defined within such staples. Due to the resilience of the fabric thickness compensator 10020, now referring to Figure 46, the fabric thickness compensator 10020 positioned within malformed staples 10030 can still apply sufficient compressive pressure to the fabric T even though the staple entrapment areas 10039 defined within such malformed clamps 10030 can be enlarged. In various circumstances, tissue thickness compensator 10020 located between adjacent staples 10030 may be pulled against tissue T by appropriately formed staples 10030 encircling a malformed staple 10030 and, as a result, apply compressive pressure to the surrounding and/or captured tissue. inside the malformed clamp 10030, for example. In various circumstances, a tissue thickness compensator can compensate for different tissue densities that may arise due to calcifications, fibrous areas, and/or tissue that has been previously stapled or treated, for example.

[000326] In accordance with the invention, a fixed, or immutable, tissue gap can be defined between the support portion and the anvil and, as a result, the clamps can be deformed to a predetermined height regardless of the thickness of the tissue captured within. of the staples. When a tissue thickness compensator is used in such cases, the tissue thickness compensator can adapt to the tissue captured between the anvil and staple cartridge of the support portion and, due to the resilience of the tissue thickness compensator, the Fabric thickness compensator can apply additional compressive pressure to the fabric. Now referring to Figures 50 to 55, a staple 10030 has been formed to a predefined height H. Referring to Figure 50, a fabric thickness compensator has not been used and the fabric T consumes the entire staple gripping area 10039 Referring to Figure 57, a portion of a fabric thickness compensator 10020 was captured by staple 10030, compressed fabric T, and consumed at least a portion of staple gripping area 10039. Now referring to Figure 52, thin tissue T was captured by clip 10030. In this embodiment, the compressed fabric T has a height of approximately 2/9H and the compressed fabric thickness compensator 10020 has a height of approximately 7/9H, for example. Referring now to Figure 53, fabric T with an intermediate thickness has been captured by clamp 10030. In this embodiment, the compressed fabric T has a height of approximately 4/9H and the compressed fabric thickness compensator 10020 has a height of approximately 5 /9H, for example. Referring now to Figure 54, fabric T with an intermediate thickness has been captured by clamp 10030. In this embodiment, the compressed fabric T has a height of approximately 2/3H and the compressed fabric thickness compensator 10020 has a height of approximately 1 /3H, for example. Referring now to Figure 53, thick tissue T has been captured by staple 10030. In this embodiment, the compressed tissue T has a height of approximately 8/9H and the compressed tissue thickness compensator 10020 has a height of approximately 1/9H, for example. In various circumstances, the fabric thickness compensator may comprise a compressed height comprising approximately 10% of the staple gripping height, approximately 20% of the staple gripping height, approximately 30% of the staple gripping height, approximately 40% of the staple gripping height, approximately 50% of the staple gripping height, approximately 60% of the staple gripping height, approximately 70% of the staple gripping height, approximately 80% of the staple gripping height, and/or approximately 90% of the clamp grip height, for example.

[000327] Clamps 10030 may comprise any suitable unformed height. Clips 10030 may comprise an unformed height of between approximately 2 mm and approximately 4.8 mm, for example. Clips 10030 may comprise an unformed height of approximately 2.0 mm, approximately 2.5 mm, approximately 3.0 mm, approximately 3.4 mm, approximately 3.5 mm, approximately 3.8 mm, approximately 4.0 mm. mm, approximately 4.1 mm, and/or approximately 4.8 mm, for example. The height H at which the clamps can be deformed can be determined by the distance between the platform surface 10011 of the support portion 10010 and the opposing anvil. The distance between the platform surface 10011 and the tissue contacting surface of the anvil can be approximately 2.5 mm (0.097"), for example. The height H can also be determined by the depth of the forming pockets defined inside the anvil The forming pockets may have a depth measured from the tissue-contacting surface, for example. Optionally, as described in more detail below, the staple cartridge 10000 may further comprise staple drivers that can lift the staples 10030 into towards the anvil and lifting or "excessively moving" the clamps above the platform surface 10011. In such cases, the height H at which the clamps 10030 are formed can also be determined by the distance at which the clamps 10030 are excessively directed. For example, staples 10030 can be moved further by approximately 0.71 mm (0.028"), for example, and can result in staples 10030 being formed at a height of approximately 4.80 mm (0.189"), for example. Clips 10030 can be formed to a height of approximately 0.8 mm, approximately 1.0 mm, approximately 1.5 mm, approximately 1.8 mm, approximately 2.0 mm, and/or approximately 2.25 mm, for example. Clips can be formed to a height between approximately 2.25 mm and approximately 3.0 mm, for example. In addition to the above, the height of the staple gripping area of a staple can be determined by the formed height of the staple and the width, or diameter, of the wire comprising the staple. The height of the staple gripping area 10039 of a staple 10030 may comprise the formed height H of the staple minus two wire diameter widths. The staple wire may comprise a diameter of approximately 0.2261 mm (0.0089"), for example. The staple wire may comprise a diameter of between approximately 0.1753 mm (0.0069") and approximately 0.3023 mm (0.0119"), for example. For example, the formed height H of a 10030 clamp may be approximately 4.80 mm (0.189") and the wire diameter of the clamp may be approximately 0.23 mm ( 0.0089") resulting in a clamp grip height of approximately 4.34 mm (0.171"), for example.

[000328] In addition to the above, the fabric thickness compensator may comprise an uncompressed, or pre-dispensed height, and may be configured to deform to one of a plurality of compressed heights. The fabric thickness compensator may comprise an uncompressed height of approximately 3.18 mm (0.125"), for example. The fabric thickness compensator may comprise an uncompressed height greater than or equal to approximately 2.032 mm (0.080 "), for example. The fabric thickness compensator may comprise an uncompressed, or pre-dispensed, height that is greater than the unfired height of the staples. The uncompressed, or pre-dispensed, height of the fabric thickness compensator can be approximately 10% higher, approximately 20% higher, approximately 40% higher, approximately 60% higher, approximately 80% higher, approximately 30 % higher, approximately 50% higher, approximately 70% higher, approximately 90% higher, and/or approximately 100% higher than the unfired height of the staples, for example. The uncompressed, or pre-dispensed, height of the fabric thickness compensator can be up to approximately 100% higher than the unfired height of the staples, for example. The uncompressed, or pre-released height of the fabric thickness compensator can be more than 100% higher than the unfired height of the staples, for example. The fabric thickness compensator may comprise an uncompressed height which is equal to the unfired height of the staples. The fabric thickness compensator may comprise an uncompressed height that is less than the unfired height of the staples. The uncompressed, or pre-dispensed height of the thickness compensator can be approximately 10% shorter, approximately 20% shorter, approximately 30% shorter, approximately 40% shorter, approximately 50% shorter, approximately 60% shorter , approximately 70% shorter, approximately 80% shorter, and/or approximately 90% shorter than the unfired height of the staples, for example. The second compressible portion may comprise an uncompressed height which is higher than an uncompressed height of the fabric T being stapled. The fabric thickness compensator may comprise an uncompressed height which is equal to an uncompressed height of the fabric T being stapled. The fabric thickness compensator may comprise an uncompressed height that is shorter than an uncompressed height of the fabric T being stapled.

[000329] As described above, a fabric thickness compensator can be compressed within a plurality of formed staples, regardless of whether thick tissue or thin tissue is captured within the staples. For example, staples within a row, or row, of staples can be deformed so that the staple gripping area of each staple comprises a height of approximately 2.0 mm, for example, where the T fabric and the Fabric thickness compensator can be compressed within this height. Under certain circumstances, the fabric T may comprise a pinch height of approximately 1.75mm within the staple gripping area while the fabric thickness compensator may comprise a pinch height of approximately 0.25mm within the staple gripping area , thus totaling the height of the clamp gripping area of approximately 2.0 mm, for example. Under certain circumstances, the fabric T may comprise a pinch height of approximately 1.50mm within the staple gripping area while the fabric thickness compensator may comprise a pinch height of approximately 0.50mm within the staple gripping area. , thus totaling the height of the clamp gripping area of approximately 2.0 mm, for example. Under certain circumstances, the fabric T may comprise a pinch height of approximately 1.25mm within the staple gripping area while the fabric thickness compensator may comprise a pinch height of approximately 0.75mm within the staple gripping area , thus totaling the height of the clamp gripping area of approximately 2.0 mm, for example. Under certain circumstances, the fabric T may comprise a pinch height of approximately 1.0 mm within the staple gripping area while the fabric thickness compensator may comprise a pinch height of approximately 1.0 mm within the staple gripping area , thus totaling the height of the clamp gripping area of approximately 2.0 mm, for example. Under certain circumstances, the fabric T may comprise a pinch height of approximately 0.75mm within the staple gripping area while the fabric thickness compensator may comprise a pinch height of approximately 1.25mm within the staple gripping area , thus totaling the height of the clamp gripping area of approximately 2.0 mm, for example. Under certain circumstances, the fabric T may comprise a pinch height of approximately 1.50 mm within the staple gripping area while the fabric thickness compensator may comprise a pinch height of approximately 0.50 mm within the gripping area. of staple, thus totaling the height of the staple gripping area of approximately 2.0 mm, for example. Under certain circumstances, the fabric T may comprise a pinch height of approximately 0.25mm within the staple gripping area while the fabric thickness compensator may comprise a pinch height of approximately 1.75mm within the staple gripping area , thus totaling the height of the clamp gripping area of approximately 2.0 mm, for example.

[000330] In addition to the above, the fabric thickness compensator may comprise an uncompressed height that is less than the height fired from the staples. The fabric thickness compensator may comprise an uncompressed height which is equal to the fired height of the staples. The fabric thickness compensator may comprise an uncompressed height that is greater than the height fired from the staples. For example, the uncompressed height of a fabric thickness compensator may comprise a thickness that is approximately 110% of the height of the formed staple, approximately 120% of the formed staple height, approximately 130% of the formed staple height, approximately 140% of the formed clamp height, approximately 150% of the formed clamp height, approximately 160% of the formed clamp height, approximately 170% of the formed clamp height, approximately 180% of the formed clamp height, approximately 190% of the formed clamp height, and/or approximately 200% of the height of the formed clip, for example. The fabric thickness compensator may comprise an uncompressed height which is more than twice the height fired from the staples. The fabric thickness compensator may comprise a compressed height that is from approximately 85% to approximately 150% of the height of the formed staple, for example. Optionally, as described above, the fabric thickness compensator can be compressed between an uncompressed thickness and a compressed thickness. The compressed thickness of a fabric thickness compensator can be approximately 10% of its uncompressed thickness, approximately 20% of its uncompressed thickness, approximately 30% of its uncompressed thickness, approximately 40% of its uncompressed thickness, approximately 50 % of its uncompressed thickness, approximately 60% of its uncompressed thickness, approximately 70% of its uncompressed thickness, approximately 80% of its uncompressed thickness, and/or approximately 90% of its uncompressed thickness, for example . The uncompressed thickness of the fabric thickness compensator can be approximately twice, approximately ten times, approximately fifty times, and/or approximately one hundred times thicker than its compressed thickness, for example. The compressed thickness of the fabric thickness compensator can be between approximately 60% and approximately 99% of its uncompressed thickness. The uncompressed thickness of the fabric thickness compensator can be at least 50% thicker than its compressed thickness. The uncompressed thickness of the fabric thickness compensator can be up to one hundred times thicker than its compressed thickness. The second compressible portion can be elastic, or at least partially elastic, and can pull the T-fabric against the deformed legs of the staples. For example, the second compressible portion can resiliently expand between the T fabric and the base of the staple so as to push the T fabric against the staple legs. As discussed in more detail below, the fabric thickness compensator can be positioned between the fabric T and the deformed clamp legs. In various circumstances, as a result of the above, the fabric thickness compensator can be configured to consume any gaps within the staple gripping area.

[000331] The tissue thickness compensator may comprise materials characterized by one or more of the following properties: biocompatible, bioabsorbable, bioresorbable, biodurable, biodegradable, compressible, fluid absorbable, dilatable, self-expanding, bioactive, drug, pharmaceutically active, anti-adhesion, hemostatic , antibiotic, antimicrobial, antiviral, nutritional, adhesive, permeable, hydrophilic and/or hydrophobic, for example. In accordance with the invention, a surgical instrument comprising an anvil and a staple cartridge may comprise a tissue thickness compensator associated with the anvil and/or staple cartridge comprising at least one of a hemostatic agent, such as fibrin and thrombus. - na, an antibiotic, such as doxicpl, and a drug, such as matrix metalloproteinases (MMPs).

[000332] The fabric thickness compensator may comprise synthetic and/or non-synthetic materials. The fabric thickness compensator may comprise a polymeric composition comprising one or more synthetic polymers and/or one or more non-synthetic polymers. The synthetic polymer may comprise an absorbable synthetic polymer and/or a non-absorbable synthetic polymer. The polymeric composition may comprise a biocompatible foam, for example. The biocompatible foam may comprise a porous open cell foam and/or a porous closed cell foam, for example. The biocompatible foam may have a uniform pore morphology or it may have a gradient pore morphology (i.e., small pores that gradually increase in size to large pores across the thickness of the foam in one direction). The polymeric composition may comprise one or more of a porous scaffold, a porous matrix, a gel matrix, a hydrogel matrix, a solution matrix, a filamentous matrix, a tubular matrix, a composite matrix, a membranous matrix, a biostable polymer, and a bio-degradable polymer, and combinations thereof. For example, the fabric thickness compensator may comprise a foam reinforced by a filamentous matrix, or it may comprise a foam that has an additional hydrogel layer that expands in the presence of body fluids to provide further compression on the fabric. In accordance with the invention, a fabric thickness compensator could also be comprised of a coating over a material and/or a second or third layer that expands in the presence of body fluids to provide even more compression on the fabric. Such a layer could be a hydrogel which could be a synthetic and/or naturally derived material and could be biodurable and/or biodegradable, for example. The tissue thickness compensator may comprise a microgel or a nanogel. The hydrogel may comprise carbohydrate-derived microgels and/or nanogels. A fabric thickness compensator may be reinforced with fibrous non-woven materials or fibrous mesh-like elements, for example, which can provide additional flexibility, rigidity, and/or strength. According to the invention, a fabric thickness compensator having a porous morphology that exhibits a gradient structure, for example small pores on one surface and larger pores on the other surface. Such morphology could be better for tissue ingrowth or hemostatic behavior. Additionally, the gradient could also be compositional with a different bioabsorption profile. A short-term absorption profile may be preferred to handle hemostasis while a long-term absorption profile may better handle tissue healing without leakage.

[000333] Examples of non-synthetic materials include, but are not limited to, lyophilized polysaccharide, glycoprotein, bovine pericardium, collagen, gelatin, fibrin, fibrinogen, elastin, proteoglycan, keratin, albumin, hydroxyethylcellulose, cellulose, oxidized cellulose, cellulose oxidized regenerate (ORC), hydroxypropyl cellulose, carboxyethyl cellulose, carboxymethyl cellulose, chitan, chitosan, casein, alginate and combinations thereof.

[000334] Examples of synthetic absorbable materials include, but are not limited to, poly(lactic acid) (PLA), poly(L-lactic acid) (PLLA), polycaprolactone (PCL), poly(glycolic acid) (PGA), poly(trimethylene carbonate) (TMC), poly(ethylene terephthalate) (PET), poly(hydroxyalkanoate) (PHA), a copolymer of glycolide and ε-caprolactone (PGCL), a copolymer of glycolide and tricarbonate - methylene, poly(glycerol sebacate) (PGS), poly(dioxanone) (PDS), polyesters, poly(orthoesters), poly(oxaesters), poly(ether-esters), polycarbonates, polyamide esters, polyanhydrides, polysaccharides, poly(ester amides), tyrosine-based polyarylates, polyamines, tyrosine-based poly(iminocarbonates), tyrosine-based polycarbonates, poly(D,L-lactide-urethane), poly (hydroxybutyrate), poly(B-hydroxybutyrate), poly(E-caprolactone), poly(ethylene glycol) (PEG), poly[bis(carboxylatephenoxy) phosphazene] poly(amino acids), pseudopoly(amino acids), polyurethanes absorbable, poly(phosphazine), polyphosphazenes, poly(alkylene oxides), polyacrylamides, poly(hydroxyethyl methacrylate), polyvinylpyrrolidone, poly(vinyl alcohols), poly(caprolactone), poly(acrylic acid), polyacetate, polypropylene, aliphatic polyesters, glycerols, copoly(ether esters), poly(alkylene oxalates), polyamides, poly(iminocarbonates), poly(alkylene oxalates) and combinations thereof. The polyester may be selected from the group consisting of polylactides, polyglycolides, trimethylene carbonates, polydioxanones, polycaprolactones, polybutesters and combinations thereof.

[000335] The synthetic absorbable polymer may comprise one or more of a 90/10 poly(glycolide-L-lactide) copolymer, commercially available from Ethicon, Inc. under the tradename VICRYL (poliglactic 910), polyglycolide, commercially available from American Cyanamid Co. under the tradename DEXON, polydioxanone, commercially available from Ethicon, Inc. under the tradename PDS, poly(glycolide-trimethylene carbonate) random block copolymer, commercially available from American Cyanamid Co. under the tradename MAXON, 75/25 poly(glycolide-and-caprolactone-polyglecaprolactone 25) copolymer, commercially available from Ethicon under the tradename MONO-CRYL, for example.

[000336] Examples of synthetic non-absorbable materials include, but are not limited to, foamed polyurethane, polypropylene (PP), polyethylene (PE), polycarbonate, polyamides such as nylon, poly(vinyl chloride) (PVC) , poly(methyl methacrylate) (PMMA), polystyrene (PS), polyester, poly(ether ether ketone) (PEEK), poly(tetrafluoroethylene) (PTFE), poly(trifluorochloroethylene) (PTFCE), poly(vinyl fluoride) (PVF), fluorinated ethylene propylene (FEP), polyacetal, polysulfone, silicones and combinations thereof. Synthetic non-absorbable polymers can include, but are not limited to, foamed elastomers and porous elastomers, such as, for example, silicone, polyisoprene, and rubber. Synthetic polymers may comprise expanded poly(tetrafluoroethylene) (ePTFE), commercially available from W. L. Gore & Associates, Inc. under the tradename GORE-TEX Soft Woven Patch and co-poly(ether-ester-urethane) foam commercially available from Polyganics under the tradename NASOPORE.

[000337] The polymeric composition may comprise from approximately 50% to approximately 90% by weight of the polymeric composition of PLLA and approximately 50% to approximately 10% by weight of the polymeric composition of PCL, for example. The polymeric composition may comprise approximately 70% by weight of PLLA and approximately 30% by weight of PCL, for example. The polymeric composition may comprise from approximately 55% to approximately 85% by weight of the PGA polymeric composition and 15% to 45% by weight of the PCL polymeric composition, for example. The polymeric composition may comprise approximately 65% by weight of PGA and approximately 35% by weight of PCL, for example. The polymeric composition may comprise from approximately 90% to approximately 95% by weight of the PGA polymeric composition and approximately 5% to approximately 10% by weight of the PLA polymeric composition, for example.

[000338] The synthetic absorbable polymer may comprise a bioabsorbable biocompatible elastomeric copolymer. Suitable bioabsorbable biocompatible elastomeric copolymers include, but are not limited to, copolymers of ecaprolactone and glycolide (preferably having a molar ratio of e-caprolactone to glycolide of from about 30:70 to about 70:30, preferably 35:65 to about 65:35, and more preferably 45:55 to 35:65); elastomeric copolymers of e-caprolactone and lactide, including L-lactide, D-lactide and mixtures thereof, or lactide copolymers (preferably having a molar ratio of e-caprolactone to lactide of about 35:65 to about 65:35 and more preferably 45:55 to 30:70), elastomeric copolymers of p-dioxanone (1,4-dioxan-2-one) and lactide including L-lactide, D-lactide and lactic acid (preferably having a molar ratio of p-dioxanone to lactide of from about 40:60 to about 60:40); elastomeric copolymers of e-caprolactone and p-dioxanone (preferably having an e-caprolactone to p-dioxanone molar ratio of from about 30:70 to about 70:30); elastomeric copolymers of p-dioxanone and trimethylene carbonate (preferably having a molar ratio of p-dioxanone to trimethylene carbonate of about 30:70 about 70:30); elastomeric copolymers of trimethylene carbonate and glycolide (preferably having a molar ratio of trimethylene carbonate to glycolide of from about 30:70 to about 70:30); elastomeric copolymer of trimethylene carbonate and lactide including L-lactide, D-lactide, mixtures thereof or lactide copolymers (preferably having a molar ratio of trimethylene carbonate to lactide of from about 30:70 to about 70 :30) and mixtures thereof. The elastomeric copolymer may be a copolymer of glycolide and e-caprolactone. Alternatively, the elastomeric copolymer is a copolymer of lactide and e-caprolactone.

[000339] The disclosures of US Patent No. 5,468,253 entitled ELASTOMERIC MEDICAL DEVICE, which was issued November 21, 1995, and US Patent No. 6,325,810 entitled FOAM BUT-TRESS FOR STAPLING APPARATUS, which was granted December 4, 2001, are incorporated herein by reference in their entirety.

[000340] The fabric thickness compensator may comprise an emulsifier. Examples of emulsifiers may include, but are not limited to, water-soluble polymers such as poly(vinyl alcohol) (PVA), polyvinylpyrrolidone (PVP), poly(ethylene glycol) (PEG), poly(propylene glycol) (PPG), PLURONICS, TWEENS, polysaccharides and combinations thereof.

[000341] The fabric thickness compensator may comprise a surfactant.

[000342] Examples of surfactants may include, but are not limited to, poly(acrylic acid), metallose, methylcellulose, ethylcellulose, propylcellulose, hydroxyethylcellulose, carboxymethylcellulose, polyoxyethylene cetyl ether, polyoxyethylene lauryl ether, polyoxyethylene octyl ether. polyoxyethylene, polyoxyethylene octylphenyl ether, polyoxyethylene oleyl ether, polyoxyethylene sorbitan monolaurate, polyoxyethylene stearyl ether, polyoxyethylene nonyl phenyl ether, poly(ethyleneoxy) ethanol dialkylphenoxy and poloxamers.

[000343] The polymeric composition may comprise a pharmaceutically active agent. The polymeric composition can release a therapeutically effective amount of the pharmaceutically active agent. The pharmaceutically active agent can be released when the polymeric composition is desorbed/absorbed. The pharmaceutically active agent may be released into the fluid, for example blood, which passes over or through the polymeric composition. Examples of pharmaceutically active agents may include, but are not limited to, hemostatic agents and drugs, such as, for example, fibrin, thrombin, and oxidized regenerated cellulose (ORC); anti-inflammatory drugs, such as diclofenac, aspirin, naxoprene, subidac and hydrocortisone; antibiotic and antimicrobial drug or agents such as, for example, triclosan, ionic silver, ampicillin, gentamicin, polymyxin B, chloramphenicol; and anti-cancer agents such as, for example, cisplatin, mitomycin, adriamycin.

[000344] The polymeric composition may comprise a hemostatic material. The tissue thickness compensator may comprise hemostatic materials comprising poly(lactic acid), poly(glycolic acid), poly(hydroxybutyrate), poly(caprolactone), poly(dioxanone), poly(alkylene oxides), co-poly(ether esters), collagen, gelatin, thrombin, fibrin, fibrinogen, fibronectin, elastin, albumin, hemoglobin, ovalbumin, polysaccharides, hyaluronic acid, chondroitin sulfate, hydroxyethyl starch, hydroxyethylcellulose, cellulose, oxidized cellulose, hydroxypropylcellulose , carboxyethylcellulose, carboxymethylcellulose, chitan, chitosan, agarose, maltose, maltodextrin, alginate, clotting factors, methacrylate, polyurethanes, cyanoacrylates, platelet agonists, vasoconstrictors, alum, calcium, RGD peptides, proteins, protamine sulfate , e-amino caproic acid, ferric sulfate, ferric subsulfates, ferric chloride, zinc, zinc chloride, aluminum chloride, aluminum sulfates, aluminum acetates, permanganates, tannins, wax and bone, poly(ethylene glycols), fucans and combinations thereof. The tissue thickness compensator can be characterized by hemostatic properties.

[000345] The polymeric composition of a fabric thickness compensator can be characterized by the percentage of porosity, pore size, and/or hardness, for example. The polymeric composition may have a porosity percentage from approximately 30% by volume to approximately 99% by volume, for example. The polymeric composition may have a porosity percentage from approximately 60% by volume to approximately 98% by volume, for example. The polymeric composition may have a porosity percentage of approximately 85% by volume to approximately 97% by volume, for example. The polymeric composition may comprise approximately 70% by weight of PLLA and approximately 30% by weight of PCL, for example, and may comprise porosity of approximately 90% by volume, for example. For example, as a result, the polymeric composition would comprise approximately 10% copolymer by volume. The polymer composition may comprise approximately 65% by weight of PGA and approximately 35% by weight of PCL, for example, and may have a porosity percentage of approximately 93% by volume to approximately 95%, in volume, for example. The polymeric composition may comprise a porosity greater than 85% by volume. The polymeric composition may have a pore size of from approximately 5 micrometers to approximately 2000 micrometers, for example. The polymeric composition may have a pore size between approximately 10 micrometers and approximately 100 micrometers, for example. For example, the polymeric composition may comprise a copolymer of PGA and PCL, for example. The polymeric composition may have a pore size between approximately 100 micrometers and approximately 1000 micrometers, for example. For example, the polymeric composition may comprise a copolymer of PLLA and PCL, for example.

[000346] According to certain aspects, the hardness of a polymeric composition can be expressed in terms of Shore hardness, which can be defined as the permanent indentation resistance of a material, as determined with a durometer, such as a Shore durometer. . In order to assess the durometer value for a given material, pressure is applied to the material with a durometer indenter foot according to ASTM procedure D2240-00 entitled, "Standard Test Method for Rubber Property-Durometer Hardness", which is fully incorporated herein by reference. The durometer's indenter foot can be applied to the material for a sufficient period of time, such as 15 seconds for example, at which time a reading is then taken at the proper scale. Depending on the type of scale used, a reading of 0 may be obtained when the indenter foot completely penetrates the material, and a reading of 100 may be obtained when no penetration occurs in the material. This reading is dimensionless. The durometer can be determined according to any suitable scale, such as type A and/or type OO scales, for example according to ASTM D2240-00. The polymer composition of a fabric thickness compensator may have a Shore A hardness value of approximately 4 A to approximately 16 A, for example, which is approximately 45 OO to approximately 65 OO in the Shore OO range. For example, the polymeric composition may comprise a PLLA/PCL copolymer or a PGA/PCL copolymer, for example. The polymer composition of a fabric thickness compensator may have a Shore A hardness value of less than 15 A. In various embodiments, the polymer composition of a fabric thickness compensator may have a Shore A hardness value of less than 10 A. The polymeric composition of a fabric thickness compensator may have a Shore A hardness value of less than 5 A. In certain embodiments, the polymeric material may have a Shore OO composition value of approximately 3500 to approximately 7500, for example.

[000347] The polymeric composition may have at least two of the properties identified above. The polymeric composition can have at least three of the properties identified above. The polymer composition may have a porosity of 85% to 97% by volume, a pore size of 5 micrometers to 2000 micrometers, and a Shore A hardness value of 4 A to 16 A and a Shore OO hardness value of 45 OO to 65 OO, for example. The polymeric composition may comprise 70% by weight of the polymeric composition of PLLA and 30% by weight of the polymeric composition of PCL having a porosity of 90% by volume, a pore size of 100 micrometers to 1000 micrometers. , and a Shore A hardness value of 4 A to 16 A and a Shore OO hardness value of 45 OO to 65 OO, for example. The polymeric composition may comprise 65% by weight of the PGA polymeric composition and 35% by weight of the PCL polymeric composition having a porosity of 93% to 95% by volume, a pore size of 10 micrometers. to 100 micrometers, and a Shore A hardness value of 4 A to 16 A and a Shore OO hardness value of 45 OO to 65 OO, for example.

[000348] The fabric thickness compensator may comprise an expandable material. As discussed above, the fabric thickness compensator may comprise a compacted material that expands when not compacted or installed, for example. The fabric thickness compensator may comprise a self-expanding material formed in situ. The tissue thickness compensator may comprise at least one precursor selected to spontaneously cross-link when brought into contact with at least one of the other precursor(s), water and/or body fluids. Referring to Figure 205, a first precursor may contact one or more other precursors to form an expandable and/or expandable tissue thickness compensator. The fabric thickness compensator may comprise a fluid swellable composition, such as a water swellable composition, for example. The fabric thickness compensator may comprise a gel comprising water.

[000349] Referring to Figures 189A and B, for example, a tissue thickness compensator 70000 may comprise at least one hydrogel precursor 70010 selected to form a hydrogel in situ and/or in vivo to expand the tissue thickness compensator 70,000. Figure 189A illustrates a fabric thickness compensator 70,000 comprising an encapsulation comprising a first hydrogel precursor 70010A and a second hydrogel precursor 70010B prior to expansion. As shown in Figure 189A, the first hydrogel precursor 70010A and the second hydrogel precursor 70010B can be physically separated from each other in the same encapsulation. A first encapsulation may comprise first hydrogel precursor 70010A and a second encapsulation may comprise second hydrogel precursor 70010B. Figure 189B illustrates the expansion of tissue thickness compensator 70000 when the hydrogel is formed in situ and/or in vivo. As shown in Figure 189B, the encapsulation may be disrupted and the first hydrogel precursor 70010A may contact the second hydrogel precursor 70010B to form the hydrogel 70020. The hydrogel may comprise an expandable material. The hydrogel can expand for up to 72 hours, for example.

[000350] The fabric thickness compensator may comprise a biodegradable foam which has an encapsulation comprising dry hydrogel particles or granules incorporated therein. Without being bound by any theory, encapsulations in foam can be formed by contacting an aqueous solution of a hydrogel precursor and an organic solution of biocompatible materials to form the foam. As shown in Figure 206, the aqueous solution and the organic solution can form micelles. The aqueous solution and the organic solution can be dried to encapsulate dry hydrogel particles or granules in the foam. For example, a hydrogel precursor, such as a hydrophilic polymer, can be dissolved in water to form a micelle dispersion. The aqueous solution may be contacted with an organic dioxane solution comprising poly(glycolic acid) and polycaprolactone. The aqueous and organic solutions can be lyophilized to form a biodegradable foam which has dry hydrogel particles or granules dispersed therein. Without being bound by any theory, it is believed that the micelles form the encapsulation which has the dry hydrogel particles or granules dispersed in the foam structure. The encapsulation can be broken and the dry hydrogel particles or granules can come into contact with a fluid, such as a body fluid, and expand.

[000351] The tissue thickness compensator may expand when it comes in contact with an activator such as a fluid for example. Referring to Figure 190, for example, a tissue thickness compensator 70050 may comprise a swellable material, such as a hydrogel, that expands when it comes into contact with a fluid 70055, such as body fluids, saline, water, and/or a activator, for example. Examples of bodily fluids may include, but are not limited to, blood, plasma, peritoneal fluid, cerebrospinal fluid, urine, lymphatic fluid, synovial fluid, vitreous fluid, saliva, gastrointestinal luminal contents, bile and/or gas (e.g. , CO2). The 70050 Fabric Thickness Compensator can expand when the 70050 Fabric Thickness Compensator absorbs fluid. In another example, the fabric thickness compensator 70050 may comprise a non-crosslinked hydrogel that expands when contacted with an activator 70055 comprising a crosslinking agent to form a crosslinked hydrogel. The fabric thickness compensator may expand when it comes in contact with an activator. Fabric Thickness Compensator can expand or dilate from contact for up to 72 hours, such as 24-72 hours, up to 24 hours, up to 48 hours, and up to 72 hours, for example, to provide continuously increasing pressure and/or compression to the fabric. As shown in Figure 190, the initial thickness of the fabric thickness compensator 70050 may be less than an expanded thickness after fluid 70055 contacts the fabric thickness compensator 70050.

[000352] Referring to Figures 187 and 188a, the staple cartridge 70100 may comprise a fabric thickness compensator 70105 and a plurality of staples 70110, each comprising staple legs 70112. As shown in Figure 187, the compensator 70105 Tissue Thickness Compensator can have an initial thickness or packed height that is less than the triggered height of the 70110 staples. The 70100 Tissue Thickness Compensator can be configured to expand in situ and/or in vivo upon contact. with a fluid 70102, such as body fluids, saline, and/or an activator, for example, to push the tissue T against the legs 70112 of the clamp 70110. As shown in Figure 188, the tissue thickness compensator 70100 can expand and/or swell when in contact with a 70102 fluid. The 70105 tissue thickness compensator can compensate for the thickness of tissue T captured by each 70110 staple. As shown in Figure 188, the Tissue Thickness Compensator Fabric thicknesser 70105 can have an expanded thickness or an uncompressed height that is less than the shot height of the 70110 staples.

[000353] Optionally, as described above, the fabric thickness compensator may comprise an initial thickness and an expanded thickness. The initial thickness of a fabric thickness compensator can be approximately 0.001% of its expanded thickness, approximately 0.01% of its expanded thickness, approximately 0.1% of its expanded thickness, approximately 1% of its expanded thickness , approximately 10% of its expanded thickness, approximately 20% of its expanded thickness, approximately 30% of its expanded thickness, approximately 40% of its expanded thickness, approximately 50% of its expanded thickness, approximately 60% of its expanded thickness , approximately 70% of its expanded thickness, approximately 80% of its expanded thickness and/or approximately 90% of its expanded thickness, for example. The expanded thickness of the fabric thickness compensator can be approximately twice, approximately five times, approximately ten times, approximately fifty times, approximately one hundred times, approximately two hundred times, approximately three hundred times, approximately four hundred times, approximately five hundred times, approximately six hundred times , approximately seven hundred times, approximately eight hundred times, approximately nine hundred times and/or approximately one thousand times thicker than its initial thickness, for example. The initial thickness of the fabric thickness compensator can be up to 1% of its expanded thickness, up to 5% of its expanded thickness, up to 10% of its expanded thickness, and up to 50% of its expanded thickness. The expanded thickness of the fabric thickness compensator can be at least 50% thicker than its initial thickness, at least 100% thicker than its initial thickness, at least 300% thicker than its initial thickness, and at least 500 % thicker than its initial thickness. As described above, in various circumstances, as a result of the above, the fabric thickness compensator may be configured to consume any gap within the staple gripping area.

[000354] As discussed above, the fabric thickness compensator may comprise a hydrogel. The hydrogel may comprise homopolymer hydrogels, copolymer hydrogels, multipolymer hydrogels, interpenetrating polymer hydrogels and combinations thereof. The hydrogel may comprise microgels, nanogels and combinations thereof. The hydrogel may generally comprise a hydrophilic polymer network that has the ability to absorb and/or retain fluids. The hydrogel may comprise a non-crosslinked hydrogel, a crosslinked hydrogel and combinations thereof. The hydrogel may comprise chemical crosslinks, physical crosslinks, hydrophobic segments and/or water-insoluble segments. The hydrogel can be chemically cross-linked via polymerization, small-molecule cross-linking, and/or polymer-polymer cross-linking. The hydrogel can be physically cross-linked through ionic interactions, hydrophobic interactions, hydrogen bonding interactions, stereocomplexation and/or supramolecular chemistry. The hydrogel may be substantially insoluble due to crosslinks, hydrophobic segments and/or water-insoluble segments, but may be expandable and/or dilatable due to fluid absorption and/or retention. The precursor may cross-link with endogenous materials and/or tissues.

[000355] The hydrogel may comprise an environmentally sensitive hydrogel (ESH). The ESH may comprise materials that have fluid expansion properties related to environmental conditions. Environmental conditions may include, but are not limited to, the physical conditions, biological conditions, and/or chemical conditions at the surgical site. The hydrogel can swell or shrink in response to temperature, pH, electric fields, ionic resistance, enzymatic and/or chemical reactions, electrical and/or magnetic stimuli, and other physiological and environmental variables, for example. ESH can comprise multifunctional acrylates, hydroxyethyl methacrylate (HEMA), elastomeric acrylates and related monomers.

[000356] The fabric thickness compensator comprising a hydrogel may comprise at least one of the non-synthetic materials and synthetic materials described above. The hydrogel may comprise a synthetic hydrogel and/or a non-synthetic hydrogel. The fabric thickness compensator may comprise a plurality of layers. The plurality of layers may comprise porous layers and/or non-porous layers. For example, the fabric thickness compensator may comprise a non-porous layer and a porous layer. In another example, the fabric thickness compensator may comprise a porous layer intermediate a non-porous first layer and a non-porous second layer. In another example, the fabric thickness compensator may comprise a non-porous layer intermediate a porous first layer and a porous second layer. The non-porous layers and the porous layers may be positioned in any order with respect to the surfaces of the staple cartridge and/or anvil.

[000357] Examples of the non-synthetic material may include, but are not limited to, albumin, alginate, carbohydrate, casein, cellulose, chitin, chitosan, collagen, blood, dextran, elastin, fibrin, fibrinogen, gelatin, heparin, hyaluronic acid, keratin, protein, whey and starch. The cellulose may comprise hydroxyethyl cellulose, oxidized cellulose, oxidized regenerated cellulose (ORC), hydroxypropyl cellulose, carboxyethyl cellulose, carboxymethyl cellulose and combinations thereof. Collagen may comprise bovine pericardium. The carbohydrate may comprise a polysaccharide, such as lyophilized polysaccharide. The protein may comprise glycoprotein, proteoglycan and combinations thereof.

[000358] Examples of the synthetic material may include, but are not limited to, poly(lactic acid), poly(glycolic acid), poly(hydroxybutyrate), poly(phosphazine), polyesters, poly(ethylene glycols), poly( ethylene), poly(ethylene oxide)-co-poly(propylene oxide), co-poly(ethylene oxide), poly(alkylene oxides), polyacrylamides, poly(hydroxyethyl methacrylate), polyvinylpyrrolidone, poly(vinyl alcohols), poly(caprolactone), poly(dioxanone), poly(acrylic acid), polyacetate, polypropylene, aliphatic polyesters, glycerols, poly(amino acids), co-poly(ether esters), poly (alkylene oxalates), polyamides, poly(iminocarbonates), poly(oxaesters), poly(orthoesters), polyphosphazenes and combinations thereof. The above non-synthetic materials can be synthetically prepared, for example synthetic hyaluronic acid, using conventional methods.

[000359] The hydrogel can be produced from one or more hydrogel precursors. The precursor may comprise a monomer and/or a macromer. The hydrogel precursor may comprise an electrophilic functional group and/or a nucleophilic electrophilic functional group. In general, electrophiles can react with nucleophiles to form a bond. The term "functional group" as used herein refers to electrophilic or nucleophilic groups that have the ability to react with each other to form a bond. Examples of electrophilic functional groups may include, but are not limited to, N-hydroxysuccinimides ("NHS"), sulfosuccinimides, carbonyldiimidazole, sulfonyl chloride, aryl halides, sulfosuccinimidyl esters, N-hydroxysuccinimidyl esters , succinimidyl esters such as succinimidyl succinates and/or succinimidyl propionates, isocyanates, thiocyanates, carbodiimides, benzotriazole carbonates, epoxides, aldehydes, maleimides, imidoesters, combinations thereof and the like. The electrophilic functional group may comprise a succinimidyl ester. Examples of nucleophilic functional groups may include, but are not limited to, -NH2 , -SH, -OH, -PH2 and -CO-NH-NH2 .

[000360] The hydrogel can be formed from a single precursor or from multiple precursors. The hydrogel can be formed from a first precursor and a second precursor. The first hydrogel precursor and the second hydrogel precursor can form a hydrogel in situ and/or in vivo upon contact. Hydrogel precursor can generally refer to a polymer, a functional group, a macromolecule, a small molecule and/or a crosslinker that can be part of a reaction to form a hydrogel. The precursor may comprise a homogeneous, heterogeneous solution or a separate phase solution in a suitable solvent, such as water or a buffer, for example. The buffer may have a pH of from about 8 to about 12, such as about 8.2 to about 9, for example. Examples of buffers may include, but are not limited to, borate buffers. The precursor(s) may be in an emulsion. In accordance with the invention, a first precursor can be reacted with a second precursor to form a hydrogel. The first precursor can spontaneously cross-link when brought into contact with the second precursor. In accordance with the invention, a first set of electrophilic functional groups on a first precursor may react with a second set of nucleophilic functional groups on a second precursor. When precursors are mixed in an environment that allows for the reaction (eg, with respect to pH, temperature, and/or solvent), the functional groups can react with each other to form covalent bonds. Precursors can become cross-linked when at least some of the precursors react with more than one other precursor.

[000361] The tissue thickness compensator may comprise at least one monomer selected from the group consisting of potassium salt of 3-sulfopropyl acrylate ("KSPA"), sodium acrylate ("NaA"), N-( tris(hydroxylmethyl)methyl)acrylamide ("tris acryl") and 2-acrylamido-2-methyl-1-propanesulfonic acid (AMPS). The fabric thickness compensator may comprise a copolymer comprising two or more monomers selected from the group consisting of KSPA, NaA, tris acryl, aMPS. The tissue thickness compensator may comprise homopolymers derived from KSPA, NaA, trisacryl and AMPS. The fabric thickness compensator may comprise hydrophilic capacity modifier monomers copolymerizable therewith. The hydrophilic capacity modifier monomers may comprise methyl methacrylate, butyl acrylate, cyclohexyl acrylate, styrene, styrene sulfonic acid.

[000362] The fabric thickness compensator may comprise a crosslinker. The crosslinker may comprise a low molecular weight di or polyvinyl crosslinking agent such as ethylene glycol diacrylate or dimethacrylate, di-, tri- or tetra(ethylene glycol) diacrylate or dimethacrylate, allyl (meth)acrylate , a C2-C8-alkylene diacrylate or dimethacrylate, divinyl ether, divinyl sulfone, di- and trivinylbenzene, trimethylolpropane triacrylate or trimethacrylate, pentaerythritol tetraacrylate or tetramethacrylate, bisphenol A, methylene bis diacrylate or dimethacrylate -acrylamide or bis-methacrylamide, ethylene-bis-acrylamide or ethylene-bis-methacrylamide, triallyl phthalate or diallyl phthalate. The cross-linker may comprise N,N'-methylene-bis-acrylamide ("MBAA").

[000363] The tissue thickness compensator may comprise at least one of acrylate and/or methacrylate functional hydrogels, biocompatible photoinitiator, alkylcyanoacrylates, isocyanate functional macromers, which optionally comprise amine functional macromers, succinimidyl ester functional macromers, which optionally comprise amine and/or sulfhydryl functional macromers, epoxy functional macromers, which optionally comprise amine functional macromers, mixtures of proteins and/or polypeptides and aldehyde crosslinkers, Genipin, and water-soluble carbodiimides, anionic polysaccharides and polyvalent cations.

[000364] The fabric thickness compensator may comprise unsaturated organic acid monomers, acrylic substituted alcohols and/or acrylamides. The fabric thickness compensator may comprise methacrylic acids, acrylic acids, glycerol acrylate, glycerol methacrylate, 2-hydroxyethyl methacrylate, 2-hydroxyethyl acrylate, 2-(dimethylaminoethyl) methacrylate, N-vinylpyrrolidone, methacrylamide and /or N,N-dimethylacrylamide poly(methacrylic acid).

[000365] The fabric thickness compensator may comprise a reinforcing material. The reinforcing material may comprise at least one of the non-synthetic materials and synthetic materials described above. The reinforcing material may comprise collagen, gelatin, fibrin, fibrinogen, elastin, keratin, albumin, hydroxyethyl cellulose, cellulose, oxidized cellulose, hydroxypropyl cellulose, carboxyethyl cellulose, carboxymethyl cellulose, chitan, chitosan, alginate, poly(lactic acid), poly( glycolic), poly(hydroxybutyrate), poly(phosphazine), polyesters, poly(ethylene glycols), poly(alkylene oxides), polyacrylamides, poly(hydroxyethyl methacrylate), polyvinylpyrrolidone, poly(vinyl alcohols), poly (caprolactone), poly(dioxanone), poly(acrylic acid), polyacetate, polyprolactone, polypropylene, aliphatic polyesters, glycerols, poly(amino acids), co-poly(ether esters), poly(alkylene oxalates) , polyamides, poly(iminocarbonates), poly(alkylene oxalates), poly(oxaesters), poly(orthoesters), polyphosphazenes and combinations thereof.

[000366] The fabric thickness compensator may comprise a layer comprising the reinforcing material. A porous layer and/or a non-porous layer of a fabric thickness compensator may comprise the reinforcing material. For example, the porous layer may comprise the reinforcing material and the non-porous layer may not comprise the reinforcing material. The reinforcing layer may comprise an inner layer intermediate a first non-porous layer and a second non-porous layer. The reinforcement layer may comprise an outer layer of fabric thickness compensator. The reinforcement layer may comprise an outer surface of the fabric thickness compensator.

[000367] The reinforcing material may comprise meshes, monofilament braids, multifilament braids, fibers, batts, felts, particles and/or powders. The reinforcement material may be incorporated into a layer of the fabric thickness compensator. The reinforcing material may be incorporated into at least one of a non-porous layer and a porous layer. A mesh comprising the reinforcing material may be formed using conventional techniques such as, for example, knitting, weaving, crocheting and/or lace making.

[000368] According to the invention, a plurality of reinforcement materials can be oriented in a random direction and/or a common direction. The common direction can be one of parallel to the staple line and perpendicular to the staple line, for example. For example, monofilament and/or multifilament braids can be oriented in a random direction and/or in a common direction. Monofilament and multifilament braids can be associated with the non-porous layer and/or the porous layer. The fabric thickness compensator may comprise a plurality of reinforcing fibers oriented in a random direction within a non-porous layer. The fabric thickness compensator may comprise a plurality of reinforcing fibers oriented in a common direction within a non-porous layer.

[000369] Referring to Figure 199, an anvil 70300 may comprise a fabric thickness compensator 70305 comprising a first non-porous layer 70307 and a second non-porous layer 70309 sealingly abutting a reinforcement layer 70310. 70310 reinforcement may comprise a hydrogel comprising ORC particles or fibers incorporated therein and the non-porous layers may comprise ORC. As shown in Figure 199, the fabric thickness compensator 70305 can be configured to conform to the contour of the anvil 70300. The inner layer of the fabric thickness compensator 70305 can conform to the inner surface of the anvil 70300, which includes the pockets. of training 70301.

[000370] The fibers can form a non-woven material such as, for example, a blanket and a felt. The fibers can be of any suitable length, for example from 0.1 mm to 100 mm and 0.4 mm to 50 mm. The reinforcing material can be ground to a powder. The powder can have a particle size of 10 micrometers to 1 cm, for example. Powder can be incorporated into the fabric thickness compensator.

[000371] The fabric thickness compensator can be formed in situ. The hydrogel can be formed in situ. The tissue thickness compensator can be formed in situ through covalent, ionic and/or hydrophobic bonds. Physical crosslinks (non-covalent) can result from complexation, hydrogen bonding, desolvation, Van der Waals interactions, ionic bonding and combinations thereof. Chemical (covalent) crosslinking can be accomplished through any number of mechanisms, including: free radical polymerization, condensation polymerization, anionic or cationic polymerization, stepwise growth polymerization, electrophile-nucleophile reactions, and combinations thereof.

[000372] Optionally, the in situ formation of the tissue thickness compensator may comprise the reaction of two or more precursors that are physically separated until in situ contact and/or the reaction to an ambient condition to react with each other to form the hydrogel. In situ polymerizable polymers can be prepared from precursor(s) which can react to form a polymer at the surgical site. The tissue thickness compensator can be formed through crosslinking reactions of the precursor(s) in situ. The precursor may comprise an initiator which has the ability to inhibit a polymerization reaction for tissue thickness compensator formation in situ. The tissue thickness compensator may comprise a precursor which can be activated at the time of application to create a cross-linked hydrogel. In situ formation of the tissue thickness compensator may comprise activating at least one precursor to form bonds to form the tissue thickness compensator. Optionally, activation can be achieved by changes in physical conditions, biological conditions, and/or chemical conditions at the surgical site that include, but are not limited to, temperature, pH, electric field, ionic strength, enzymatic and/or chemical reactions. , electrical and/or magnetic stimuli and other physiological and environmental variables. Precursors can be contacted outside the body and introduced into the surgical site.

[000373] The tissue thickness compensator may comprise one or more encapsulations, or cells, which may be configured to store at least one component therein. The encapsulation can be configured to store a hydrogel precursor therein. The encapsulation can be configured to store two components in it, for example. The encapsulation may be configured to store a first hydrogel precursor and a second hydrogel precursor therein. A first encapsulation can be configured to store a first hydrogel precursor therein and a second encapsulation can be configured to store a second hydrogel precursor therein. As described above, the encapsulations may be aligned, or at least substantially aligned, with the clamp legs to puncture and/or otherwise rupture the encapsulations when the clamp legs contact the encapsulation. Encapsulations can be compressed, crushed, flattened and/or otherwise broken when clamps are installed. After the encapsulations have been broken, the component(s) stored in them can flow out of the encapsulation. The component stored therein may come into contact with other components, fabric thickness compensator layers and/or fabric. The other components may flow from the same or different encapsulations, provided in the tissue thickness compensator layers and/or provided at the surgical site by the physician. As a result of the foregoing, the component(s) stored in the encapsulations may provide expansion and/or dilation of the tissue thickness compensator.

[000374] The fabric thickness compensator may comprise a layer comprising encapsulations. The encapsulation may comprise a void, a pocket, a dome, a tube and combinations thereof associated with the layer. Encapsulations can comprise empty spaces in the layer. The layer may comprise two layers that can be secured together, where encapsulations can be defined between the two layers. Encapsulations may comprise bellows on the surface of the layer. For example, at least a portion of the encapsulations may be positioned within bellows extending above the layer. Encapsulations may comprise pockets formed within the layer. A first portion of the encapsulations may comprise a dome and a second portion of the encapsulations may comprise a pocket. Encapsulations may comprise a tube embedded in the layer. The tube may comprise the non-synthetic materials and/or the synthetic materials described herein, such as PLA. The fabric thickness compensator may comprise a bioabsorbable foam, such as ORC, which comprises PLA tubes embedded therein, and the tube may encapsulate a hydrogel, for example. Encapsulations can comprise distinct cells that are not connected to each other. One or more of the encapsulations may be in fluid communication with each other through one or more passages, conduits and/or channels, for example extending through the layer.

[000375] The release rate of a component from the encapsulation can be controlled by the thickness of the tissue thickness compensator, the composition of the tissue thickness compensator, the size of the component, the hydrophilic capacity of the component and/or the physical and /or chemicals between the component, the tissue thickness compensator composition and/or the surgical instrument, for example. The layer may comprise one or more thin sections or weakened portions, such as partial perforations, for example, which may facilitate puncture of the layer and rupture of encapsulations. Partial perforations may not extend completely through a layer while, in some cases, perforations may extend completely through the layer.

[000376] Referring to Figures 194 and 195a, the fabric thickness compensator 70150 may comprise an outer layer 70152A and an inner layer 70152B comprising encapsulations 70154. The encapsulation may comprise an encapsulated first component and an encapsulated second component. The encapsulations may independently comprise one of a first encapsulated component and a second encapsulated component. The first encapsulated component can be separated from the second encapsulated component. The outer layer 70152A may comprise a fabric contacting surface. The inner layer 70152B may comprise an instrument-contacting surface. The instrument contacting surface 70152B may be releasably attached to the anvil 70156. The outer layer 70152A may be attached to the inner layer 70152B to define a void between the outer layer 70152A and the inner layer 70152B. As shown in Figure 194, each package 70154 may comprise a dome over the instrument-contacting surface of the inner layer 70152B. The dome may comprise partial perforations to facilitate the incision of the layer by the clamp legs and the rupture of the encapsulation. As shown in Figure 195, the anvil 70156 may comprise a plurality of rows of forming pocket 70158, wherein the bells of the encapsulations 70154 may be aligned with the forming pocket 70158. The tissue contacting surface may comprise a flat surface that lacks domes. The tissue contacting surface may comprise one or more encapsulations, such as the 70154 encapsulations, for example, extending therefrom.

[000377] Optionally, an anvil may comprise a tissue thickness compensator comprising an encapsulated component comprising at least one microsphere particle. The fabric thickness compensator may comprise an encapsulation comprising an encapsulated first component and an encapsulated second component. The fabric thickness compensator may comprise an encapsulation comprising a first microsphere particle and a second microsphere particle.

[000378] Referring to Figure 196, a stapling apparatus may comprise an anvil 70180 and a staple cartridge (illustrated in other figures). The staples 70190 of a staple cartridge can be deformed by an anvil 70180 when the anvil 70180 is moved to a closed position and/or by a staple drive system 70192 which moves the staples 70190 toward the closed anvil 70180. The legs 70194 of the clamps can contact the anvil 70180 so that the clamps 70190 are at least partially deformed. Anvil 70180 may comprise a fabric thickness compensator 70182 comprising an outer layer 70183A and an inner layer 70183B. Fabric thickness compensator 70182 may comprise an encapsulated first component and an encapsulated second component. The encapsulations 210185 may be aligned, or at least substantially aligned, so that when the staple legs 70194 are pushed through the T fabric and outer layer 70183A, the staple legs 70194 may puncture and/or otherwise rupture the 70185 packages. As shown in Figure 196, the 70190C clamp is in its fully fired position, the 70190B clamp is in the process of being fired, and the 70190A clamp is in its non-fired position. Staple legs 70190C and 70190B moved through the fabric T, outer layer 70183A and inner layer 70183B of the fabric thickness compensator 70182 and came into contact with an anvil 70180 positioned opposite the staple cartridge. After the 70185 encapsulations have been ruptured, the encapsulated components can flow out and come into contact with each other, with body fluids and/or T-tissue, for example. The encapsulated components can react to form a reaction product such as a hydrogel, for example to expand between the T fabric and the base of the staple and push the T fabric against the legs of the staple. In various circumstances, as a result of the above, the fabric thickness compensator may be configured to consume any gaps within the staple gripping area.

[000379] The tissue thickness compensator may be suitable for use with a surgical instrument. As described above, the tissue thickness compensator can be associated with the staple cartridge and/or the anvil. The fabric thickness compensator can be configured in any suitable shape, size and/or dimension to fit the staple cartridge and/or anvil. As described herein, the tissue thickness compensator may be releasably attached to the staple cartridge and/or anvil. The tissue thickness compensator may be attached to the staple cartridge and/or anvil in any mechanical and/or chemical manner capable of retaining the tissue thickness compensator in contact with the staple cartridge and/or anvil, before or during the stapling process. The tissue thickness compensator can be removed or released from the staple cartridge and/or anvil after the staple has penetrated the tissue thickness compensator. The tissue thickness compensator can be removed or released from the staple cartridge and/or anvil as the staple cartridge and/or anvil moves in the opposite direction of the tissue thickness compensator.

[000380] Referring to Figures 191 to 193, the stapling apparatus 70118 may comprise an anvil 70120 and a staple cartridge 70122 comprising a firing element 70124, a plurality of staples 70128, a knife edge 70129 and a fabric thickness compensator 70130. The fabric thickness compensator 70130 may comprise at least one encapsulated component. The encapsulated component may be ruptured when the fabric thickness compensator is compacted, stapled and/or cut. Referring to Figure 192, for example, staples 70128 may be installed between a non-fired position and a fired position so that the staple legs move through the fabric thickness compensator 70130, penetrate through a base surface and a top surface of the 70130 fabric thickness compensator, penetrate the fabric T and contact an anvil 70120 positioned opposite the staple cartridge 70118. The encapsulated components may react with each other, with an embedded or dispersed hydrophilic powder in the tissue thickness compensator and/or with body fluids to expand or dilate the tissue thickness compensator 70130. As the legs are deformed against the anvil, the legs of each clamp may capture a portion of the tissue thickness compensator 70130 and a portion of the fabric T inside each staple 70128 and apply a compressive force to the fabric T. As shown in Figures 192 and 193, the offset 70130 fabric thickness can compensate for the T fabric thickness captured by each 70128 staple.

[000381] Referring to Figure 197, a surgical instrument 70200 may comprise an anvil 70205 comprising an upper tissue thickness compensator 70210 and a staple cartridge 70215 comprising a lower tissue thickness compensator 70220 and an inner layer 70225. The upper fabric thickness compensator 70210 can be positioned on a first side of the target fabric and the lower fabric thickness compensator can be positioned on a second side of the fabric. The upper fabric thickness compensator 70210 may comprise ORC, the outer layer of the lower fabric thickness compensator may comprise a hydrogel having ORC particles incorporated therein, and the inner layer of the lower fabric thickness compensator may comprise ORC, for example.

[000382] Referring to Figures 200 to 202, a surgical instrument 70400 may comprise a staple cartridge 70405 and an anvil 70410. The staple cartridge 70405 may comprise a tissue thickness compensator 70415 including bioabsorbable foam. The bioabsorbable foam may comprise an encapsulation comprising an encapsulated component 70420. The bioabsorbable foam may comprise ORC and the encapsulated component may comprise a drug, for example. Fabric thickness compensator 70415 of anvil 70410 may comprise an inner layer 70425 and an outer layer 70430. The inner layer 70425 may comprise a bioabsorbable foam and the outer layer 70430 may comprise a hydrogel, optionally comprising reinforcing materials, for example . During an exemplary firing sequence, referring primarily to Figure 201, a slider 70435 may first contact clamp 70440A and begin to lift the clamp. As the 70435 slider advances further distally, the 70435 slider can begin to lift the 70440B-D clips and any subsequent clips in a sequential order. Sliding bracket 70435 can drive clamps 70440 upward so that the legs of the clamps contact the opposing anvil 70410 and are deformed into a desired shape. With respect to the firing sequence illustrated in Figure 201, the 70440A-C staples have been moved to their fully fired positions, the 70440D staple is in the process of being fired, and the 70420E staple is still in its unfired position. The encapsulated component 70470 can be broken by the clamp legs during the exemplary firing sequence. The encapsulated component 70420 may flow from the encapsulation around the clamp legs to contact the tissue T. Under various circumstances, further compression of the tissue thickness compensator may compress additional drug from the encapsulation. The drug can immediately treat the tissue and can reduce tissue bleeding.

[000383] Under various circumstances, a surgeon or other clinician may supply fluid to the tissue thickness compensator for the manufacture of a tissue thickness compensator comprising at least one drug stored and/or absorbed therein. In accordance with the invention, a staple cartridge and/or anvil may comprise a door configured to provide access to the fabric thickness compensator. Referring to Figure 203B, a staple cartridge 70500 may comprise a port 70505 at a distal end thereof, for example. Port 70505 can be configured to receive a 70510 needle, such as a fenestrated needle shown in Figure 203A. The clinician may insert a needle 70510 through port 70505 into tissue thickness compensator 70515 to supply fluid to tissue thickness compensator 70515. The fluid may comprise a drug and hydrogel precursor, for example. As described above, fluid may be released from the fabric thickness compensator into the fabric when the fabric thickness compensator is ruptured and/or compacted. For example, the drug may be released from the 70515 tissue thickness compensator as the 70515 tissue thickness compensator is biodegradable.

[000384] Now referring to Figure 14, a staple cartridge, such as the staple cartridge 10000, for example, may comprise a support portion 10010 and a compressible fabric thickness compensator 10020. Now referring to Figures 16 to 18 , the support portion 10010 may comprise a support surface 10011 and a plurality of clip recesses 10012 defined within the support portion 10010. Each clip recess 10012 may be sized and configured to releasably store a clip, such as a clamp 10030, for example. Staple cartridge 10000 may further comprise a plurality of staple drivers 10040 which can each be configured to support one or more staples 10030 within staple cavities 10012 when staples 10030 and staple drivers 10040 are in the their unfired positions. For example, referring primarily to Figures 22 and 23, each clamp driver 10040 may comprise one or more cradles, or channels, 10041, for example, which may be configured to support the clamps and limit relative movement between the clamps 10030 and the staple drivers 10040. Again referring to Figure 16, the staple cartridge 10000 may further comprise a staple firing slider 10050 which is moveable from a proximal end 10001 to a distal end 10002 of the staple cartridge so as to lift sequentially the staple drivers 10040 and staples 10030 from their unfired positions to an anvil positioned opposite the staple cartridge 10000. Referring primarily to Figures 16 and 18, each staple 10030 may comprise a base 10031 and one or more legs 10032 extending from base 10031 wherein each clamp may be at least one of substantially U-shaped and subs essentially V-shaped, for example. Clamps 10030 may be configured so that the ends of clamp legs 10032 are recessed with respect to platform surface 10011 of support portion 10010 when clamps 10030 are in their unfired positions. Clamps 10030 may be configured so that the ends of clamp legs 10032 are flush with the platform surface 10011 of support portion 10010 when clamps 10030 are in their unfired positions. Clamps 10030 may be configured so that the ends of clamp legs 10032, or at least some portion of clamp legs 10032, extend above the platform surface 10011 of support portion 10010 when clamps 10030 are in their non-active positions. shots. In such cases, clip legs 10032 may extend inwardly and may be fitted within fabric thickness compensator 10020 when clips 10030 are in their unfired positions. For example, the clamp legs 10032 can extend above the platform surface 10011 by approximately 1.9 mm (0.075"), for example. The clamp legs 10032 can extend above the platform surface 10011 by a distance between approximately 0.64 mm (0.025") and approximately 3.18 mm (0.125"), for example. In addition to those set out above, the fabric thickness compensator 10020 may comprise an uncompressed thickness between approximately 2.0 mm (0.08 ") and approximately 3.18 mm (0.125"), for example.

[000385] In use, in addition to the above and with reference primarily to Figure 31, an anvil, such as the anvil, 10060, for example, can be moved to a closed position opposite the staple cartridge 10000. As described in more In the details below, the anvil 10060 can position the fabric against the fabric thickness compensator 10020 and compress the fabric thickness compensator 10020 against the platform surface 10011 of the support portion 10010, for example. When the anvil 10060 has been properly positioned, the staples 10030 can be dispensed with, as also illustrated in Figure 31. Optionally, as mentioned above, the staple firing slider 10050 can be moved from the proximal end 10001 of the clamps 10000 to the distal end 10002, as illustrated in Figure 32. When sled 10050 is advanced, sled 10050 can contact clamp drivers 10040 and lift clamp drivers 10040 into clamp cavities 10012. Slider 10050 and staple drivers 10040 may each comprise one or more slopes, or inclined surfaces, which may cooperate to move staple drivers 10040 upward from their unfired positions. For example, with reference to Figures 19 to 23, each clamp driver 10040 may comprise at least one sloped surface 10042 and the slider 10050 may comprise one or more sloped surfaces 10052 which can be configured so that sloped surfaces 10052 can slide under the inclined surface 10042 when the slider 10050 is advanced distally within the staple cartridge. When the staple drivers 10040 are lifted into their respective staple cavities 10012, the staple drivers 10040 may lift the staples 10030 so that the staples 10030 can emerge from their staple cavities 10012 through openings in the staple holder 10011 . During an exemplary firing sequence, referring primarily to Figures 25 to 27, slider 10050 may first contact clamp 10030a and begin lifting clamp 10030a. When the sled 10050 is further advanced distally, the sled 10050 may begin lifting clamps 10030b, 10030c, 10030d, 10030e, and 10030f, and any subsequent clamps, in a sequential order. As illustrated in Figure 27, the slider 10050 can direct the clamps 10030 upwards so that the legs 10032 of the clamps contact the opposing anvil, are deformed into a desired shape, and ejected from the support portion 10010. In various circumstances , the sled 10030 can move multiple clamps up simultaneously as part of a firing sequence. With respect to the firing sequence illustrated in Figure 27, staples 10030a and 10030b have been moved to their fully fired positions and ejected from support portion 10010, staples 10030c and 10030d are in the process of being fired and are at least partially contained within the support portion 10010, and clamps 10030e and 10030f are still in their unfired positions.

[000386] As discussed above, and with reference to Figure 33, the clamp legs 10032 of the clamps 10030 may extend above the support surface 10011 of the support portion 10010 when the clamps 10030 are in their unfired positions. With further reference to this firing sequence illustrated in Figure 27, the staples 10030e and 10030f are illustrated in their unfired position and their staple legs 10032 extend above the support surface 10011 and into the fabric thickness compensator 10020. ends of staple legs 10032, or any other portion of staple legs 10032, may not protrude through a top fabric contacting surface 10021 of fabric thickness compensator 10020 when staples 10030 are in their unfired positions . When the staples 10030 are moved from their unfired positions to their fired positions, as illustrated in Figure 27, the tips of the staple legs may protrude through the fabric contacting surface 10032. The tips of the staple legs 10032 may comprise sharp points that can cut and penetrate the fabric thickness compensator 10020. The fabric thickness compensator 10020 may comprise a plurality of openings that may be configured to receive the staple legs 10032 and allow the staple legs 10032 to slide in relative to fabric thickness compensator 10020. Support portion 10010 may further comprise a plurality of guides 10013 extending from platform surface 10011. Guides 10013 may be positioned adjacent to surface staple cavity openings in the surface. support 10011 so that the clamp legs 10032 can be at least partially supported by the guides s 10013. A guide 10013 may be positioned at a proximal end and/or a distal end of a staple cavity opening. In accordance with the invention, a first guide 10013 can be positioned at a first end of each opening of the staple cavity and a second guide 10013 can be positioned at a second end of each opening of the staple cavity so that each first guide 10013 can support a first clamp leg 10032 of a clamp 10030 and each second guide 10013 can support a second clamp leg 10032 of the clamp. Referring to Figure 33, each guide 10013 may comprise a groove or slot, such as groove 10016 for example, within which a clamp leg 10032 may be slidably received. Optionally, each guide 10013 may comprise a handle, protuberance, and/or peg that may extend from the platform surface 10011 and may extend into the fabric thickness compensator 10020. As discussed in more detail below, the handles, protuberances , and/or pegs may reduce relative movement between the fabric thickness compensator 10020 and the support portion 10010. The ends of the clamp legs 10032 may be positioned within the guides 10013 and may not extend above the top surfaces of the clips 10032. guides 10013 when clamps 10030 are in their unfired position. For example, guides 10013 may define a guide height and clamps 10030 may not extend above this guide height when they are in their unfired positions.

[000387] According to the invention, a fabric thickness compensator, such as the fabric thickness compensator 10020, for example, can be comprised of a single sheet of material. A fabric thickness compensator may comprise a continuous sheet of material that may cover the entire upper platform surface 10011 of the support portion 10010 or, alternatively, cover less than the entire platform surface 10011. The sheet of material may cover the staple cavity openings in support portion 10010 while, alternatively, the sheet of material may comprise openings that can be aligned, or at least partially aligned, with the staple cavity openings. In accordance with the invention, a fabric thickness compensator may be comprised of multiple layers of material. Referring now to Figure 15, a fabric thickness compensator may comprise a compressible core and a shell surrounding the compressible core. A housing 10022 may be configured to releasably secure the compressible core to the support portion 10010. For example, the support portion 10010 may comprise one or more projections, such as projections 10014 (Figure 18), for example, that extend therefrom and which can be received within one or more openings and/or slots, such as openings 10024, for example, defined in housing 10022. Projections 10014 and openings 10024 can be configured so that the projections 10014 can secure the housing 10022 to the support portion 10010. The ends of the projections 10014 may be deformed, as by a hot-fitting process, for example, in order to widen the ends of the projections 10014 and, as a result, limit movement relative between the housing 10022 and the support portion 10010. The housing 10022 may comprise one or more perforations 10025 that can facilitate the release of the housing 10022 from the support portion 10010, as illustrated in Figure 15. Referring now to Figure 24, a fabric thickness compensator may comprise a housing 10222 that includes a plurality of apertures 10223, wherein apertures 10223 may be aligned, or at least partially aligned, with apertures in the staple cavity in support portion 10010. The fabric thickness compensator core may also comprise apertures that are aligned, or at least partially aligned, with apertures 10223 in housing 10222. Alternatively, the fabric thickness compensator core may comprises a continuous body and can extend below openings 10223 so that the continuous body covers the openings of the staple cavity in the platform surface 10011.

[000388] Optionally, as described above, a fabric thickness compensator may comprise a housing for releasably securing a compressible core to the support portion 10010. For example, with reference to Figure 16, a staple cartridge may additionally comprise tabs retainers 10026 which may be configured to inhibit the shell, and compressible core, from prematurely detaching from the support portion 10010. Optionally, each retaining clip 10026 may comprise apertures 10028 which may be configured to receive projections 10014 that extend from the support portion 10010 so that the retainer clips 10026 can be retained on the support portion 10010. The retainer clips 10026 may each comprise at least one reservoir portion 10027 which can extend beneath the support portion 10010 and can support and retain the clamp drivers 10040 within the support portion 10010. As described As described above, a fabric thickness compensator may be removably attached to the support portion 10010 by the clips 10030. More particularly, as also described above, the legs of the staples 10030 may extend into the fabric thickness compensator 10020 when the staples 10030 are in the unfired position and, as a result, releasably secure the fabric thickness compensator 10020 to the support portion 10010. The legs of the staples 10030 may be in contact with the side walls of their respective staple cavities 10012 wherein, due to friction between the staple legs 10032 and the side walls, staples 10030 and fabric thickness compensator 10020 may be held in position until staples 10030 are dispensed from staple cartridge 10000. When staples 10030 are dispensed, the fabric thickness compensator 10020 can be captured inside the staples 10030 and held against the stapled fabric T. When the big When one is later moved to an open position to release the fabric T, the support portion 10010 can be moved away from the fabric thickness compensator 10020 which has been secured to the fabric. An adhesive may be used to removably secure the fabric thickness compensator 10020 to the support portion 10010. A two-part adhesive may be used of which a first part may be placed on the platform surface 10011 and a second part. part of the adhesive can be placed on the fabric thickness compensator 10020 so that when the fabric thickness compensator 10020 is placed against the platform surface 10011, the first part can contact the second part to activate the adhesive and detachably attaching the fabric thickness compensator 10020 to the support portion 10010. Optionally, any other suitable means could be used to detachably attach the fabric thickness compensator to the support portion of a staple cartridge.

[000389] In addition to the above, the slider 10050 can be advanced from the proximal end 10001 to the distal end 10002 to completely dispense all staples 10030 contained within the staple cartridge 10000. Now referring to Figures 56 to 60, the slider 10050 may be advanced distally into a longitudinal cavity 10016 within the support portion 10010 by a trigger element, or cutter bar, 10052 of a surgical stapler. In use, the 10000 staple cartridge can be inserted into a staple cartridge channel in a surgical stapler jaw, such as the 10070 staple cartridge channel, for example, and the 10052 trigger element can be advanced to contact with the 10050 slider as shown in Figure 56. When the sled 10050 is advanced distally by the trigger element 10052, the sled 10050 may contact the more proximal staple driver or drivers 10040 and fire or eject clips 10030 from the cartridge body 10010 as described above. As illustrated in Figure 56, the trigger element 10052 may additionally comprise a cutting edge 10053 which can be advanced distally through a knife slot in the support portion 10010 when the clamps 10030 are being triggered. In accordance with the invention, a corresponding knife slot can extend through the anvil positioned opposite the staple cartridge 10000 so that the cutting edge 10053 can extend between the anvil and the support portion 10010 and cut the fabric and the fabric thickness compensator positioned between them. In various circumstances, slider 10050 may be advanced distally by trigger element 10052 until slider 10050 reaches distal end 10002 of staple cartridge 10000, as illustrated in Figure 58. At this point trigger element 10052 may be retracted proximally. Slider 10050 may be retracted proximally with trigger element 10052 but, now referring to Figure 59, slider 10050 may be left behind at distal end 10002 of staple cartridge 10000 when trigger element 10052 is retracted. When the trigger element 10052 has been sufficiently retracted, the anvil can be reopened, the tissue thickness compensator 10020 can be detached from the support portion 10010, and the remaining non-implanted portion of the used staple cartridge 10000, including the holder 10010, can be removed from the staple cartridge groove 10070.

[000390] After the used staple cartridge 10000 has been removed from the staple cartridge slot, in addition to the above, a new staple cartridge 10000, or any other suitable staple cartridge, can be inserted into the staple cartridge slot 10070 In addition to the above, the staple cartridge channel 10070, the trigger element 10052, and/or the staple cartridge 10000 may comprise cooperating elements that can prevent the trigger element 10052 from being advanced distally a second time, or a second time. subsequent time, without a new, or unfired, staple cartridge 10000 positioned in the staple cartridge groove 10070. More particularly, again with reference to Figure 56, when firing element 10052 is advanced into contact with slider 10050 and, when the slider 10050 is in its proximal unfired position, a support tip 10055 of the firing element 10052 may be positioned on and/or along a support protrusion. and 10056 on slider 10050 such that trigger 10052 is held in a sufficient vertical position to prevent a lock, or beam, 10054 extending from trigger 10052 from falling into a locking recess defined within the groove of staple cartridge. As the latch 10054 will not fall into the locking recess, under such circumstances, the latch 10054 may not be in a position bordering a distal side wall 10057 of the locking recess when the trigger 10052 is advanced. When the trigger element 10052 pushes the sled 10050 distally, the trigger element 10052 can be supported in its firing position upwards due to the support tip 10055 resting on the support projection 10056. When the trigger element 10052 is retracted with respect to the slider 10050, as discussed above and illustrated in Figure 59, the trigger element 10052 may detach downwards from its upward position when the support tip 10055 is no longer resting on the support boss 10056 of the slider 10050. For example, the surgical clip may comprise a spring 10058, and/or any other suitable traction element, which may be configured to traction the trigger element 10052 to its downward position. When the trigger element 10052 has fully retracted, as shown in Figure 60, the trigger element 10052 cannot be advanced distally through the used staple cartridge 10000. More particularly, the trigger element 10052 cannot be held in its position. upper position by the sled 10050 when the sled 10050, at this point in the operating sequence, has been left behind at the distal end 10002 of the staple cartridge 10000. Thus, as mentioned above, in the case where the trigger element 10052 is advanced again without replacement of the staple cartridge, the locking beam 10054 will contact the side wall 10057 of the locking recess which will prevent the trigger element 10052 from being advanced distally into the staple cartridge 10000 again. In other words, once the used staple cartridge 10000 has been replaced with a new staple cartridge, the new staple cartridge will have a proximally positioned sled 10050 that can hold the firing element 10052 in its upper position and allow the element to trigger 10052 is re-advanced distally.

[000391] As described above, the sled 10050 can be configured to move the staple drivers 10040 between a first unfired position and a second fired position so as to eject the staples 10030 from the support portion 10010. The staple drivers 10040 may be contained within clip cavities 10012 after clips 10030 have been ejected from support portion 10010. Support portion 10010 may comprise one or more retention elements which may be configured to prevent clamp drivers 10040 from being ejected or fall out of staple cavities 10012. Alternatively, slider 10050 may be configured to eject staple drivers 10040 from support portion 10010 with staples 10030. For example, staple drivers 10040 may be comprised of a bioabsorbable material. and/or biocompatible, such as Ultem, for example. Staple drivers can be attached to staples 10030. For example, a staple driver can be molded onto and/or around the base of each staple 10030 so that the driver is integrally formed with the staple. US Patent Application Serial No. 11/541,123, entitled SURGICAL STAPLES HAVING COMPRESSIBLE OR CRUSHABLE MEMBERS FOR SECURING TISSUE THEREIN AND STAPLING INSTRUMENTS FOR DEPLOYING THE SAME, filed September 29, 2006, is incorporated herein by reference at its entirety.

[000392] As described above, a surgical stapling instrument may comprise a staple cartridge groove configured to receive a staple cartridge, an anvil rotationally coupled to the staple cartridge groove, and a trigger element comprising a tip. blade that is movable with respect to the anvil and staple cartridge groove. In use, a staple cartridge can be positioned inside the staple cartridge groove and, after the staple cartridge has been at least partially used, the staple cartridge can be removed from the staple cartridge groove and replaced with a new one. new staple cartridge. For example, the staple cartridge groove, anvil, and/or trigger element of the surgical stapling instrument can be reused with the replacement staple cartridge. Alternatively, a staple cartridge may comprise a portion of a disposable loading unit assembly which may include a staple cartridge channel, an anvil, and/or a firing element, for example, which can be replaced along with the cartridge. of staples as part of the replacement disposable charging unit assembly. Certain disposable charging unit assemblies are disclosed in US Patent Application Serial No. 12/031,817 entitled END EFFECTOR COUPLING ARRANGEMENTS FOR A SURGICAL CUTTING AND STAPLING INSTRUMENT, which was filed February 15, 2008, the disclosure of which is incorporated herein by way of reference.

[000393] The fabric thickness compensator may comprise an extrudable, fusible and/or moldable composition comprising at least one of the synthetic and/or non-synthetic materials described herein. The fabric thickness compensator may comprise a film or sheet comprising two or more layers. Fabric thickness compensator can be obtained using conventional methods such as mixing, blending, formulating, spraying, capillary absorption, solvent evaporation, immersion, brushing, steam deposition, extrusion, calendering, casting , molding and the like. In extrusion, an aperture may be in the form of a die comprising at least one aperture for shaping the emerging extrudate. In calendering, an opening may comprise a throttling between two rollers. Conventional molding methods may include, but are not limited to, blow molding, injection molding, foam injection, compaction molding, thermoforming, extrusion, foam extrusion, blown film forming, calendering, spinning, solvent welding, coating methods such as dip coating and spin coating, solution casting and film molding, plastisol processing (including knife coating, roller coating and casting) and combinations thereof. In injection molding, an opening may comprise a nozzle and/or channels/gutters and/or mold features and cavities. In compaction modeling, the composition can be placed in a mold cavity, heated to a suitable temperature, and formed upon exposure to compaction under relatively high pressure. In casting, the composition may comprise an aqueous liquid or slurry that can be poured or otherwise supplied into, on and/or around a mold or object to replicate features of the mold or object. After casting, the composition can be dried, cooled and/or cured to form a solid.

[000394] In accordance with the invention, a method of manufacturing a fabric thickness compensator may generally comprise providing a fabric thickness compensator composition, liquefying the composition to make it flowable, and forming the composition in molten, semi-molten or plastic state forming a layer and/or film having the desired thickness. Referring to Figure 198A, a fabric thickness compensator can be manufactured by dissolving a hydrogel precursor in an aqueous solution, dispersing biocompatible particles and/or fibers therein, providing a mold that has biocompatible particles therein. , feeding the solution into the mold, bringing an activator and the solution into contact, and curing the solution to form the tissue thickness compensator comprising an outer layer comprising biocompatible particles and an inner layer comprising biocompatible particles incorporated therein. As shown in Figure 198A, a biocompatible layer 70250 can be supplied to the bottom of a mold 70260 and an aqueous solution of a hydrogel precursor 70255 that has biocompatible particles 70257 disposed therein can be supplied to the mold 70260 and the aqueous solution can be be cured to form a fabric thickness compensator having a first layer comprising a biocompatible material, such as ORC, for example, and a second layer comprising a hydrogel having biocompatible fibers, such as ORC fibers, disposed therein. The fabric thickness compensator may comprise a foam comprising an outer layer comprising biocompatible particles and an inner layer comprising biocompatible particles incorporated therein. A fabric thickness compensator can be made by dissolving sodium alginate in water, dispersing ORC particles therein, providing a mold that has ORC particles in it, and pouring the solution into the mold. , spraying or infusing calcium chloride to contact the solution to initiate crosslinking of the sodium alginate, freeze drying the hydrogel to form the tissue thickness compensator comprising an outer layer that comprises ORC and an inner layer comprising a hydrogel and ORC particles incorporated therein.

[000395] Referring to Figure 198B, a method of manufacturing a three-layer fabric thickness compensator may comprise, in general, dissolving a first hydrogel precursor in a first aqueous solution, dispersing biocomposite particles and/or fibers. - compatible in the first aqueous solution, supply a 70260 mold that has a 70250 first layer of biocompatible particles in it, supply the first aqueous solution in the mold, place an activator and the first aqueous solution in contact, cure the first aqueous solution to form a second layer 70255, dissolve a second hydrogel precursor in a second aqueous solution, feed the second aqueous solution into the mold, cure the second aqueous solution to form a third layer 70265. A three-layer fabric thickness compensator can be manufactured dissolving a sodium alginate in water to form a first aqueous solution, dispersing ORC particles in the first aqueous solution, providing a a mold that has a first layer of ORC particles in it, by pouring the first aqueous solution into the mold, spraying or infusing calcium chloride to contact the first aqueous solution to initiate crosslinking. sodium alginate, freeze-drying the first aqueous solution to form a second layer comprising a hydrogel having ORC particles incorporated therein, and dissolving a sodium alginate in water to form a second solution. aqueous solution, pouring the second aqueous solution into the mold, spraying or infusing calcium chloride to contact the second aqueous solution to initiate crosslinking of the sodium alginate, and drying by freezing the second aqueous solution to form a third layer comprising a hydrogel.

[000396] According to the invention, a method of manufacturing a tissue thickness compensator comprising at least one drug stored and/or absorbed therein may generally comprise providing a tissue thickness compensator and contacting the tissue thickness compensator and the medicament to retain the medicament in the tissue thickness compensator. A method of manufacturing a fabric thickness compensator comprising an antibacterial material may comprise supplying a hydrogel, drying the hydrogel, swelling the hydrogel in an aqueous solution of silver nitrate, contacting the hydrogel and a chloride solution. of sodium to form the fabric thickness compensator that has antibacterial properties. The fabric thickness compensator may comprise silver dispersed therein.

[000397] Referring to Figure 204, a method for manufacturing a fabric thickness compensator may comprise co-extrusion and/or bonding. Fabric thickness compensator 70550 may comprise a laminate comprising a first layer 70555 and a second layer 70560 sealingly abutting an inner layer 70565 comprising a hydrogel, for example. The hydrogel may comprise a dry film, a dry foam, a powder and/or granules, for example. The hydrogel may comprise superabsorbent materials such as, for example, polyvinylpyrrolidone, carboxymethylcellulose, poly(sulfopropyl acrylate). The first and/or second layers can be produced in line by feeding raw materials from the first and second layers, respectively, into an extruder of a feeder tank and thereafter feeding the first and second layers. Inner layer 70565 raw materials can be added to an extruder feed hopper. The raw materials can be dispersed and dispersedly formulated at an elevated temperature inside the extruder. As raw materials exit die 70570 at an inlet, the inner layer 70565 may be deposited onto a surface of the first layer 70555. The fabric thickness compensator may comprise a foam, film, powder and/or granule. First and second layers 70555 and 70560 can be positioned in face-to-face relationship. The second layer 70560 may be aligned with the first layer 70555 in a face-to-face relationship by a cylinder 70575. The first layer 70555 may be adhered to the second layer 70560, wherein the first and second layers 70555, 70560 may entrap physically the inner layer 70565. The layers may be joined under light pressure, under conventional calender bonding processes, and/or through the use of adhesives, for example, to form the fabric thickness compensator 70550. As shown in Figure 78, the first and second layers 70555 and 70560 can be joined through a lamination process using a grooved roll 70580, for example. Optionally, as a result of the foregoing, the inner layer 70565 may be contained and/or sealed by the first and second layers 70555 and 70560 which may collectively form an outer layer, or barrier. The outer layer can prevent or reduce moisture from contacting the 70565 inner layer until the outer layer is ruptured.

[000398] Referring to Figure 61, an end actuator 12 for a surgical instrument 10 (Figure 1) can be configured to receive a cartridge assembly of fasteners, such as the staple cartridge 20000, for example. As illustrated in Figure 61, the 20000 staple cartridge can be configured to fit into a 20072 cartridge groove of a 20070 jaw of the end actuator 12. Alternatively, the 20000 staple cartridge can form a single piece with the end actuator 12 so that staple cartridge 20000 and end actuator 12 are formed as a unitary construction. Staple cartridge 20000 may comprise a first body portion, such as a rigid support portion 20010, for example. Staple cartridge 20000 may also comprise a second body portion, such as a compressible portion or a fabric thickness compensator 20020, for example. Alternatively, fabric thickness compensator 20020 may not comprise an integral part of staple cartridge 20000, but may be positioned otherwise with respect to end actuator 12. For example, fabric thickness compensator 20020 may be secured to an anvil 20060 of the end actuator 12 or may be otherwise retained to the end actuator 12. Referring to Figure 78, the staple cartridge may additionally comprise retaining tabs 20126 which may be configured to prevent the fabric thickness compensator from 20020 prematurely separates from the support portion 20010. The reader will note that the fabric thickness compensators described herein can be installed or otherwise engaged with a variety of end actuators and that they are within the scope of the present disclosure.

[000399] Similar to the tissue thickness compensators described herein, now with reference to Figure 78, the tissue thickness compensator 20020 can be released or disengaged from the surgical end actuator 12. For example, the rigid support portion 20010 of the 20000 staple cartridge can remain engaged with the 20072 fastener cartridge groove of the 20070 end actuator grip while the 20020 fabric thickness compensator disengages from the 20010 rigid support portion. The 20020 fabric thickness compensator can release it. end actuator 12 after clamps 20030 (Figures 78 to 83) are installed from clamp cavities 20012 into rigid support portion 2010. Clamps 20030 can be fired from clamp cavities 20012 so that clamps 20030 engage the compensator of fabric thickness 20020. Also, in general, with reference to Figures 63, 82 and 83, a staple 20030 can capture a portion of the thickness compensator fabric sura 20020 together with stapled fabric T. The fabric thickness compensator 20020 can be deformable and the portion of the fabric thickness compensator 20020 that is captured by a fired staple 20030 can be compacted. Similar to the fabric thickness compensators described herein, the fabric thickness compensator 20020 can compensate for different thicknesses, compressibilities and/or densities of fabric T captured by each staple 20030. Additionally, as also described herein, the fabric thickness compensator Fabric thickness 20020 can compensate for gaps created by malformed staples 20030.

[000400] The Fabric Thickness Compensator 20020 can be compressible between uncompacted height(s) and compacted height(s). Referring to Figure 78, the fabric thickness compensator 20020 may have a top surface 20021 and a base surface 20022. The height of the fabric thickness compensator may be the distance between the top surface 20021 and the base surface 20022. The uncompacted height of the fabric thickness compensator 20020 can be the distance between the top surface 20021 and the base surface 20022 when minimal force or no shape is applied to the fabric thickness compensator 20020, i.e. , when the Fabric Thickness Compensator 20020 is not compacted. The compressed height of the fabric thickness compensator 20020 can be the distance between the top surface 20021 and the base surface 20022 when a force is applied to the fabric thickness compensator 20020, such as when a fired staple 20030 captures a portion of the compensator fabric thickness 20020, for example. The tissue thickness compensator 20020 may have a distal end 20025 and a proximal end 20026. As illustrated in Figure 78, the uncompressed height of the tissue thickness compensator 20020 may be uniform between the distal end 20025 and the proximal end 20026 of the fabric thickness compensator 20020. Alternatively, the uncompacted height may vary between the distal end 20025 and the proximal end 20026. For example, the top surface 20021 and/or the base surface 20022 of the fabric thickness compensator 20020 may be angled and/or staggered with respect to each other so that the uncompacted height varies between the proximal end 20026 and the distal end 20025. The uncompacted height of the 20020 tissue thickness compensator may be approximately 2 millimeters (0.08 inch ), for example. Alternatively, the uncompacted height of the fabric thickness compensator 20020 can vary between approximately 0.064 centimeters and approximately 0.25 centimeters (approximately 0.025 inches and approximately 0.10 inches), for example.

[000401] As described in more detail in this document, the tissue thickness compensator 20020 can be compacted to different heights compacted between the proximal end 20026 and the distal end 20025 thereof. Alternatively, the fabric thickness compensator 20020 may be uniformly compacted along the length thereof. The compressed height(s) of the 20020 fabric thickness compensator may depend on the geometry of the end actuator 12, the characteristics of the 20020 fabric thickness compensator, the T-engaged fabric and/or the 20030 clamps, for example. The compressed height of the fabric thickness compensator 20020 can be related to the fabric gap in the end actuator 12. Optionally, when the anvil 20060 is tightened towards the staple cartridge 20000, the fabric gap can be defined between a surface of top platform 20011 (Figure 78) of staple cartridge 20000 and a tissue contacting surface 20061 (Figure 61) of anvil 20060, for example. The fabric gap may be approximately 0.64 mm or approximately 0.25 cm (approximately 0.025 inch or approximately 0.100 inch, for example). The fabric gap may be approximately 0.750 mm or approximately 3,500 mm, for example. The compacted height of the fabric thickness compensator 20020 can be equal to or substantially equal to the fabric span, for example. When the fabric T is positioned within the fabric gap of the end actuator 12, the compressed height of the fabric thickness compensator may be lower in order to accommodate the fabric T. For example, where the fabric gap is approximately 0.750 mm, the compressed height of the fabric thickness compensator can be approximately 0.500 mm. Where the fabric gap is approximately 3,500 mm, the packed height of the fabric thickness compensator 20020 may be approximately 2.5 mm, for example. Furthermore, the fabric thickness compensator 20020 may comprise a minimum compacted height. For example, the minimum compressed height of the 20020 Fabric Thickness Compensator can be approximately 0.250 mm. The fabric gap defined between the platform surface of the staple cartridge and the fabric-contacting surface of the anvil may be equal to, or at least substantially equal to, the uncompacted height of the fabric thickness compensator, for example.

[000402] Referring primarily to Figure 62, the fabric thickness compensator 20020 may comprise a fibrous non-woven material 20080 including the fibers 20082. The fabric thickness compensator 20020 may comprise felt or a felt-like material. The 20082 fibers in the 20080 nonwoven material may be joined by any means known in the art including, but not limited to, needle-punching, thermowelding, hydroentangling, ultrasonic patterned bonding, chemical bonding, and melt blown bonding. Additionally, the layers of nonwoven material 20080 may be mechanically, thermally or chemically joined to form the fabric thickness compensator 20020. As described in greater detail herein, the fibrous nonwoven material 20080 may be compressible, which may allow for the compaction of the fabric thickness compensator 20020. The fabric thickness compensator 20020 may also comprise a non-compressible portion. For example, the fabric thickness compensator 20020 may comprise a compressible non-woven material 20080 and a non-compressible portion.

[000403] Further, referring primarily to Figure 62, the nonwoven material 20080 may comprise a plurality of fibers 20082. At least some of the fibers 20082 in the nonwoven material 20080 may be crimped fibers 20086. The crimped fibers 20086 may be, for example, example, crimped, twisted, spiral wound, folded, bent, spiraled, curled and/or bowed in 20080 non-woven material. As described in more detail in this document, 20086 crimped fibers can be of any suitable shape so that the deformation of the fibers crimped 20086 generates a spring action or a reset force. The 20086 crimped fibers can be heat formed to form a spiral wound or substantially spiral-like shape. Crimp fibers 20086 can be formed from non-crimp fibers 20084. For example, non-crimp fibers 20084 can be wound around a heated mandrel to form a substantially spiral-like shape.

[000404] The fabric thickness compensator 20020 may comprise a homogeneous absorbable polymeric matrix. The homogeneous absorbable polymeric matrix may comprise a foam, gel and/or film, for example. Additionally, the plurality of fibers 20082 can be dispersed throughout the homogeneous absorbable polymeric matrix. At least part of the 20082 fibers in the homogeneous absorbable polymer matrix may be composed of crimped 20086 fibers, for example. As described in more detail in this document, the homogeneous absorbable polymer matrix of the fabric thickness compensator 2002 may be compressible.

[000405] Referring to Figures 65 and 66, the crimped fibers 20086 may be randomly dispersed throughout at least a portion of the non-woven material 20080. For example, the crimped fibers 20086 may be randomly dispersed throughout the non-woven material 20080 such that a portion of the 20080 nonwoven material comprises more 20086 crimped fibers than other portions of the 20080 nonwoven material. Additionally, the 20086 crimped fibers can be joined into fiber bundles 20085a, 20085b, 20085c, 20085d and 20085e , for example, in non-woven material 20080. The shape of the crimped fibers 20086 can cause the 20086 fibers to become entangled during the manufacture of the non-woven material 20080; the entanglement of the crimped fibers 20086 may, in turn, result in the formation of fiber bundles 20085a, 20085b, 20085c, 20085d and 20085e. Additionally or alternatively, the crimp fibers 20086 may be randomly oriented along the nonwoven material 20080. For example, with reference to Figure 62, a first crimp fiber 20086a may be oriented in a first direction, a second crimp fiber 20086b may be oriented in a second direction and a third crimped fiber 20086c can be oriented in a third direction.

[000406] The crimped fibers 20086 can be systematically distributed and/or arranged along at least a portion of the non-woven material 20080. For example, now referring to Figure 67, the crimped fibers 20186 can be positioned in an arrangement 20185, wherein a plurality of crimped fibers 20186a is disposed in a first direction and another plurality of crimped fibers 20186b is disposed in a second direction. The 20186 crimp fibers can overlap so that they are intertwined or interconnected with each other. The crimp fibers 20186 can be systematically arranged so that one crimp fiber 20186a is substantially parallel to the other crimp fiber 20186a. Yet another crimp fiber 20186b may be substantially transverse to some crimp fibers 20186a. Optionally, the crimp fibers 20186a can be substantially aligned with a first Y axis and the crimp fibers 20186b can be substantially aligned with a second X axis. The first Y axis can be perpendicular or substantially perpendicular to the second X axis, for example.

[000407] Referring primarily to Figure 68, the crimped fibers 20286 may be arranged in an arrangement 20285. Each of the crimped fibers 20286 may comprise a longitudinal axis defined between a first end 20287 and a second end 20289 of the crimp fiber 20286. The crimp fibers 20286 may be systematically distributed in the nonwoven material 20080 so that a first end 20287 of a crimp fiber 20286 is positioned adjacent a second end 20289 of another crimp fiber 20286. Alternatively, now referring to the Figure 69, a fiber array 20385 may comprise a first crimp fiber 20386a oriented in a first direction, a second crimp fiber 20386b oriented in a second direction, and a third crimp fiber 20386c oriented in a third direction, for example. In accordance with the invention, a single pattern or arrangement of crimped fibers 20286 can be repeated throughout the non-woven material 20080. The crimped fibers can be arranged in different patterns along the non-woven material 20080. As a further alternative, the material The non-woven fabric 20080 may comprise at least one pattern of crimped fibers as well as a plurality of randomly oriented and/or randomly distributed crimp fibers.

[000408] Again with reference to Figure 62, the plurality of fibers 20082 in the non-woven material 20080 may comprise at least some non-crimped fibers 20084. The non-crimped fibers 20084 and the crimped fibers 20086 in the non-woven material 20080 may be interwoven or interconnected . The ratio of 20086 crimped fibers to 20084 non-crimped fibers can be approximately 25:1, for example. Alternatively, the ratio of crimped 20086 fibers to non-crimped 20084 fibers can be approximately 1:25, for example. Alternatively, the ratio of crimped 20086 fibers to non-crimped 20084 fibers can be approximately 1:1, for example. As described in more detail in this document, the number of crimped fibers 20086 per unit volume of 20080 non-woven material can affect the restoring force generated by the 20080 non-woven material when the 20080 non-woven material has been deformed. As also described in more detail in this document, the restoring force generated by the non-woven material 20080 may also depend on, for example, the material, shape, size, position and/or orientation of crimped and non-crimped fibers 20086, 20084 on non-woven material 20080.

[000409] The fibers 20082 of the non-woven material 20080 may comprise a polymeric composition. The polymeric composition of the 20082 fibers may comprise non-absorbable polymers, absorbable polymers, or combinations thereof. Absorbable polymers may include bioabsorbable biocompatible elastomeric polymers. Furthermore, the polymeric composition of the 20082 fibers may comprise synthetic polymers, non-synthetic polymers or combinations thereof. Examples of synthetic polymers include, but are not limited to, poly(glycolic acid) (PGA), poly(lactic acid) (PLA), polycaprolactone (PCL), polydioxanone (PDO) and copolymers thereof. For example, 20082 fibers may comprise a 90/10 poly(glycolide-L-lactide) copolymer, such as, for example, the copolymer commercially available from Ethicon, Inc. under the tradename "VICRYL (polyglactic 910)", Examples of non-synthetic polymers include, but are not limited to, lyophilized polysaccharide, glycoprotein, elastin, proteoglycan, gelatin, collagen and oxidized regenerated cellulose (ORC). Optionally, similar to the polymeric compositions in fabric thickness compensators described herein, the polymeric composition of the 20082 fibers can include varying amounts of absorbable polymers, non-absorbable polymers, synthetic polymers and/or non-synthetic polymers, for example by weight.

[000410] The crimped fibers 20086 of the non-woven material 20080 may comprise a first polymeric composition and the non-crimp fibers 20084 of the non-woven material 20080 may comprise a different polymeric composition. For example, 20086 crimped fibers may comprise synthetic polymer(s), such as poly(glycolide-L-lactide) 90/10, while 20084 non-crimped fibers may comprise non-crimp polymer(s). synthetic(s) such as oxidized regenerated cellulose. Alternatively, the 20086 crimped fibers and the 20084 non-crimped fibers may comprise the same polymeric composition.

[000411] As described herein, crimped fibers 20086 and non-crimped fibers 20084 can be gripped together, e.g. by needle punching, thermowelding, hydroentangling, ultrasonic pattern bonding, chemical bonding and melt blow bonding. The 20086 crimp fibers that comprise synthetic polymers such as "VICRYL (polyglactic 910)" and the 20084 non-crimp fibers that comprise oxidized regenerated cellulose can be needle-punched together to form the 20080 non-woven material. The 20080 non-woven material may comprise approximately 5% to 50% by weight of "VICRYL crimped (polyglactic 910)" 20086 fibers and approximately 5% to 50% by weight of non-crimped oxidized regenerated cellulose (ORC) 20084 fibers, for example. When the 20080 non-woven material comes into contact with the T fabric, the 20084 non-crimped ORC fibers can rapidly react with the plasma in the fabric to form a gelatinous mass, for example. The formation of the gelatinous ORC mass can be instantaneous or nearly instantaneous with tissue contact. Additionally, after formation of the gelatinous ORC mass, the 20086 crimp "VICRYL (polyglactic 910)" fibers may remain dispersed throughout the 20080 non-woven material. For example, the 20086 crimp fibers may be suspended in the gelatinous ORC mass. As the gelatinous ORC mass is bioabsorbed, the crimped "VICRYL (polyglactic 910)" 20086 fibers can exert a flexing force on adjacent tissue, as described in more detail herein. Additionally, the fabric can begin to cure around the "VICRYL (polyglactic 910)" fibers and/or the formed staples 30030, also as described in greater detail herein.

[000412] Referring primarily to Figures 78 to 81, the support portion 20010 of the staple cartridge 20000 may comprise a cartridge body 20017, a top platform surface 20011, and a plurality of staple cavities 20012. Each staple cavity 20012 may define an entry in the platform surface 20011. A clip 20030 may be removably positioned in a clip cavity 20012. In accordance with the invention, a single clip 20030 is disposed in each clip cavity 20012. Figures 82 and 83 and similar to the clips described herein, each clip 20030 may comprise a base 20031 that has a first end 20035 and a second end 20036. A clip leg 20032 may extend from the first end 20035 of the base 20031 and another leg of clip 20032 may extend from the second end 20036 of base 20031. Again with reference to Figures 78 to 81, prior to positioning of clips 20030, the tab 20030 20031 of each staple 20030 may be supported by a staple driver 20040 positioned within the rigid support portion 20010 of the staple cartridge 20000. Also prior to positioning of the staples 20030, the legs 20032 of each staple 20030 may be at least partially contained within a 20012 clamp cavity.

[000413] 20030 clamps can be installed between a home position and a triggered position. For example, referring primarily to Figure 81, the 20030 staples can be in a home position (20030e, 20030f staples), a partially fired or intermediate position (20030c, 20030d staples), or a fired position (20030a, 20030b staples). A 20040 trigger can drive the clamps between the home position and the triggered position. For example, the base 20031 of each clamp 20030 may be supported by a driver 20040. The legs 20032 of a clamp (clamps 20030e, 20030f in Figure 80, for example) may be positioned within a clamp cavity 20012. trigger element or staple trigger slide 20050 translates from the proximal end 20001 to the distal end 20002 of the 20000 staple cartridge, an inclined surface 20051 on the slide holder 20050 may contact an inclined surface 20042 on a 20040 driver to position the clamp 20030 positioned above the contacting driver 20040. The clamps 20030 can be installed between a home position and a fired position so that the legs 20032 move along the nonwoven material 20080 of the fabric thickness compensator 20020, penetrate on the top surface 20021 of the fabric thickness compensator 20020, penetrate the fabric T and contact an anvil 20060 (Fig. a 61) positioned opposite the staple cartridge 20000 on the end actuator 12. The staple legs 20032 can be deformed against the anvil 20060 and the legs 20032 of each staple 20030 can capture a portion of the nonwoven material 20080 and a portion of the T fabric

[000414] In the fired configuration (Figures 82 and 83), each staple 20030 can apply a compressive force to the fabric T and the fabric thickness compensator 20020 captured by the staple 20030. Referring primarily to Figures 80 and 81, the legs 20032 of each staple 20030 may be deformed downwardly towards the base 20031 of the staple 20030 to form a staple gripping area 20039. The staple gripping area 20039 may be the area in which the fabric T and the thickness compensator of fabric 20020 can be captured by a fired staple 20030. In various circumstances, the staple gripping area 20039 can be defined between the inner surfaces of deformed legs 20032 and the inner surface of the base 20031 of a staple 20030. The size of the area 20039 clamping rate for a 20030 clamp may depend on a number of factors, such as the length of the legs, the diameter of the legs, the width of the base, and/or the extent to which the legs are deformed. ada, for example.

[000415] Optionally, when a non-woven material 20080 is captured in a staple gripping area 20039, the captured portion of the non-woven material 20080 may be compacted. The compacted height of nonwoven material 20080 captured in a staple gripping area 20039 may vary within the staple cartridge 20000 depending on the T fabric in that same staple gripping area 20039. For example, where the T fabric is thinner, the 20039 staple gripping area may have more room for the 20080 non-woven material and as a result the 20080 non-woven material may not be as compacted as it would be if the T fabric were thicker. Where the T fabric is thicker, the 20080 non-woven material can be compressed further to accommodate the thicker T fabric, for example. For example, with reference to Figure 82, the nonwoven material 20080 can be compacted to a first height in a first staple gripping area 20039a, a second height in a second staple gripping area 20039b, a third height in a third staple gripping area 20039c, a fourth height at a fourth staple gripping area 20039d, and a fifth height at a fifth staple gripping area 20039e, for example. Similarly, as illustrated in Figure 83, the nonwoven material 20080 can be compacted to a first height in the first staple gripping area 20039a, a second height in the second staple gripping area 20039b, a third height in the third gripping area. clamp grip 20039c and a fourth height in the fourth clamp grip area 20039d. Alternatively, the compacted height of the 20080 non-woven material can be uniform across the 20010 staple cartridge.

[000416] Optionally, an applied force can move the 20080 nonwoven material from an initial uncompacted configuration to a compacted configuration. Additionally, the non-woven material 20080 can be resilient so that, when compacted, the non-woven material 20080 can generate a flexing or restoring force. When deformed, the 20080 non-woven material may seek to recover from the compressed or deformed configuration. As the 20080 nonwoven material seeks to recover, it may exert a flexing or restoring force on the tissue also captured in the 30039 staple grip area, as described in more detail in this document. When the applied force is subsequently removed, the restoring force can cause the nonwoven material to recover to the compacted configuration. The 20080 nonwoven material can recover to the initial uncompacted configuration or can recover to a configuration substantially similar to the initial uncompacted configuration. The deformation of the 20080 non-woven material can be elastic. The deformation of the non-woven material can be partially elastic and partially plastic.

[000417] When a portion of the non-woven material 20080 is compacted in a staple gripping area 20039, the crimped fibers 20086 in that portion of the non-woven compensator 20039 may also be compacted or otherwise deformed. The amount of deformed crimped fiber 20086 may correspond to the amount by which the captured portion of the non-woven material 20080 is compacted. For example, with reference to Figure 63, nonwoven material 20080 may be captured by means of installed staples 20030. Where nonwoven material 20080 is more compacted by an installed staple 20030, the average strain of crimped fibers 20086 may be greater. Additionally, where the nonwoven material 20080 is less compacted by an installed staple, the average strain of crimped fibers 20086 may be less. Similarly, with reference to Figures 82 and 83, in a staple gripping area 20039d in which the nonwoven material 20080 is most compacted, the crimped fibers 20086 in that staple gripping area 20039d may be, on average, more deformed . Additionally, in a staple gripping area 20039a in which the nonwoven material 20080 is less compacted, the crimped fibers 20086 in that staple gripping area 20039a can be, on average, less deformed.

[000418] The ability of the non-woven material 20080 to recover from the deformed configuration, that is, the resilience of the non-woven material 20080, may be a function of the resilience of the crimped fibers 20086 in the non-woven material 20080. The crimped fibers 20086 can be deform elastically. The deformation of the crimped fibers 20086 can be partially elastic and partially plastic. Optionally, the compaction of each 20086 crimp fiber can cause the 20086 compacted crimp fibers to generate a flexing or restoring force. For example, 20086 compacted crimp fibers can generate restoring force as 20086 fibers seek to recover from their compacted configuration. 20086 fibers can seek to return to their initial uncompressed configuration or to a configuration substantially similar to it. 20086 crimped fibers may seek to partially return to their initial configuration. Optionally, only a portion of the crimped fibers 20086 in the nonwoven material 20080 may be resilient. When a 20086 crimp fiber is comprised of a linear elastic material, the restoring force of the 20086 compacted crimp fiber can be a function of the amount by which the 20086 crimp fiber is compacted and the spring coefficient of the 20086 crimp fiber, for example . The spring coefficient of the crimped fiber 20086 may depend at least on the orientation, material, shape and/or size of the crimped fiber 20086, for example.

[000419] The crimped fibers 20086 in the non-woven material 20080 can comprise a uniform spring coefficient. Alternatively, the spring coefficient of the crimped fibers 20086 in the nonwoven material 20080 may vary. When a 20086 crimp fiber that has a large spring coefficient is compacted to large measures, the 20086 crimp fiber can generate a large restoring force. When a 20086 crimped fiber that has the same large spring coefficient is less compacted, the 20086 crimped fiber can generate a lower restoring force. The aggregate of restoring forces generated by crimped fibers compacted 20086 in non-woven material 20080 can generate a combined restoring force along non-woven material 20080 of fabric thickness compensator 20020. Non-woven material 20080 can exert the restoring force combined over the T fabric captured by a staple fired 20030 with the compacted non-woven material 20080.

[000420] Furthermore, the number of crimped fibers 20086 per unit volume of 20080 non-woven material can affect the spring coefficient of 20080 non-woven material. For example, resilience in a 20080 non-woven material can be low when the number of crimped fibers 20086 per unit volume of non-woven material 20080 is low, for example; the resilience of the nonwoven material 20080 may be higher when the number of crimped fibers 20086 per unit volume of nonwoven material 20080 is higher, for example; and the resilience of the nonwoven material 20080 can be even higher when the number of crimped fibers 20086 per unit volume of nonwoven material 20080 is even higher, for example. When the resilience of the 20080 non-woven material is low, such as when the number of crimped fibers 20086 per unit volume of 20080 non-woven material is low, the combined restoring force exerted by the 20020 fabric thickness compensator on the captured fabric T can also be low. When the resilience of the 20080 non-woven material is higher, such as when the number of crimped fibers 20086 per unit volume of 20080 non-woven material is higher, the aggregate restoring force exerted by the 20020 fabric thickness compensator on the captured fabric T can also be higher.

[000421] Referring primarily to Figure 64, a non-woven material 20080' of a fabric thickness compensator 20020' may comprise a therapeutic agent 20088, such as a drug and/or pharmaceutically active agent, for example. The non-woven material 20080' can release a therapeutically effective amount of the therapeutic agent 20088. For example, the therapeutic agent 20088 can be released as the non-woven material 20080' is absorbed. The therapeutic agent 20088 can be released into fluid, such as blood, for example, by passing over or through the non-woven material 20080'. Examples of therapeutic agents 20088 may include, but are not limited to, hemostatic agents and drugs such as, for example, fibrin, thrombin and/or oxidized regenerated cellulose (ORC); anti-inflammatory drugs such as, for example, diclofenac, aspirin, naproxen, sulindac and/or hydrocortisone; antibiotic and antimicrobial drugs or agents such as, for example, triclosan, ionic silver, ampicillin, gentamicin, polymyxin B and/or chloramphenicol; and anti-cancer agents such as, for example, cisplatin, mitomycin and/or adriamycin. The therapeutic agent 20088 may comprise a biological agent, such as a stem cell, for example. The fibers 20082 of the nonwoven material 20080' may comprise the therapeutic agent 20088. Alternatively, the therapeutic agent 20088 may be added to the nonwoven material 20080' or otherwise integrated within the fabric thickness compensator 20020'.

[000422] Referring primarily to Figures 70 to 70B, a fabric thickness compensator 20520 for an end actuator 12 (Figure 61) may comprise a plurality of coiled springs or fibers 20586. Similar to crimped fibers 20086 described herein, the spiral wound fibers 20586 can be, for example, crimped, twisted, spiral wound, angled, bent, spiraled, curled and/or bowed within the fabric thickness compensator 20520. The spiral wound fibers 20586 can be wound around a mandrel to form a spiral or substantially spiral-like shape. The spiral wound fibers 20586 may be randomly oriented and/or randomly distributed along the fabric thickness compensator 20520. Alternatively, the spiral wound fibers 20586 may be systematically arranged and/or evenly distributed along the fabric thickness compensator. 20520. For example, with reference to Figure 70, the spiral wound fibers 20586 may comprise a longitudinal axis between a first end 20587 and a second end 20589 of the spiral wound fiber 20586. The longitudinal axes of the spiral wound fibers 20520 in the compensator of fabric thickness 20520 may be parallel or substantially parallel. The first end 20587 of each spiral wound fiber 20520 may be positioned along a first longitudinal side 20523 of the fabric thickness compensator 20520 and the second end 20589 of each spiral wound fiber 20586 may be positioned along a second side longitudinal 20524 of the fabric thickness compensator 20520. In such an arrangement, the spiral wound fibers 20586 may laterally traverse the fabric thickness compensator. Alternatively, the spiral wound fibers 20586 may run longitudinally or diagonally through the fabric thickness compensator 20520.

[000423] Optionally, similar to the crimped fibers 20086 described herein, the spiral wound fibers 20586 may comprise a polymeric composition. The crimped fibers 20586 may be at least partially elastic so that the deformation of the crimped fibers 20586 generates a restoring force. The polymer composition of the spiral wound fibers 20586 may comprise polycaprolactone (PCL), for example, so that the spiral wound fibers 20586 are not soluble in a chlorophyll solvent. Referring to Figure 70A, the springs or spiral wound fibers 20520 can be retained in a 20580 offset material. The 20580 offset material can retain the spiral wound fibers 20586 in a loaded position so that the spiral wound fibers 20586 exert a flexing load on or within the 20580 plywood material. The 20580 plywood material can hold the spiral wound fibers 20586 in a neutral position, wherein the spiral wound fibers 20586 do not exert a flex load on or within the 20580 offset material. The 20580 offset material may be bioabsorbable and, in some cases, may comprise a foam such as poly(glycolic acid) (PGA) foam. Furthermore, the 20580 offset material may be soluble in a chlorophyll solvent, for example. The fabric thickness compensator may comprise spiral wound fibers 20586 comprising polycaprolactone (PCL) and the compensating material 20580 comprising poly(glycolic acid) (PGA) foam, for example, so that the fibers wound in spiral 20520 are not soluble in a chlorophyll solvent although the 20580 make-up material is soluble in the chlorophyll solvent. Compensation material 20580 may be at least partially elastic so that compaction of compensation material 20580 generates a restoring force. Additionally, referring to Figure 70B, the compensation material 20580 of the tissue thickness compensator 20520 may comprise a therapeutic agent 20588, such as stem cells, for example. The 20580 make-up material can release a therapeutically effective amount of the 20588 therapeutic agent as the 20580 make-up material is absorbed.

[000424] Similar to the fabric thickness compensator 20020 described herein, the fabric thickness compensator 20520 may be compressible. For example, as staples 20030 (Figures 78 to 81) are installed from a home position to a fired position, staples 20030 may engage a fabric thickness compensator portion 20520. In accordance with the invention, a staple 20030 can capture a portion of the fabric thickness compensator 20520 and the adjacent fabric T. The clamp 20030 can apply a compressive force to the captured portion of the fabric thickness compensator 20520 and the fabric T such that the fabric thickness compensator 20520 be compressed from an uncompacted height to a compacted height. Compaction of the fabric thickness compensator 20520 can result in a corresponding deformation of the spiral wound fibers 20586 therein. As described in more detail in this document, the deformation of each spiral-wound fiber 20586 can generate a restoring force that may depend on the resilience of the spiral-wound fiber, for example, the amount by which the spiral-wound fiber 20586 is and/or the spring coefficient of the spiral wound fiber 20586. The spring coefficient of the spiral wound fiber 20586 may depend at least on the orientation, material, shape and/or size of the spiral wound fiber 20586, for example example. The deformation of the spiral wound fibers 20586 in the fabric thickness compensator 20520 can generate restoring forces along the fabric thickness compensator 20520. The fabric thickness compensator 20520 can exert the aggregate restoring force generated by the spiral wound fibers deformed 20586 and/or resilient compensation material 20586 in the captured fabric T in the fired staples 20030.

[000425] Referring primarily to Figures 71 and 72, a fabric thickness compensator 20620 for an end actuator 12 may comprise a plurality of spring coils 20686. Similar to crimped fibers 20086 and spiral wound fibers 20586 described herein, spring coils 20686 can be, for example, crimped, twisted, spiral wound, bent, bent, coiled, curled and/or bowed in fabric thickness compensator 20620. Optionally, similar to fibers and spirals described herein, coil springs 20686 may comprise a polymeric composition. Additionally, spring coils 20686 may be at least partially elastic so that deformation of spring coils 20686 generates a restoring force. Spring coils 20686 may comprise a first end 20687, a second end 20689 and a longitudinal axis therebetween. Referring to Figure 71, the first end 20686 of a coil of spring 20686 can be positioned on or near a proximal end 20626 of the tissue thickness compensator and the second end 20689 of the same coil of spring 20686 can be positioned over or proximate to a distal end 20625 of the fabric thickness compensator 20620 so that the spring coil 20686 longitudinally traverses the fabric thickness compensator 20620, for example. Alternatively, the spiral wound fibers 20686 may cross laterally or diagonally through the fabric thickness compensator 20620.

[000426] Fabric thickness compensator 20620 may comprise an outer film 20680 that at least partially surrounds at least one coil of spring 20686. Referring to Figure 71, outer film 20680 may extend around the perimeter of multiple spring coils 20686 in fabric thickness compensator 20620. Alternatively, outer film 20680 may completely encapsulate spring coils 20686 or at least one spring coil 20686 in fabric thickness compensator 20620. Outer film 20680 may retain the coils spring 20686 on end actuator 12. Outer film 20680 may retain spring coils 20686 in a loaded position so that spring coils 20686 generate a flexing load and exert a flexing force on outer film 20680. Alternatively , outer film 20680 can retain spring coils 20686 in a neutral position. The fabric thickness compensator 20620 may also comprise a filler material 20624. The filler material 20624 may be retained within and/or around the spring coils 20686 by the outer film 20680. The filler material 20624 may comprise an agent. 20688, similar to the therapeutic agents described herein. Additionally, infill material 20624 may support spring coils 20686 in fabric thickness compensator 20620. Infill material 20624 may be compressible and at least partially resilient so that infill material 20624 contributes to the flexing force or of restoration generated by the 20620 Tissue Thickness Compensator, as described in more detail- in this document.

[000427] Similar to the fabric thickness compensators described herein, the fabric thickness compensator 20620 may be compressible. As the staples 20030 (Figures 78 to 81) are installed from a home position to a fired position, the staples 20030 can engage a portion of the fabric thickness compensator 20620. Optionally, each staple 20030 can capture a portion of the fabric thickness compensator 20620. fabric thickness 20620 together with adjacent fabric T. Clip 20030 may apply a compressive force to the captured portion of fabric thickness compensator 20620 and captured fabric T such that fabric thickness compensator 20620 is compacted between a height uncompressed and a compressed height. Compaction of the fabric thickness compensator 20620 can result in corresponding deformation of the spring coils 20686 retained therein (Figure 72). As described in more detail in this document, the deformation of each of the spring coils 20686 can generate a restoring force that depends on the resilience of the spring coil 20686, for example, the amount by which the spring coil 20686 is deformed and/or or the spring coefficient of the spring coil 20686. The spring coefficient of a spring coil 20686 may depend at least on the material, shape, and/or dimensions of the spring coil 20686, for example. Furthermore, depending on the resilience of the 20624 infill material and 20680 outer film, compaction of 20624 infill material and/or 20680 outer film can also generate restoring forces. The aggregate of restoring forces generated by at least the deformed spring coils 20686, the filler material 20624, and/or the outer film 20680 in the fabric thickness compensator 20620 can generate restoring forces along the fabric thickness compensator 20620. The fabric thickness compensator 20620 can exert the aggregate restoring force generated by the deformed spring coils 20686 on the captured fabric T in a fired staple 20030.

[000428] Optionally, referring primarily to Figures 73 to 75, a fabric thickness compensator 20720 for an end actuator 12 may comprise a plurality of spring coils 20786. Similar to the spiral wound fibers and springs herein described, spring coils 20786 can be, for example, crimped, twisted, spiral wound, bent, bent, coiled, curled and/or bowed in fabric thickness compensator 20720. Spring coils 20786 can be at least partially elastic so that the deformation of the 20786 spring coils generates a restoring force. Additionally, spring coils 20786 may comprise a first end 20787, a second end 20789 and a longitudinal axis therebetween. Referring primarily to Figure 75 , the first end 20787 of the spring coil 20786 can be positioned on or near the proximal end 20726 of the fabric thickness compensator 20720 and the second end 20789 of the spring coil 20786 can be positioned on or close to the distal end 20725 of fabric thickness compensator 20720 so that spring coil 20786 crosses longitudinally through fabric thickness compensator 20720. Spring coil 20786 can extend longitudinally in two parallel rows on fabric thickness compensator 20720 Fabric thickness compensator 20720 may be positioned on an end actuator 12 so that a sliding support 20050 (Figure 61) or cutting element 20052 can translate along a slot 20015 between parallel rows of spring coils 20786. Alternatively, 20786 spring coils can cross laterally or diagonally through the thickness compensator. the fabric 20720.

[000429] Again with reference to Figure 75, spring coils 20786 may be retained or incorporated into a 20780 offset material. The 20780 offset material may be bioabsorbable and, in some cases, may comprise a foam such as, for example, a poly(glycolic acid) (PGA) foam. The offset material 20780 may be resilient so that the deformation of the offset material 20780 generates a flexing force. The 20780 offset material may be soluble in a chlorophyll solvent, for example. For example, the fabric thickness compensator may comprise spring coils 20786 comprising polycaprolactone (PCL) and compensating material 20780 comprising poly(glycolic acid) (PGA) foam so that spring coils 20786 are not soluble. in a chlorophyll solvent although the 20780 make-up material is soluble in a chlorophyll solvent, for example. The compensating material 20780 may be at least partially resilient so that the deformation of the compensating material 20780 generates a flexing load or restoring force.

[000430] Fabric thickness compensator 20720 may comprise braided strands 20790, which can extend between parallel rows of spring coils 20786. For example, with reference to Figure 75, a first braided yarn 20790 can cross diagonally the two parallel rows of coiled springs 20786 and a second braided strand 20790 can also diagonally cross the two parallel rows of coiled springs 20786. The first and second braided strands 20790 can cross. The braided strands 20790 can cross multiple times along the length of the fabric thickness compensator 20720. The braided strands 20790 can retain the spring coils 20786 in a loaded configuration so that the spring coils 20786 are retained in a substantially flat on the fabric thickness compensator 20720. The braided strands 20790 passing through the fabric thickness compensator 20720 can be directly attached to the spring coils 20786. Alternatively, the braided strands 20790 can be coupled to the spring coils 20786 via a bracket 20792 that extend through each spring coil 20786 along the longitudinal axis thereof.

[000431] As described in more detail in this document, a staple cartridge 20000 may comprise a slot 20015 configured to receive a sliding translational support 20050 comprising a cutting element 20052 (Figure 61). As the sliding support 20050 translates along the slot 20015, the sliding support 20050 can eject staples 20030 from fastener cavities 20012 in the staple cartridge 20000 and the cutting element 20052 can simultaneously or nearly simultaneously retract the fabric T. Again with reference to the Figure 75, as the cutting element 20052 translates, it can also spread the interwoven strands 20790 that cross between the parallel rows of spring coils 20786 in the fabric thickness compensator 20720. As the braided strands 20790 are separated, each coil spring coil 20786 can be released from its loaded configuration so that each spring coil 20786 returns from a substantially flat loaded position to an expanded position on fabric thickness compensator 20720. Optionally, when a spring coil 20786 is expanded, the spring material 20780 offset that surrounds the 20786 spring coil can also expand.

[000432] Optionally, as the 20030 staples (Figures 78 to 81) are installed from a home position to a fired position, the 20030 staples can engage a portion of the 20720 Fabric Thickness Compensator and the 20720 Fabric Thickness Compensator may expand, or attempt to expand, within the staples 20030 and may apply a compressive force to the fabric T. Optionally, at least one staple 20030 may capture a portion of the fabric thickness compensator 20720 along with the fabric adjacent T. Clip 20030 may apply a compressive force to the captured portion of the fabric thickness compensator 20720 and the captured fabric T such that the fabric thickness compensator 20720 is compacted between an uncompacted height and a compacted height. Compaction of the fabric thickness compensator 20720 can result in corresponding deformation of the spring coils 20786 and the compensation material 20780 retained therein. As described in more detail in this document, the deformation of each of the spring coils 20786 can generate a restoring force that may depend on the resilience of the spring coil, for example, the amount by which the spring coil 20786 is deformed. and/or the spring coefficient of the spring coil 20786. The spring coefficient of a spring coil 20786 may depend at least on the orientation, material, shape and/or size of the spring coil 20786, for example. The aggregate of restoring forces generated by at least the deformed spring coils 20786 and/or compensating material 30380 in the fabric thickness compensator 20720 can generate restoring forces along the fabric thickness compensator 20720. fabric 20720 can exert the aggregate restoring force generated by deformed spring coils 20786 on fabric thickness compensator 20720 on captured fabric T and fired staples 20030.

[000433] Optionally, referring primarily to Figures 76 and 77, a tissue thickness compensator 20820 for a surgical end actuator 12 may comprise a spring coil 20886. Similar to the fibers and coils described herein, the coil spring 20886 may be, for example, crimped, twisted, spiral wound, bent, bent, spiraled, curled and/or bowed in fabric thickness compensator 20820. Spring spiral 20886 may comprise a polymeric composition and may be at least less partially elastic, so that the deformation of the spring coil 20886 generates a flexing force. Additionally, the spring coil 20886 may comprise a first end 20887 and a second end 20889. Referring to Figure 76, the first end 20887 may be positioned on or near the proximal end 20826 of the fabric thickness compensator 20820 and the second end 20889 may be positioned on or near the distal end 20825 of the 20820 fabric thickness compensator. The spring coil 20886 may coil or snake from the proximal end 20825 to the distal end 20826 of the 20820 fabric thickness compensator.

[000434] Again with reference to Figure 76, the spring coil 20886 may be retained or incorporated into a compensation material 20880. The compensation material 20880 may be bioabsorbable and, in some cases, may comprise a foam such as, for example, poly(glycolic acid) (PGA) foam. The 20880 offset material may be soluble in a chlorophyll solvent, for example. The fabric thickness compensator may comprise spring coils 20886 comprising polycaprolactone (PCL) and compensating material 20880 comprising poly(glycolic acid) (PGA) foam, for example, so that spring coil 20886 is not soluble in a chlorophyll solvent although the 20880 make-up material is soluble in a chlorophyll solvent. The compensating material 20880 may be at least partially resilient so that the deformation of the compensating material 20880 generates a flexing load or restoring force.

[000435] Similar to the fabric thickness compensators described herein, for example, the fabric thickness compensator 20820 may be compressible. Compaction of the fabric thickness compensator 20820 can result in a deformation of at least a portion of the spring coil 20886 retained or incorporated into the compensation material 20880 of the fabric thickness compensator 20820. As described in more detail in this document, the deformation of Coil Spring 20886 can generate restoring forces which may depend on the resilience of Coil Spring 20886, the amount by which Coil Spring 20886 is deformed and/or the spring coefficient of Coil Spring 20886, for example. The aggregate of restoring forces generated by the deformed spring coil 20886 and/or the deformed compensation material 20880 can generate restoring forces along the fabric thickness compensator 20820. The fabric thickness compensator 20820 can exert the restoring force aggregated over the captured tissue T on the fired staples 20030.

[000436] Now referring to Figure 84, a surgical end actuator 12 may comprise a tissue thickness compensator 30020 which has at least one tubular member 30080. The tissue thickness compensator 30020 may be retained on the end actuator 12. As described in more detail in this document, a fastener on the end actuator 12 can be installed so that the fastener moves to a triggered position and deforms at least a portion of the tubular member 30080 in the fabric thickness compensator 30020 The reader will note that tissue thickness compensators comprising at least one tubular member as described herein may be installed or otherwise engaged with a variety of surgical end actuators and that these are within the scope of the invention. present revelation.

[000437] Optionally, still referring to Figure 84, the fabric thickness compensator 30020 can be positioned relative to the anvil 30060 of the end actuator 12. Alternatively, the fabric thickness compensator 30020 can be positioned relative to a fastener cartridge assembly, such as the 12 End Actuator 30000 Staple Cartridge. The 30000 Staple Cartridge can be configured to fit into a 30072 Cartridge Chute of a 30070 End Actuator Jaw 12. For example, fabric thickness compensator 30020 may be releasably secured to staple cartridge 30000. Tubular member 30080 of fabric thickness compensator 30020 may be positioned adjacent a top platform surface 30011 of a rigid support portion 30010 of the staple cartridge 30000. The tubular member 30080 may be secured to the top platform surface 30011 by means of an adhesive or by a shell, similar to fur. at least one of the housings described herein (eg, Figure 16). Fabric thickness compensator 30020 may form a single piece with an assembly comprising staple cartridge 30000 so that staple cartridge 30000 and fabric thickness compensator 30020 are formed as a unitary construction. For example, staple cartridge 30000 may comprise a first body portion, such as rigid support portion 30010 and a second body portion, such as fabric thickness compensator 30020, for example.

[000438] Referring to Figures 84 to 86, the tubular member 30080 in the tissue thickness compensator 30020 may comprise an elongate portion 30082 that has at least one lumen 30084 extending at least partially therethrough. Referring primarily to Figure 86, the elongated portion 30082 of the tubular member 30080 may comprise woven or braided cords 30090, as described in greater detail herein. Alternatively, elongate portion 30082 may comprise a solid structure, such as a polymeric extrusion, rather than woven strands 30090. Elongate portion 30082 of tubular member 30080 may comprise a thickness. The thickness of the elongate portion 30082 can be substantially uniform along the length and around the diameter thereof; in other cases, the thickness may vary. The elongate portion 30082 may be elongated so that the length of the elongate portion 30082 is greater than the diameter of the elongate portion 30082, for example. The elongated portion may comprise a length of approximately 3.05 centimeters to approximately 6.60 centimeters (approximately 1.20 inches to approximately 2.60 inches) and a diameter of approximately 0.25 centimeters to approximately 0.38 centimeters (approximately 0 .10 inch to approximately 0.15 inch), for example. The length of the tubular element 20080 can be approximately 3.56 centimeters (1.40 inches), for example, and the diameter of the tubular element 20080 can be approximately 0.318 centimeters (0.125 inches), for example. Furthermore, the elongated portion 30082 may define a substantially circular or elliptical cross-sectional shape, for example. Alternatively, the cross-sectional shape may comprise a polygonal shape such as, for example, a triangle, a hexagon and/or an octagon. Referring again to Figure 84, tubular member 30080 may comprise a first distal end 30083 and a second proximal end 30085. The cross-sectional shape of the elongate portion 30082 may taper at the first and/or second end 30083, 30085, wherein at least one end 30083, 30085 of the tubular member 30080 may be closed and/or sealed. Alternatively, a lumen 30084 may continue through the distal ends 30083, 30085 of the tubular member 30080 so that the ends 30083, 30085 are open.

[000439] The tubular member 30080 may comprise a single central lumen 30084 that extends at least partially through the elongate portion 30084. The lumen 30084 may extend through the entire length of the elongate portion 30084. As a further alternative, the tubular member 30080 may comprise multiple lumens 30084 extending therethrough. Lumens 30084 extending through tubular member 30080 may be circular, semi-circular, wedge-shaped, and/or combinations thereof. In accordance with the invention, a tubular member 30080 may also comprise support mats which may form a modified "T" or "X" shape, for example, within the lumen 30084. Dimensions, lumen(s) ) and/or the support blanket(s) on the tubular element 30080 may define the cross-sectional shape of the tubular member 30080. The cross-sectional shape of the tubular member 30080 may be consistent along its length or, alternatively, the cross-sectional shape of the tubular member 30080 may vary along its length. As described in more detail in this document, the cross-sectional shape of the tubular member 30080 can affect the compressibility and resilience of the tubular member 30080.

[000440] The tubular element 30080 may comprise a vertical diameter and a horizontal diameter; the dimensions thereof may be selected depending on the arrangement of the tubular element 30080 in the end actuator 12, the dimensions of the end actuator 12, including the fabric gap of the end actuator 12, and the likely geometry of the clamp gripping areas 30039. For example, the vertical diameter of the tubular member 30080 may be related to the likely height of a formed clamp. In such cases, the vertical diameter of the tubular element 30080 can be selected so that the vertical diameter can be reduced from approximately 5% to approximately 20% when the tubular element 30080 is captured by a formed clamp 30030. For example, a tubular element 30080 having a vertical diameter of approximately 0.254 centimeters (0.100 inches) may be used for staples having an expected formed height of approximately 0.20 centimeters to approximately 0.24 centimeters (approximately 0.080 inches to approximately 0.095 inches). As a result, the vertical diameter of the tubular member 30080 can be reduced from approximately 5% to approximately 20% when captured by the formed clamp 30030 even when no T-fabric is captured therein. When the fabric T is captured by the formed clamp 30030, the compaction of the tubular member 30080 can be even greater. The vertical diameter may be uniform along the length of the tubular member 30080 or, alternatively, the vertical diameter may vary along the length thereof.

[000441] The horizontal diameter of the tubular element 30080 may be greater than, equal to or less than the vertical diameter of the tubular element 30080 when the tubular element 30080 is in an undeformed or recovered configuration. For example, with reference to Figure 85, the horizontal diameter can be approximately three times larger than the vertical diameter, for example. The horizontal diameter may be approximately 10 mm (0.400) and the vertical diameter may be approximately 3.18 mm (0.125 inches), for example. Alternatively, now referring to Figure 87, the horizontal diameter of a collapsible tube 31080 may be equal to or substantially equal to the vertical diameter of the tubular member 31080 when the tubular member 31080 is in an undeformed or recovered configuration. The horizontal diameter may be approximately 3.18 mm (0.125 inches) and the vertical diameter may also be approximately 3.18 mm (0.125 inches), for example. The tubular member 30080 may comprise a vertical diameter of approximately 0.32 centimeters (0.125 inches), a horizontal diameter of approximately 1.01 centimeters (0.400 inches), and a length of approximately 3.6 centimeters (1.400 inches). As described in more detail in this document, when a force A is applied to the tubular member 30080 and/or 31080, the tubular member may deform so that the cross-sectional geometry, including the horizontal and vertical diameters, may change.

[000442] Again with reference to Figures 84 to 86, the tubular element 30080 in the fabric thickness compensator 30020 may be deformable. The entire tubular element 30080 can be deformable. For example, tubular member 30080 may be deformable from proximal end 30083 to distal end 30085 of elongate portion 30082 and around the entire circumference thereof. Alternatively, only a portion of the tubular member 30080 may be deformable. For example, only an intermediate length of the elongate portion 30082 and/or only a portion of the circumference of the tubular member 30080 can be deformable.

[000443] When a compressive force is applied to a point of contact on the elongated portion 30082 of the tubular element 30080, the point of contact may shift, which can change the cross-sectional dimensions of the tubular element 30080. For example, again Referring to Figure 85, tubular member 30080 may comprise a top apex 30086 and a base apex 30088 at elongated portion 30082. In the initial undeformed configuration, tubular member 30080 may comprise undeformed cross-sectional dimensions, including a diameter undeformed vertical between top apex 30086 and base apex 30088. When a compressive force A is applied to butt apex 30086, tubular member 30080 may move into a deformed configuration. In the deformed configuration, the cross-sectional dimensions of the 30080 tube can be changed. For example, the tube 30086 may comprise a deformed vertical diameter between the top apex 30086 and the base apex 30088, which may be smaller than the undeformed vertical diameter. Referring to Figure 87, the horizontal diameter of the deformed tube 30080 can be elongated, for example, when the tubular member 30080 moves from an undeformed configuration to a deformed configuration. The deformed cross-sectional dimensions of the deformed tube 30080 may depend at least on the position, angular orientation and/or magnitude of the applied force A. As described in more detail in this document, the deformation of a deformable tube 30080 can generate a bending force. or restoration which may depend on the resilience of the tubular element 30080.

[000444] Still referring to Figure 85, the tubular element 30080 can generate a flexing or restoring force when compacted. In such cases, as described herein, the tubular member 30080 may move from an initial undeformed configuration to a deformed configuration when a force A is applied to a point of contact on the elongated portion 30082 of the tubular member 30080. applied A is removed, the deformed tube 30080 can recover from the deformed configuration. The deformed tube 30080 can recover to the initial undeformed configuration or can recover to a configuration substantially similar to the initial undeformed configuration. The ability of the tubular element 30080 to recover from a deformed configuration is related to the resilience of the tubular element 30080.

[000445] Again with reference to Figure 85, a tubular element 30080 can exert a flexing or restoring force. Restoration force can be generated by the tubular element 30080 when an applied force A is exerted on the tubular element 30080, for example, by a clamp 30030 (Figures 88 and 89), as described in more detail in this document. An applied force A can change the cross-sectional dimensions of the tubular member 30080. Furthermore, in linear elastic materials, the restoring force of each deformed portion of the tubular member 30080 can be a function of the deformed dimensions of the tubular member 30080 and the coefficient of force. spring of that portion of the tubular member 30080. The spring coefficient of a collapsible tube 30080 may depend at least on the orientation, material, cross-sectional geometry, and/or dimensions of the tubular member 30080, for example. The tubular member 30080 in a fabric thickness compensator 30020 may comprise a uniform spring coefficient. Alternatively, the spring coefficient can vary along the length and/or around the diameter of the tubular member 30080. When a portion of a collapsible tube 30080 that has a first spring coefficient is compressed to large extents, the tubular member 30080 can generate a great restoring force. When a portion of the tubular element 30080 that has the same first coefficient as the spring is compressed to a lesser extent, the tubular element 30080 can generate a lower restoring force.

[000446] Referring again to Figure 84, the tubular element 30080 in the fabric thickness compensator 30020 may comprise a polymeric composition. The elongate portion 30082 of the tubular member 30080 may comprise the polymeric composition. Additionally, the polymeric composition may comprise an at least partially elastic material so that deformation of the tubular member 30080 generates a restoring force. The polymeric composition may comprise non-absorbable polymers, absorbable polymers or combinations thereof, for example. Examples of synthetic polymers include, but are not limited to, poly(glycolic acid) (PGA), poly(lactic acid) (PLA), polycaprolactone (PCL), polydioxanone (PDO) and copolymers thereof. Absorbable polymers may include bioabsorbable biocompatible elastomeric polymers, for example. Furthermore, the polymeric composition of the tubular member 30080 may comprise synthetic polymers, non-synthetic polymers or combinations thereof, for example. Optionally, similar to the polymeric compositions described elsewhere herein, the polymeric composition of the tubular member 30080 can include varying amounts of absorbable polymers, non-absorbable polymers, synthetic polymers and/or non-synthetic polymers, for example, by weight.

[000447] Referring to Figures 84 and 85, tubular member 30080 may comprise a therapeutic agent 30098 such as a pharmaceutically active agent or medicament, for example. The therapeutic agent 30098 may be retained in the lumen 30084 of the tubular member 30080. The elongate portion 30082 may encapsulate or partially encapsulate the therapeutic agent 30098. Additionally or alternatively, the polymeric composition of the elongate portion 30082 may comprise the therapeutic agent 30098 The tubular member 30080 can release a therapeutically effective amount of the therapeutic agent 30098. The therapeutic agent 30098 can be released as the tubular member 30080 is absorbed. For example, therapeutic agent 30098 can be released into fluid (such as blood) that passes over or through tubular member 30080. As a further alternative, therapeutic agent 30098 can be released when a clamp 30030 (Figures 88 and 89) pierces the tubular element 30080 and/or when the cutting element 30052 on the staple firing slide support 30050 (Figure 84) cuts a portion of the tubular element 30080, for example. Examples of 30098 therapeutics may include, but are not limited to, hemostatic agents and drugs such as, for example, fibrin, thrombin and/or oxidized regenerated cellulose (ORC), anti-inflammatory drugs such as, for example, diclofenac, aspirin, naproxen , sulindac and/or hydrocortisone, antibiotic and antimicrobial drugs or agents such as, for example, triclosan, ionic silver, ampicillinA, gentamicin, polymyxin B and/or chloramphenicol, anticancer agents such as, for example, cisplatin, mitomycin and/or or adriamycin, and/or biological agents such as stem cells.

[000448] Again with reference to Figures 84, 88 and 89, fasteners such as staples 30030, for example, can be installed from a staple cartridge 30000 so that staples 30030 engage a fabric thickness compensator 30020 and apply a force A to a tubular member 32080 therein. As described herein, the application of a force A to the tubular member 30080 can cause the tubular member 30080 to deform. Similar to the end actuators 12 described herein, the rigid support portion 30010 of the staple cartridge 30000 can comprise a cartridge body 30017, a platform surface 30011, and a plurality of clip cavities 30012 therein. Each clamp cavity 30012 may define an entry in the platform surface 30011 and a clamp 30030 may be removably positioned in a clamp cavity 30012 (Figure 104). Referring primarily to Figures 88 and 89, each clamp 30030 may comprise a base 30031 and two clamp legs 30032 extending from the base 30031. Prior to positioning of the clamps 30030, the base 30031 of each clamp 30030 may be supported by a staple driver 30040 (Figure 104) positioned within the rigid support portion 30010 of the staple cartridge 30000. Also prior to the positioning of the staples 30030, the legs 30032 of each staple 30030 may be at least partially contained within the clamp cavity. clamp 30012 (FIG 104).

[000449] Optionally, as described in more detail in this document, 30030 clamps can be installed between a home position and a triggered position. For example, a sliding staple firing bracket 30050 can engage a driver 30040 (Figure 104) to move at least one staple 30030 between the home position and the fired position. Referring primarily to Figure 88, the staple 30030 can be moved to a triggered position, where the legs 30032 of the staple 30030 engage a tubular member 32080 of a fabric thickness compensator 32020, penetrate the fabric T, and come into contact. with an anvil 30060 (Figure 104) positioned opposite the staple cartridge 30000 on the surgical end actuator 12. The staple forming pockets 30062 on the anvil 30060 can bend the staple legs 30032 so that the fired staple 30030 captures a portion of the tubular member 32080 and a portion of the fabric T in a staple gripping area 30039. As described in more detail herein, at least one staple leg 30032 can pierce the tubular member 32080 of the fabric thickness compensator 32020 when the staple 30030 move between the home position and the triggered position. Alternatively, the clamp legs 30032 can move around the perimeter of the tubular member 32080 so that the clamp legs 30032 prevent puncturing the tubular member 32080. Similar to the fasteners described herein, the legs 30032 of each clamp 30030 can be deformed downwardly towards the base 30031 of the clamp 30030 to form a clamp gripping area 30039 therebetween. The staple gripping area 30039 can be the area in which the fabric T and a portion of the fabric thickness compensator 32020 can be captured by a fired staple 30030. In the fired position, each staple 30030 can apply a compressive force to the fabric T and fabric thickness compensator 32020 captured in staple gripping area 30039 of staple 30030.

[000450] Still referring to Figure 88, when the tubular element 32080 is captured in a clamp gripping area 30039, the captured portion of the tubular element 32080 may be deformed, as described herein. Furthermore, the tubular member 32080 can be deformed to different deformed configurations in different staple gripping areas 30039 depending on, for example, the thickness, compressibility and/or density of the T-tissue captured in that same staple gripping area 30039. tubular member 32080 in fabric thickness compensator 32080 may extend longitudinally through successive staple gripping areas 30039. In such an arrangement, tubular member 32080 can be deformed to different deformed configurations in each staple gripping area 30039 along with along a row of fired staples 30030. Now referring to Figure 89, tubular elements 33080 in a fabric thickness compensator 33020 may be laterally disposed in staple gripping areas 30039 along a row of fired staples 30030. tubular elements 33080 can be retained by a flexible housing 33210. In such Under the arrangements, the tubular elements 33080 and the flexible housing 33210 can be deformed to different deformed configurations in each clamp gripping area 30039. For example, where the T fabric is thinner, the tubular elements 33080 can be less compacted and where the T fabric is thicker, the tubular elements 33080 may be more compacted to accommodate the thicker T fabric. Alternatively, the deformed dimensions of the tubular elements 33080 may be uniform across the entire length and/or width of the thickness compensator T. fabric 33020.

[000451] Referring to Figures 90 to 92, a tubular element 34080 in a fabric thickness compensator 34020 may comprise a plurality of strands 34090. Referring primarily to Figure 90, strands 34090 may be woven or braided forming a tubular lattice 34092 forming tubular member 34080. Tubular lattice 34092 formed by strands 34090 may be substantially hollow. The strands 34090 of the tubular member 34080 may be solid strands, tubular strands and/or other suitable shapes. For example, with reference to Figure 91, a single strand 34090 of tubular grating 34092 may be a tube. Referring to Figure 93, a wire 34090 may comprise at least one lumen 34094 extending therethrough. The number, geometry and/or dimensions of the 34094 lumens can determine the cross-sectional shape of the 34090 wire. For example, a 34090 wire may comprise circular lumen(s), semicircular lumen(s). ), wedge-shaped lumen(s) and/or combinations thereof. In accordance with the invention, a yarn 34090 may also comprise backing mats 34096 which may form a modified "T" or "X" shape, for example. At least the diameter of the 34090 wire, the lumen(s) extending therethrough, and the support mat(s) can characterize the cross-sectional shape of a 34090 wire. The cross-sectional shape of each 34090 wire, as discussed in more detail in this document, can affect the flexing or restoring force generated by the 34090 wire and the corresponding flexing or restoring force generated by the 34080 tubular member.

[000452] Referring to Figure 94, a tubular grid 34092 of strands 34090 can be deformable. |The tubular screen 34092 can produce or contribute to the deformability and/or resilience of the tubular member 34080. For example, the strands 34090 of the tubular screen 34092 can be woven together so that the strands 34090 are configured to slide and/or or bend in relation to each other. When a force is applied to the elongated portion 34082 of the tubular member 34080, the strands 34090 therein may slide and/or bend so that the tubular lattice 34092 moves into a deformed configuration. For example, still referring to Figure 94, a staple 30030 can compress the tubular screen 34092 and the captured T-fabric in a staple grip area 34039 which can cause the strands 34090 of the tubular screen 34092 to slip and/or bend. in relation to each other. A top apex 34086 of the tubular screen 34092 may move towards a bottom apex 34088 of the tubular screen 34092 when the tubular screen 34092 is compacted to the warped configuration to accommodate the captured tissue T in a staple gripping area 30039. Under various circumstances, the tubular reticle 34092 captured in a fired staple 30030 will seek to resume its undeformed configuration and may apply a restoring force to the captured tissue T. Additionally, portions of the tubular reticle 34092 positioned between the areas of Clip entrapment 30039, i.e., not captured by a fired clip 30030, can also be deformed due to deformation of adjacent portions of tubular lattice 34092 that are within the staple entrapment areas 30039. Where tubular lattice 34092 is deformed, tubular lattice 34092 may seek to recover or partially recover from the deformed configuration. Optionally, portions of the tubular grid 34092 can recover to their initial configurations and other portions of the tubular grid 34092 can only partially recover and/or remain fully compacted.

[000453] Similar to the description of the tubular elements in this document, each wire 34090 can also be deformable. Additionally, deformation of a wire 34090 can generate a restoring force that depends on the resilience of each wire 34090. Referring primarily to Figures 91 and 92, each wire 34090 of a tubular screen 34092 may be tubular. Alternatively, each strand 34090 of a tubular screen 34092 may be solid. As a further alternative, the tubular grid 30092 may comprise at least one tubular yarn 34090, at least one solid yarn 34090, at least one "X" or "T" shaped yarn 34090 and/or a combination thereof.

[000454] The strands 34090 in the tubular member 34080 may comprise a polymeric composition. The polymeric composition of a 34090 yarn may comprise non-absorbable polymers, absorbable polymers, or combinations thereof. Examples of synthetic polymers include, but are not limited to, poly(glycolic acid) (PGA), poly(lactic acid) (PLA), polycaprolactone (PCL), polydioxanone (PDO) and copolymers thereof. Absorbable polymers can include bioabsorbable biocompatible elastomeric polymers, for example. Furthermore, the polymeric composition of yarn 34090 may comprise synthetic polymers, non-synthetic polymers and/or combinations thereof. Optionally, similar to the polymeric compositions described elsewhere herein, the polymeric composition of yarn 34090 can include varying amounts of absorbable polymers, non-absorbable polymers, synthetic polymers and/or non-synthetic polymers, for example by weight.

[000455] The strands 34090 in the tubular member 34080 may additionally comprise a therapeutic agent 34098 (Figure 91) such as a pharmaceutically active agent or medicament, for example. Wire 34090 can deliver a therapeutically effective amount of therapeutic agent 34098. Therapeutic agent 34098 can be released as tubular wire 34090 is absorbed. For example, therapeutic agent 30098 may be released into fluid, such as blood, for example, that passes over or through wire 34090. As a further alternative, therapeutic agent 34098 may be released when a clamp 30030 pierces wire 34090 and/or or when the cutting element 30052 on the staple-firing slider 30050 (Figure 84) cuts a portion of the tubular lattice 34092, for example. Examples of 34098 therapeutics may include, but are not limited to, hemostatic agents and drugs such as, for example, fibrin, thrombin and/or oxidized regenerated cellulose (ORC), anti-inflammatory drugs such as, for example, diclofenac, aspirin , naproxen, subidac and/or hydrocortisone, antibiotic and antimicrobial drugs or agents such as, for example, triclosan, ionic silver, ampicillin, gentamicin, polymyxin B and/or chloramphenicol, anticancer agents such as, for example, cisplatin , mitomycin and/or adriamycin; and/or biological agents such as, for example, stem cells.

[000456] Referring to Figures 95 and 96, a tubular member 35080 may comprise multiple layers 35100 of strands 35090. The tubular member 35080 may comprise multiple layers 35100 of tubular crosshairs 35092. Referring to Figure 95, tubular member 35080 may comprise a first layer 35100a and a second layer 35100b of strands 35090, for example. Referring now to Figure 96, a tubular member 35180 of a fabric thickness compensator 35120 may comprise a third layer 35100c of strands 35090, for example. Furthermore, different layers 35100 in the tubular member 35180 may comprise different materials. Each layer 35100a, 35100b, 35100c may be bioabsorbable, wherein each layer 35100a, 35100b, 35100c may comprise a different polymeric composition. For example, first layer 35100a may comprise a first polymeric composition; second layer 35100b may comprise a second polymeric composition; and the third layer 35100c may comprise a third polymeric composition. In such cases, layers 35100a, 35100b, 35100c of tubular member 35180 can be bioabsorbed at different rates. For example, first layer 35100a can absorb quickly, second layer 35100b can absorb more slowly than first layer 35100a, and third layer 35100c can absorb more slowly than first layer 35100a and/or second layer 35100b. Alternatively, first layer 35100a can absorb slowly, second layer 35100b can absorb faster than first layer 35100a and third layer 35100c can absorb faster than first layer 35100a and/or second layer 35100b.

[000457] Similar to the 34090 strands described herein, the 35090 strands in the tubular member 35180 may comprise a drug 35098. Again referring to Figure 95, to control evasion or release of the drug(s) 35098 , the first layer 35100a of strands 35090 comprising a drug 35098a can be bioabsorbed at a first rate and the second layer 35100b of strands 35090 comprising a drug 30098b can be bioabsorbed at a second rate. For example, the first layer 35100a can absorb quickly to allow a quick initial release of the drug 35098a and the second layer 35100b can absorb more slowly to allow a controlled release of the drug 30098b. The medicament 35098a in the strands 35090 of the first layer 30100a may be different from the medicament 35098b in the strands 35090 of the second layer 35100b. For example, strands 35090 in first layer 35100a may comprise oxidized regenerated cellulose (ORC) and strands 35090 in second layer 35100b may comprise a solution comprising hyaluronic acid. In such cases, initial absorption of the first layer 35100a may release oxidized regenerated cellulose to help control bleeding while subsequent absorption of the second layer 35100b may release a solution comprising hyaluronic acid to help prevent tissue adhesion. Alternatively, layers 35100a, 35100b may comprise the same drug 35098a, 35098b. For example, again referring to Figure 96, strands 35090 in layers 35100a, 35100b and 35100c may comprise an anti-cancer agent, such as, for example, cisplatin. In addition, the first layer 35100a can absorb quickly to allow a rapid initial release of cisplatin, the second layer 35100b can absorb more slowly to allow a controlled release of cisplatin, and the third layer 35100c can absorb more slowly to allow a more prolonged controlled release of cisplatin. cisplatin.

[000458] Referring to Figures 97 and 98, a fabric thickness compensator 36020 may comprise an overmolding material 36024. The overmolding material 36024 may be formed outside of a tubular member 36080, within a tubular member 36080 or inside and outside of tubular member 36080. Referring to Figure 97, overmolding material 36024 may be co-extruded into and out of tubular member 36080 and tubular member 36080 may comprise tubular lattice 36092 of strands 36090. polymer composition described herein, the 36024 overmolding material may comprise poly(glycolic acid) (PGA), poly(lactic acid) (PLA) and/or any other bioabsorbable and biocompatible elastomeric polymer, for example. Additionally, the overmolding material 36024 may be non-porous so that the overmolding material 36024 forms a fluid impermeable layer on the tubular member 36080. The overmolding material 36024 may define a lumen 36084 therethrough.

[000459] In addition to the above discussed, the tubular member 36080 and/or the strands 36090 in a tubular lattice 36092 may comprise a therapeutic agent 36098. Still referring to Figures 97 and 98, a non-porous overmolding material 36024 may contain drug 36098 within an internal lumen 36084a. Alternatively or additionally, the non-porous overmolding material 36024 may contain the drug 36098 within an intermediate lumen 36084b such as, for example, the intermediate lumen 36084b which contains the tubular lattice 36092 of strands comprising drug 36090. has been arranged above, tubular member 36080 can be positioned with respect to staple cavities 30012 and a cutting element 30052 in staple cartridge 30000 (Figure 84). The positioning of the clamps 30030 and/or the translation of the cutting element 30052 may be configured to puncture or rupture the non-porous overmolding material 36024 so that the drug 36098 contained in at least one lumen 36084 of the tubular element 30080 can be released from the lumen 30084. Referring to Figure 99, a tubular member 37080 may comprise a non-porous film 37110. The non-porous film 37110 may at least partially surround a cross-hatch 37092 or a first layer 37100a and a second layer 37100b of cross-hatch 30092 to provide a fluid impermeable cover similar to the 36024 overmolding material described herein.

[000460] As described herein, a tubular element may comprise at least one of a bioabsorbable material, a therapeutic agent, a plurality of strands, a tubular lattice, layers of tubular lattices, an overmolding material , a non-porous film or combinations thereof. For example, with reference to Figure 100, a tubular member 38080 may comprise an over-molding material 38024 and a plurality of strands 38090 positioned through a central lumen 38084 of the tubular member 38080. Strands 38090 may comprise a therapeutic agent. 38098. Alternatively, for example, with reference to Figure 101, a tubular member 39080 may comprise an overmolding material 39024 and a therapeutic agent 39098 positioned in a central lumen 39084 of the tubular member 39080, for example. Optionally, at least one of the tubular member 39080 and the overmolding material 39024 may comprise a fluid therapeutic agent 39098.

[000461] First, again, with reference to Figure 84, the tubular element 30080 may be positioned relative to the rigid support portion 30010 of the staple cartridge 30000. The tubular element 30080 may be longitudinally positioned adjacent the rigid support portion 30010. Tubular element 30080 may be substantially parallel to or aligned with a longitudinal slot or cavity 30015 in rigid support portion 30010. Tubular element 30080 may be aligned with longitudinal slot 30015 such that a portion of tubular element 30080 overlaps with it. a portion of the longitudinal slot 30015. In such cases, a cutting element 30052 in the staple-firing sliding support 30050 may separate a portion of the tubular element 30080 as the cutting edge 30052 translates along the longitudinal slot 30015. Alternatively, the element tube 30080 may be longitudinally positioned on a first or second side of longitudinal slot 30015. As an alternative In addition, tubular member 30080 may be positioned relative to rigid support portion 30010 of staple cartridge 30000 such that tubular member 30080 crosses laterally or diagonally through at least a portion of rigid support portion 30010.

[000462] Referring to Figure 102, for example, a fabric thickness compensator 40020 can comprise multiple tubular elements 40080. The tubular elements 40080 can comprise different lengths, cross-sectional shapes and/or materials, for example. Additionally, the tubular elements 40080 may be positioned relative to the rigid support portion 40010 of the staple cartridge 30000 so that the tubular axes of the tubular elements 40080 are parallel to one another. The tubular axes of the tubular elements 40080 may be longitudinally aligned so that a first tubular element 40080 is positioned within another tubular element 40080. Alternatively, the parallel tubular elements 40080 may longitudinally traverse the staple cartridge 30000, for example. As a further alternative, parallel tubular elements 40080 may cross laterally or diagonally through staple cartridge 30000. Alternatively, non-parallel tubular elements 40080 may be angularly oriented relative to each other so that their tubular axes intersect and/or are not parallel to each other.

[000463] Referring to Figures 102 to 105, a fabric thickness compensator 40020 may have two tubular elements 40080; a first tubular element 40080a may be longitudinally positioned on a first side of longitudinal slot 30015 in rigid support portion 30010 and a second tubular element 40080b may be longitudinally positioned on a second side of longitudinal slot 30015. Each tubular element 40080 may comprise a - tubular casing 40092 of strands 40090. The staple cartridge 30000 may comprise a total of six rows of staple cavities 30012, wherein three rows of staple cavities 30012 are positioned on each side of longitudinal slot 30015, for example. In such cases, it may not be necessary for the cutting edge 30052 on the staple-firing slider 30050 to separate a portion of the tubular member 40080.

[000464] Similarly, now referring to Figures 106 and 107, a fabric thickness compensator 41020 may comprise two tubular elements 41080a, 41080b longitudinally disposed in the staple cartridge 30000. Similar to the above, the staples 30030 of three rows of clip cavities 30012 may engage a tubular member 41080a and clips 30030 of three different rows of clip cavities 30012 may engage another tubular member 41080b. Still referring to Figures 106 and 107, the installed clamps 30030 can engage the tubular element 40080 at different locations throughout its cross-section of the tubular element 40080. As discussed herein, the resilience of flexing and the corresponding restoring force exerted by the tubular element 41080 may depend on the cross-sectional shape of the tubular element 41080, among other things. A clamp 30030 positioned in a clamp gripping area 30039 located on or near an arcuate portion of the tubular member 41080 may experience greater restoring force than a clamp 30030 in a clamp gripping area 30039 positioned close to a non-returnable portion. arched. Similarly, a clamp 30030 positioned in the clamp gripping area 30039 in the non-arcuate portion of the tubular member 41080 may experience less restoring force than the restoring force experienced by a clamp 30030 positioned on or closer to the arcuate portion of the tubular member 30080. In other words, the arcuate portions of a collapsible tube 41080 may have a greater spring coefficient than the non-arcuate portion of the tubular member 41080 due to the possibility that a greater amount of elastic material can be captured by the clamps 30030 along such portions. Optionally, as a result, with reference primarily to Figure 107, the restoring force generated by the fabric thickness compensator 41020 may be greater near clamps 30030a and 30030c and less close to clamp 30030b on tubular member 30080a. Correspondingly, the restoring force generated by the fabric thickness compensator 41020 may be greater near clamps 30030d and 30030f than close to clamp 30030e on tubular member 30080b.

[000465] Again with reference to Figures 102 to 105, the cross-sectional geometries of beads 40090 comprising the tubular lattice 40092 can be selected in order to provide a desired flex resilience and corresponding restoring force exerted by the tubular reticle 40092. For example, again with reference to Figure 103, strands 40090a positioned in the arcuate portions of the tubular member 40080 may comprise X-shaped cross-sections, while strands 40090b positioned in non-arcuate portions of the tubular element 40080 may comprise tubular cross-sections. Strands 40090a and 40090b comprising different geometries in cross section can be woven together to form tubular lattice 40092. Alternatively, strands 40090a and 40090b can be secured together with an adhesive, for example. Referring to Figures 104 and 105, the different cross-sectional geometries of 40090 strands in the 40080 tubular element can optimize the restoring force experienced in 30039 staple grip areas throughout the 30000 staple cartridge. Specific cross-sectional geometries can be selected so that the flex constant in areas of staple entrapment 30039 throughout the staple cartridge is substantially balanced or equal.

[000466] Referring to Figure 108, tubular elements 41080a, 41080b of a fabric thickness compensator 41120 may be joined by a joining portion 41126. Although the translational cutting element 30052 may be configured to pass between the tubular elements 41080a and 41080b, it may be necessary for the cutting member 30052 to separate at least a portion of the joining portion 41126. The joining portion 41126 may comprise a soft material, such as a foam or gel, which is easily separated by the member. 30052. The joint portion 41026 may releasably secure the tissue thickness compensator 41120 to the surgical end actuator 12. The joint portion 41126 may be attached to the top platform surface 30011 of the rigid support portion. 30010 so that the joining portion 41126 remains retained in the surgical end actuator 12 after the tubular elements 41080a, 41080b are released therefrom.

[000467] Referring to Figures 109 and 110, a fabric thickness compensator 42020 may comprise multiple tubular elements 42080 so that the number of tubular elements 42080 is equal to the number of rows of staple cavities 30012 in the staple cartridge 30000, for example. The staple cartridge 30000 can comprise six rows of staple cavities 30012 and the fabric thickness compensator 42020 can comprise six tubular elements 42080. Each tubular element 42080 can be substantially aligned with a row of staple cavities 30012. When staples 30030 are ejected from a row of clip cavities 30012, each clip 30030 of that row can pierce the same tubular member 42080 (Figure 110). The deformation of a tube 42080 can have little or no impact on the deformation of an adjacent tube 42080. Consequently, the tubular elements 42080 can exert a substantially discontinuous and customized flexing force in areas of clamp grip 30039 along the entire width. of staple cartridge 30030. Where staples 30030 fired from multiple rows of staple cavities 30012 engage the same tubular member 35080 (Figure 107), the deformation of tubular member 35080 may be less customized. For example, deformation of a collapsible tube 35080 in a clamp gripping area 30039 in a first row can impact the deformation of that tubular member 35080 in a clamp gripping area 30039 in another row. The translational cutting edge 30052 can prevent separation of the tubular elements 42080. Alternatively, referring to Figure 111, a fabric thickness compensator 43020 may comprise more than six tubular elements 43080 such as, for example, seven tubular elements 44080. Additionally , tube elements 43080 can be symmetrically or non-symmetrically arranged on end actuator 12. When an odd number of tube elements 43080 are arranged longitudinally and symmetrically on end actuator 12, translational cutting element 30052 can be configured to separate the intermediate tubular element that overlaps the longitudinal channel 30015.

[000468] Referring to Figure 112, a fabric thickness compensator 44020 may comprise a central tubular member 44080b that is at least partially aligned with longitudinal slot 30015 in rigid support portion 33010 of staple cartridge 30000. fabric 44020 may additionally comprise at least one peripheral tubular member 44080a, 44080c situated on one side of longitudinal slot 30015. For example, fabric thickness compensator 44020 may comprise three tubular members 44080: a first peripheral tubular member 44080a may be longitudinally positioned on a first side of the longitudinal slot 30015 of the staple cartridge 30000, a central tubular member 44080b may be positioned substantially over and/or aligned with the longitudinal slot 30015 and a second peripheral tubular member 44080c may be longitudinally positioned on a second side of the longitudinal slot 30015. The central tubular element 44080 b may comprise a horizontal diameter which is substantially elongated with respect to the vertical diameter. The central tubular element 44080b and/or any other tubular element can overlap multiple rows of clamp cavities 30012. Still referring to Figure 112, the central tubular element 44080b can overlap four rows of clamp cavities 30012 and each peripheral tubular element 44080a , 44080c can overlap a single row of clip cavities 30012, for example. Alternatively, central tubular member 44080b may overlap less than four rows of clamp cavities 30012, such as two rows of staple cavities 30012, for example. Additionally, peripheral tubular elements 44080a, 44080c may overlap more than one row of clamp cavities 30012 such as, for example, two rows of clamp cavities 30012. Now referring to Figure 113, a central tubular element 44180b of a compensator of tissue thickness 44120 may comprise a therapeutic agent 44198 in a lumen 44184 of the central tubular member 44180b. Optionally, central tubular member 44180b and/or at least one peripheral tubular member 44080a, 44080c may comprise therapeutic agent 44198 and/or any other suitable therapeutic agent.

[000469] Referring to Figure 114, the fabric thickness compensator 44220 may comprise a housing 44224, which may be similar to the overmolding material 32024 described herein. Housing 44224 retains multiple tubular elements 44080 in position on end actuator 12. Housing 44224 may be co-extruded with tubular elements 44080. Tube elements 44080 may comprise tubular lattice 44092 of strands 44090. Similar to polymeric compositions described elsewhere in this document, substrate 44224 may comprise poly(glycolic acid) (PGA), poly(lactic acid) (PLA) and/or any other suitable bioabsorbable biocompatible elastomeric polymer, for example. Additionally, the housing 44224 may be non-porous so that the housing 44224 forms a fluid impermeable layer on the fabric thickness compensator 44220, for example. In addition to the discussion of this document, the tubular member 44080 and/or the strands 44090 in the tubular lattice 44092 may comprise a therapeutic agent 44098. The non-porous housing 44224 may contain the therapeutic agent 44098 in the fabric thickness compensator. As described herein, tubular member 44080 may be positioned with respect to clip cavities 30012 and a cutting member 30052 in clip cartridge 30000. Positioning clips 30030 and/or translation of cutting member 30052 may be configured to puncture or rupture the non-porous housing 44224 so that the therapeutic agent 44198 contained therein can be released from the fabric thickness compensator 44020.

[000470] Referring to Figure 115, a fabric thickness compensator 44320 may comprise a central tubular member 44380b which comprises a tubular screen 44392. The tubular screen 44392 may have a nonwoven portion or a gap 44381 that is substantially aligned with the slit. 30015 of the rigid support portion 30010. In such cases, a woven portion of the tubular lattice 44092 of the tubular element 44380b does not overlap the longitudinal slot 30015. Accordingly, the cutting element 30052 on the sliding clip-fire support 30052 may translate along the longitudinal slot 30015 without separating an overlapping woven portion of the tubular grid 44392. Although the clamps 30030c and 30030d positioned adjacent to the gap 44381 in the tubular member 44380b may receive less support from the tubular grid structure 44392, additional features may provide supports for those 30030 clamps and/or additional restoring force in entrapment areas the clamp 30039 thereof. For example, as described in more detail in this document, the additional tubular elements, blanket support material, springs and/or struts can be positioned at least inside or at least outside the tubular element 44380b near gap 44381, for example .

[000471] Now referring to Figures 116 to 119, a fabric thickness compensator 45020 may comprise multiple tubular elements 45080 which traverse laterally through the staple cartridge 30000. The tubular elements 45080 may be positioned perpendicular to the rows of staple cavities 30012 and/or or to the longitudinal axis of the rigid support portion 30010 of the staple cartridge 30000. Referring to Figure 116, the tubular elements 45080 may pass through the longitudinal slot 30015 in the staple cartridge 30000 so that the cutting element 30052 in the sliding firing support clip 30050 is configured to separate the tubular elements 45080 as the clip trigger slider 30050 translates along the longitudinal slot 30015. Alternatively, now referring to Figure 117, the fabric thickness compensator 46020 may comprise two sets of elements 46080 side traversing tubes. The first set of tu elements 46080a can be positioned on a first side of the longitudinal slot 30015 and the second set of tubular side traversing elements 46080b can be positioned on a second side of the longitudinal slot 30015. In such an arrangement, the cutting element 30052 can be configured to pass between the two sets of tubular elements 46080 without separating a portion of the tubular elements 46080. Alternatively, the cutting element 30052 may separate at least one tubular element 46080 passing through the longitudinal slot 30015 while at least one other tubular element 46080 is not crosses longitudinal slot 30015 and is not separated by cutting element 30052.

[000472] As tubular elements 45080 laterally traverse the staple cartridge 30000, with reference to Figures 118 and 119, a staple 30030 may engage at least one tubular element 45080 in each staple gripping area 30039. In In such an arrangement, each tubular element 45080 can provide a discontinuous restoring force along the length of the staple cartridge 30000. For example, with reference primarily to Figure 119, tubular elements 45080 positioned near the proximal end of the tissue thickness compensator. of the 45020, where the fabric is thicker, can be compacted to a greater extent compared to the 45080 tubular elements positioned near the distal end of the 45020 Fabric Thickness Compensator where the fabric is thinner. As a result, 45080 tubular elements positioned closer to the proximal end of the 45020 Tissue Thickness Compensator can provide a restoring force greater than the restoring force that could be generated by 46080 tubular elements positioned closer to the distal end of the thickness compensator. fabric thickness 45020. Additionally, still referring to Figure 119, the deformation of a tube 45080 can have little or no impact on the deformation of an adjacent tube 45080. Consequently, the tubular elements 45080 can exert a substantially discontinuous flexing force and customized in the 30039 clamp grip areas along the length of the 30030 clamp cartridge. Where multiple 30030 clamps fired from a single row of 30012 clamp cavities engage the same 35080 tubular element, the deformation of the 35080 tubular element may be less customized . For example, deformation of a collapsible tube 35080 in one clamp gripping area 30039 can impact the deformation of that tubular member 35080 in another clamp gripping area 30039.

[000473] As a further alternative, with reference to Figures 120 to 125, the tubular elements 47080 of the fabric thickness compensator 47020 can diagonally pass through the staple cartridge 30000. The tubular elements 47080 can pass through the longitudinal slot 30015 of the staple cartridge 30000 so that the cutting element 30052 on the sliding clamp firing bracket 30050 is configured to separate the diagonally traversing tubular elements 47080 as the sliding clamp firing support 30052 translates along the longitudinal slot 30015. Alternatively, the fabric thickness compensator 47020 may comprise two sets of diagonal traversing tubular elements 47080. A first set of diagonal traversing tubular elements 47080 may be positioned on a first side of longitudinal slot 30015 and a second set of 47080 diagonal traversing tubular elements can be positioned on a second side of the lo slot ngitudinal 30015. In such an arrangement, the cutting element 30052 may pass between the two sets of tubular elements 47080 and may not separate either tubular element 47080.

[000474] Still referring to Figures 120 to 123, the diagonally traversed tubular elements 47080 may be positioned in the clamp cartridge 30000 so that a gap is defined between the tubular elements 47080. A gap between adjacent tubular elements 47080 may to provide space for a horizontal expansion of the tubular elements 47080 when a compressive force is applied thereto, as, for example, by the T-fabric captured in the staple gripping area 30039 of the formed staple 30030. The tubular elements 47080 may be connected along a gap by a film or sheet of material 47024. The sheet of material may be positioned on at least one of the platform surface 30011 of the rigid support portion 30010 and/or the fabric contacting side of the tubular elements 47080.

[000475] Referring to Figures 124 and 125, at least one diagonal traversing tubular member 47080 may be positioned with respect to the clamp cavities 30012 in the staple cartridge 30000 so that the tubular element 47080 is positioned between the legs 30032 of the staples 30030 installed from multiple rows of 30012 clamp cavities. As the 30030 clamps are moved from the home position to the fired position, as described in more detail in this document, the clamp legs 30032 can remain positioned around the tubular member 47080. clips may be deformed so that clip legs 30032 wrap around the perimeter of tubular member 47080, for example. In such an arrangement, the clamps 30030 can be configured to move into the fired or formed position without puncturing the tubular member 47080. Movement of the clamp legs 30032 around the tubular member 47080 could prevent inadvertent release of a therapeutic agent 47098 retained in the same. The selected angular orientation of each tubular element 47080 with respect to the longitudinal slot 30015 of the staple cartridge 30000 may depend on the position of the staple cavities 30012 in the staple cartridge 30000. For example, the tubular elements 47080 may be positioned at an angle of approximately forty-five (45) degrees with respect to longitudinal slot 30015 of staple cartridge 30000. Alternatively, tubular elements 47080 may be positioned at an angle of fifteen (15) to seventy-five (75) degrees with respect to longitudinal slot 30015 of the 30000 staple cartridge, for example.

[000476] Similar to the descriptions throughout the present disclosure, multiple tubular elements in a fabric thickness compensator may be connected by a bonding agent, wrapper, fabric, overmolding, compensating material, and/or any other adhesive or proper connection structure, for example. Referring to Figures 126-128, a flexible housing 48024 can encircle or encapsulate the tubular elements 48080 in a fabric thickness compensator 48020. The flexible housing 48024 can immobilize the tubular elements 48080 in the end actuator 12 and can retain each tubular element. 48080 in position such as in longitudinal alignment to a row of staple cavities 30012. Fabric thickness compensator 48020 may comprise six tubular elements 48080, for example. The flexible housing 48024 may be sufficiently deformable and resilient to immobilize the tubular elements 48020 involved therein while allowing deformation and recovery of the tubular elements 48080. Additionally, the flexible housing 48024 can encircle the tubular elements 48080 in tension and may remain in tension engagement. to the tubular elements 48080 as they deform and/or recover.

[000477] Referring to Figure 127, prior to positioning of staples 30030, anvil 30060 can be pivoted or rotated downwards to compress fabric thickness compensator 48020 and fabric T between anvil 30060 and staple cartridge 30000. The compaction of the fabric thickness compensator 48020 may include a corresponding compaction of the flexible housing 48024 and the tubular elements 48020 therein. As the tubular elements 48020 deform, the flexible housing 48024 can similarly deform. Tube elements 48020 can be evenly compacted across the entire width of the staple cartridge 30000 and flexible housing 48024 can experience similarly uniform compaction along tube elements 48080. Referring to Figure 128, when anvil 30060 is opened after the 30030 staples have been installed from the 30000 staple cartridge, the 48080 tubular elements can recover or partially recover from the compacted configurations (Figure 127). In accordance with the invention, a tubular member 48080 is recoverable so that the tubular member 48080 returns to its initial undeformed configuration. A tubular member 48080 may partially recover so that the tubular member 48080 partially returns to its initial undeformed configuration. For example, the deformation of tubular member 48080 can be partially elastic and partially plastic. As the tubular elements 48080 recover, the flexible housing 48024 can remain tensionally engaged with each tubular element 48080. The tubular elements 48080 and the flexible housing 48024 can recover to the extent that the tubular elements 48080 and the T fabric fill the areas clamping force 30039 while the tubular elements 48080 exert adequate restoring force on the fabric T therein. Referring to Figure 129, in other cases, a fabric thickness compensator 48120 comprising six tubular elements 48180 retained in a flexible housing 48124 may be positioned on anvil 30060 of end actuator 12, for example.

[000478] Referring to Figures 130 to 133, a fabric thickness compensator 49020 may comprise a tubular member 49080 longitudinally positioned along the longitudinal axis of the anvil 30060. The fabric thickness compensator 49020 may be attached to the anvil 30060 of the actuator end cap 12 by means of a compressible compensating material 49024. Additionally, the compressible compensating material 49024 may surround or encapsulate the tubular member 49080. Similar to the disclosures in the present invention, the tubular member 49080 may comprise at least one therapeutic agent 49098 which can be released by absorbing various components of the fabric thickness compensator 49020, piercing the tubular element 49080 by staples 30030 fired from staple cartridge 30000 and/or cutting element 30052.

[000479] Referring to Figure 131, a staple cartridge 30000 may comprise staples 30030 positioned in staple cavities 30012, wherein, prior to positioning the staples 30030, the anvil 30060 and tissue thickness compensator 49020 attached thereto can pivot towards the staple cartridge 30000 and compact the captured T fabric therebetween. The tubular member 49080 of the fabric thickness compensator 49020 can be uniformly deformed along the length of the staple cartridge 30000 by the components of rotation 30060 (Figure 131). Referring to Figures 132 and 133, the sliding staple firing bracket 30050 can translate along longitudinal slot 30015 in staple cartridge 30000 and engage each driver 30040 positioned below a staple 30030 in a staple cavity 30010, wherein each engaged driver 30040 can fire or eject staple 30030 from staple cavity 30012. When anvil 30060 releases pressure on the fabric T and fabric thickness compensator 49020, the fabric thickness compensator 49020, including the tubular member 49080 and 49024 Compressible Compensation Material, can recover or partially recover from the compressed configurations (Figure 131) to a rebounded configuration (Figures 132 and 133). The tubular member 49080 and the compressible compensating material 49024 can recover to the extent that the tissue thickness compensator 49020 and the T fabric fill in the staple entrapment areas 30039 while the tissue thickness compensator 49020 exerts a restoring force. in the captured tissue T.

[000480] Referring to Figures 124 to 126, two tissue thickness compensators 50020a, 50020b can be positioned on the end actuator 12 of a surgical instrument. For example, a first fabric thickness compensator 50020a may be attached to the staple cartridge 30000 in the lower jaw 30070 and a second fabric thickness compensator 50020b may be attached to the anvil 30060. The first fabric thickness compensator 50020a may comprise a plurality of longitudinally arranged tubular elements 50080 and retained in a first compensation material 50024a. At least one tubular member 50080 may comprise a therapeutic agent 50098, similar to the therapeutic agents described herein. The first offset material 50024a may be deformable or substantially rigid. Additionally, first compensation material 50024a may retain tubular elements 50080 in position with respect to clamp groove 30000. For example, first compensation material 50024a may retain each tubular element 50080 in longitudinal alignment to a row of clamp cavities 30012 The second fabric thickness compensator 50020b may comprise first compensating material 50024a, a second compensating material 50024b and/or a third compensating material 50024c. The second and third compensation materials 50024b, 50024c may be deformable or substantially rigid.

[000481] Anvil 30060 can rotate and apply a compressive force to fabric thickness compensators 50020a, 50020b and fabric T between anvil 30060 and staple cartridge 30000. In some cases, neither the first fabric thickness compensator 50020a nor the second fabric thickness compensator 50020b can be compressible. Alternatively, at least one component of the first fabric thickness compensator 50020a and/or the second fabric thickness compensator 50020b may be compressible. When staples 30030 are fired from staple cartridge 30000, now referring to Figures 135 and 136, each staple 30030 may pierce a tubular member 50080 retained in the first fabric thickness compensator 50020a. As shown in Figure 135, the therapeutic agent 50098 retained in the tubular member 50080 can be released when a staple 30030 pierces the tubular member 50080. When released, the therapeutic agent 50098 can coat the staple legs 30032 and the surrounding T fabric. the fired staple 30030. The 30030 staples can also pierce the second fabric thickness compensator 50020b when the 30030 staples are fired from the staple cartridge 30000.

[000482] Referring to Figures 137 to 140, a fabric thickness compensator 51020 may comprise at least one tubular member 51080 laterally traversing the fabric thickness compensator 51020. For example, with reference to Figure 137, the thickness compensator of fabric 51020 can be positioned with respect to the staple cartridge 30000 so that the first end 51083 of the tubular side thru member 51080 can be positioned proximate a first longitudinal side of the staple cartridge 30000 and a second end 51085 of the element lateral traverse tube 51080 may be positioned proximate a second longitudinal side of staple cartridge 30000. Tube member 51080 may comprise a capsule-like shape, for example. As illustrated in Figure 138, tubular member 51080 may be pierced between first end 51083 and second end 51085, and in some cases tubular member 51080 may be punctured on or near the center 51087 of tubular member 51080. 51080 may comprise a polymeric composition, such as a biocompatible bioabsorbable elastomeric polymer, for example. Additionally, again referring to Figure 137, the fabric thickness compensator 51020 may comprise a plurality of lateral traversing tubular elements 51080. Thirteen tubular elements 51080 may be disposed laterally on the fabric thickness compensator 51020, for example.

[000483] Referring again to Figure 137, the fabric thickness compensator 51020 may additionally comprise a compensating material 51024 that at least partially surrounds the tubular elements 51080. The compensating material 51024 may comprise a bioabsorbable polymer such as, for example, lyophilized polysaccharide, glycoprotein, elastin, proteoglycan, gelatin, collagen and/or oxidized regenerated cellulose (ORC). The offset material 51024 can retain the tubular elements 51080 in position on the fabric thickness compensator 51020. Additionally, the offset material 51024 can be secured to the top platform surface 30011 of the rigid support portion 30010 of the staple cartridge 30000 so that the compensation material 51020 is securely positioned on the end actuator 12. The compensation material 51024 may comprise at least one drug 51098.

[000484] Still referring to Figure 137, the laterally positioned tubular elements 51080 can be positioned with respect to the translational cutting element 30052 so that the cutting element 30052 is configured to separate the tubular elements 51080. The cutting element 30052 can separate the tubular elements 51080 on or near the bore therein. When the tubular elements 51080 are separated into two halves, the separate portions of the tubular elements 51080 may be configured to swell or expand, as shown in Figure 139. For example, the tubular element 51080 may comprise a hydrophilic substance 51099 that can be released and/or exposed when the tubular member 51080 is detached. Furthermore, when the hydrophilic substance 51099 comes into contact with body fluids in the T-tissue, the hydrophilic substance 51099 can attract the fluid, which can cause the tubular member 51080 to swell or expand. As the tubular member 51080 expands, the compensation material 51024 surrounding the tubular member 51080 may shift or adjust to accommodate the flared tubular member 51080. For example, when the compensation material 51024 comprises gelatin, the gelatin may shift to accommodate the flared tubular elements 51080. Now referring to Figure 140, the expansion of the tubular elements 51080 and the displacement of the 51024 offset material can cause a corresponding expansion of the fabric thickness compensator 51020.

[000485] Similar to other fabric thickness compensators discussed throughout the present disclosure, the fabric thickness compensator 51020 can be deformed or compacted by an applied force. Additionally, the fabric thickness compensator 51020 can be resilient enough that it produces a flexing force when deformed by the applied force and can subsequently recover or partially recover when the applied force is removed. Optionally, when the fabric thickness compensator 51020 is captured in a staple gripping area 30039, the staple 30030 can deform the fabric thickness compensator 51020. For example, the staple 30030 can deform the tubular elements 51080 and/or the compensating material 51024 of the fabric thickness compensator 51020 that are captured by the fired staples 30030. Optionally, the uncaptured portions of the fabric thickness compensator 51020 can also be deformed due to deformation in the staple gripping areas 30039. When deformed, the 51020 fabric thickness compensator can seek to recover from the warped configuration. Optionally, such recovery may occur prior to the hydrophilic expansion of the tubular element 51080, simultaneously with the hydrophilic expansion of the tubular element 51080, and/or after the hydrophilic expansion of the tubular element 51080. As the fabric thickness compensator 51020 seeks to recover, it may exert a restoring force on the tissue also captured in the staple grip area 30039, as described in more detail in this document.

[000486] Optionally, at least one of the tubular elements 51080 and/or the compensating material 51024 in the tissue thickness compensator 51020 may comprise a therapeutic agent 51098. When the tubular element 51080 containing a therapeutic agent 51098 is separated, the therapeutic agent 51098 contained in tubular elements 51080 may be released. Furthermore, when the compensation material 51024 comprises the therapeutic agent 51098, the therapeutic agent 51098 can be released as the bioabsorbable compensation material 51024 is absorbed. The 51020 Tissue Thickness Compensator can provide a rapid initial release of the 51098 therapeutic agent followed by a controlled release of the 51098 therapeutic agent. For example, the 51020 Tissue Thickness Compensator can provide a rapid initial release of the 51098 therapeutic agent from the tubular elements 51080 for the T fabric along the cut line when the tubular elements 51080 comprising the therapeutic agent 51098 are separated. Additionally, as the bioabsorbable compensation material 51024 comprising the therapeutic agent 51098 is absorbed, the tissue thickness compensator 51020 can provide a sustained controlled release of the therapeutic agent 51098. At least part of the therapeutic agent 51098 may remain in the tubular element. 51080 for a short period of time before the therapeutic agent 51098 flows into the make-up material 51024. Alternatively, at least part of the therapeutic agent 51098 may remain in the tubular member 51080 until the tubular member 51080 is absorbed. The therapeutic agent 51098 released from the tubular member 51080 and the compensation material 51024 may be the same. Alternatively, tubular member 51080 and compensating material 51024 may comprise different therapeutic agents or different combinations of therapeutic agents, for example.

[000487] Still referring to Figure 140, the end actuator 12 can cut the fabric T and fire staples 30030 into the separated fabric T almost simultaneously or in rapid succession. In such cases, a clip 30030 may be installed within the fabric T immediately after the cutting element 30052 has separated the tubular member 51080 adjacent the fabric T. In other words, the clips 30030 may engage the fabric thickness compensator. 51020 immediately after or simultaneously with the expansion of the tubular member 51080 and the expansion of the fabric thickness compensator 51020. The fabric thickness compensator 51020 may continue to grow or expand after the staples 30030 have been fired into the fabric T The 30030 clamps can be configured to pierce the 51080 tubular elements when the 30030 clamps are installed. In such cases, therapeutic agents 51098 still retained in separate tube elements 51080 may be released from tube elements 51080 and, in some cases, may cover legs 30031 of fired clamps 30030.

[000488] Referring to Figure 141, the fabric thickness compensator 51020 may be fabricated by means of a molding technique, for example. In accordance with the invention, a frame, or mold, 51120 may comprise a first longitudinal side 51122 and a second longitudinal side 51124. Each longitudinal side 51124 may comprise one or more notches 51130, which may each be configured to receive the first or second end 50183, 50185 of a collapsible tube 51080. The first end 50183 of the tubular element 51080 can be positioned in a first notch 51130a on the first longitudinal side 51122 and the second end 50183 of the tubular element 51080 can be positioned in a second notch 51130b on the second longitudinal side 51124 so that the tubular element 51080 laterally traverses the frame 51120. The notch 51180 may comprise a semi-circular groove, which can clamply engage the first or second end 50183, 50185 of the element tubular 51080 in the same. The first notch 51130a can be positioned directly along the second notch 51130b and the tubular member 51080 can be positioned perpendicular, or at least substantially perpendicular, to the longitudinal axis of the frame 51120. Alternatively, the first notch 51130a can be offset from the second notch 51130b so that the tubular member 51080 is angularly positioned with respect to the longitudinal axis of the frame 51120. As a further alternative, at least one tubular member 51080 may be longitudinally positioned within the frame 51120 so that the tubular member extends between the sides 51126, 51128 of the frame 51120. Additionally, at least one tubular element may be angularly positioned in the frame between two notches in the lateral sides 51126, 51128 of the frame and/or between a notch in a lateral side 51126 and a notch in a longitudinal side 51124, for example. The frame 51120 may comprise a support projection 51136, which can support the tubular elements 51080 positioned within the frame 51120.

[000489] The frame 51120 may comprise notches 51130 to accommodate twelve tubular elements 51080, for example. The frame slots 51130 can be filled with tubular elements 51080 while, alternatively, less than the entirety of the slots 51130 can be filled. Optionally, at least one tubular element 51080 can be positioned in the frame 51120. At least half of the notches 51130 can receive the tubular elements 51080. Since the tubular elements 51080 are positioned in the frame 51120, the compensating material 51024 can be added to the frame 51120. Compensation material 51024 may be fluid when added to frame 51120. For example, compensation material 51024 may pour into frame 51120 and may flow around tubular elements 51080 positioned therein. Referring to Figure 142, the fluidic make-up material 51024 can flow around the tubular member 51080 supported by the notches 51130 in the frame 51120. After the make-up material 51024 cures, or at least cures sufficiently, now with reference to Figure 143, the Fabric thickness compensator 51020 comprising the compensation material 51024 and tubular elements 51080 may be removed from the frame 51120. The fabric thickness compensator 51020 may be trimmed. For example, excess ply material 51024 can be removed from fabric thickness compensator 51020 so that the longitudinal sides of the ply material are substantially flat. Furthermore, with reference to Figure 144, the first and second ends 50183, 50185 of the tubular elements 51080 can be compacted together, or closed, in order to seal the tubular element 51080. The ends can be closed before the tubular elements 51080 are closed. placed in the frame 51120. Alternatively, the trimming process may transect the ends 51083, 51085 and a thermal stacking process may be used to seal and/or close the ends 51083, 51085 of the tubular elements 51080.

[000490] Again with reference to Figure 141, a reinforcing pin 51127 can be positioned within each tubular element 51080. For example, the reinforcing pin 51127 can extend through a longitudinal lumen of the tubular element 51080. reinforcing pin 51127 may extend beyond each tubular element 51080 so that reinforcing pin 51127 can be positioned in notches 51130 in frame 51120. In embodiments having reinforcing pins 51127, reinforcing pins 51127 may support tubular elements 51080 when the compensation material 51204 is poured into the frame 51120 and as the fluidic compensation material 51024 flows around the tubular elements 51080, for example. Once the compensating material 51024 cures, solidifies and/or freeze-dries or cures, solidifies and/or freeze-dries sufficiently, the tissue thickness compensator 51020 can be removed from the frame 51120 and the reinforcement pins 51127 can be removed from the longitudinal lumens of the tubular elements 51080. The tubular elements 51080 can then be filled with medicaments, for example. After the tubular elements 51080 are filled with medicaments, the fabric thickness compensator 51020, including the ends 51083, 51085 of the tubular elements 51080, for example, can be trimmed. Fabric thickness compensator 51020 may be die cut, for example, and/or sealed by heat and/or pressure, for example.

[000491] As discussed herein, the fabric thickness compensator 52020 can comprise multiple tubular elements 51080. Now referring to Figure 145, the tubular elements 51080 can comprise different material properties, dimensions and geometries. For example, a first tubular element 51080a can comprise a first thickness and a first material and a second tubular element 51080b can comprise a second thickness and a second material. Optionally, at least two tubular elements 51080 in the fabric thickness compensator 52020 may comprise the same material. Alternatively, each tubular member 51080 in the fabric thickness compensator 5202 may comprise different materials. Similarly, at least two tubular elements 51080 in fabric thickness compensator 52020 may comprise the same geometry. Alternatively, each tubular member 51080 in the fabric thickness compensator 52020 may comprise different geometries.

[000492] Referring now to Figures 208 to 211, a fabric thickness compensator 51220 may comprise at least one tubular member 51280 that crosses laterally the fabric thickness compensator 51220. Referring to Figure 208, the fabric thickness compensator 51220 may be positioned relative to anvil 30060 of end actuator 12. Fabric thickness compensator 51220 may be attached to a gripping surface 30061 of anvil 30060 of end actuator 12, for example. Referring primarily to Figure 209, tubular member 51280 may comprise a capsule-like shape, for example. Tubular member 51280 may comprise a polymeric composition, such as a biocompatible, bioabsorbable elastomeric polymer, for example.

[000493] Referring again to Figure 208, the fabric thickness compensator 51220 may additionally comprise a compensating material 51224 which at least partially surrounds the tubular elements 51280. The compensating material 51224 may comprise a bioabsorbable polymer such as, for example, lyophilized polysaccharide, glycoprotein, elastin, proteoglycan, gelatin, collagen and/or oxidized regenerated cellulose (ORC), for example. In a similar manner to the above, the balancing material 51024 can retain the tubular elements 51280 in position on the fabric thickness compensator 51220. Additionally, the balancing material 51224 can be secured to the gripping surface 30061 of the anvil 30060. such that the compensating material 51220 is securely positioned on the end actuator 12. The compensating material 51224 may comprise at least one medicament.

[000494] Still referring to Figure 208, the laterally positioned tubular elements 51280 can be positioned with respect to the cutting element 30252 on a sliding support in translation 30250 so that the translatable cutting element 30252 is configured to separate the elements 51280. Cutting element 30252 can separate tubular elements 51280 on or near the center of each tubular element 51280, for example. When the tubular elements 51280 are separated into two halves, the separate portions of the tubular elements 51280 may be configured to dilate or expand, as shown in Figure 208. Referring primarily to Figure 210, a tubular element 51280 may comprise a hydrophilic substance 51099 that can be released and/or exposed when the tubular member 51280 is separated. Furthermore, now referring to Figure 211, when the hydrophilic substance 51099 comes into contact with bodily fluids in the T-tissue, the hydrophilic substance 51099 can attract the fluid, which can cause the tubular member 51280 to swell or expand. As the tubular member 51280 expands, the compensation material 51224 surrounding the tubular member 51280 may shift or adjust to accommodate the flared tubular member 51280. For example, when the compensation material 51224 comprises gelatin, the gelatin may shift to accommodate the flared tubular member 51280. Again referring to Figure 208, the expansion of the tubular members 51280 and the displacement of the compensating material 51224 can cause a corresponding expansion of the fabric thickness compensator 51220.

[000495] Similar to other fabric thickness compensators discussed throughout the present disclosure, the fabric thickness compensator 51220 can be deformed or compacted by an applied force. Additionally, the fabric thickness compensator 51220 can be resilient enough that it produces a flexing force when deformed by the applied force and can subsequently recover or partially recover when the applied force is removed. Optionally, when the fabric thickness compensator 51220 is captured in a staple gripping area 30039 (Figure 88), the staple 30030 can deform the fabric thickness compensator 51220. For example, the staple 30030 can deform the tubular elements 51280 and/or the compensation material 51224 of the fabric thickness compensator 51220 captured by the fired staple 30030. Optionally, the uncaptured portions of the fabric thickness compensator 51220 may also be deformed due to deformation in the staple gripping areas 30039. When deformed, the 51220 fabric thickness compensator can seek to recover from the deformed configuration. Optionally, such recovery can occur before the hydrophilic expansion of the tubular element 51280, simultaneously with the hydrophilic expansion of the tubular element 51280 and/or after the hydrophilic expansion of the tubular element 51280. As the fabric thickness compensator 51220 seeks to recover , it can exert a restoring force on tissue also captured in the staple gripping area 30039, as described in more detail in this document.

[000496] Referring to Figures 146 to 149, a fabric thickness compensator 52020 may comprise one or more tubular elements 52080 laterally traversing the fabric thickness compensator 52020, similar to at least one fabric thickness compensator herein described. Fabric thickness compensator 52020 may comprise multiple lateral traverse tubular elements 52080. Fabric thickness compensator 52020 may additionally comprise one or more sheets of material 52024 that hold or retain at least one tubular element 52080 in the thickness compensator of fabric 52020. The one or more sheets of material 52024 may be positioned above and/or below the tubular elements 52080 and may securely retain each tubular element 52080 in the fabric thickness compensator 52020. Referring primarily to Figure 146, the Fabric thickness compensator may comprise a first sheet of material 52024a and a second sheet of material 52024b. Tubular elements 52080 can be positioned between the first and second sheets of material 52024a, 52024b. Additionally, still referring to Figure 146, the sheet of material 52024b may be secured to the top platform surface 30011 of the rigid support portion of the staple cartridge 30000 so that the fabric thickness compensator 52020 is securely positioned in the end actuator 12. Alternatively, one or more sheets of material 52024 may be attached to anvil 30060 or otherwise retained in end actuator 12.

[000497] Referring primarily to Figure 147, the fabric thickness compensator 52020 may be porous and/or permeable. For example, the sheet of material 52024 may comprise a plurality of apertures 52026. The apertures 52026 may be substantially circular. The apertures 52036 may be visible in the sheet of material 52024. Alternatively, the apertures 52036 may be microscopic. Still referring to Figure 147, tubular elements 52080 may also comprise a plurality of apertures 52026. Referring to Figure 148, a fabric thickness compensator 52120 may comprise a sheet of material 52124 comprising a plurality of non-circular apertures 52126. For example, apertures 52126 may be diamond-shaped and/or slotted. Alternatively, referring to Figure 149, a fabric thickness compensator 52220 may comprise a tubular member 52280 which comprises a permeable tubular lattice 52292. The sheet of material 52224 may comprise a biocompatible bioabsorbable elastomeric polymer and may comprise a drug, for example.

[000498] At least one tubular member 52080 can be configured to dilate or expand, as illustrated in Figures 150A-150D. For example, with reference to Figure 150A, the tubular elements 52080 may be positioned intermediate the first and second sheets of material 52024a, 52024b on the fabric thickness compensator 52020. When the fabric thickness compensator 52020 contacts the fabric T, as shown in Figure 150B, the fabric thickness compensator 52020 is expandable. For example, tubular elements 52080 may comprise a hydrophilic substance 52099 that expands when exposed to fluid within and/or on fabric T. Additionally, sheet of material 52024 and tubular elements 52080 may be permeable, as described herein. , so that the fabric fluid T can permeate the fabric thickness compensator 52020 thus allowing the fluid to contact the hydrophilic substance 52099 within the tubular elements 52080. As the tubular elements 52080 expand, the sheet of material 52024 that surrounds tubular elements 52080 may shift or adjust to accommodate dilated tubular elements 52080. Similar to various fabric thickness compensators discussed throughout the present disclosure, the expanded fabric thickness compensator 52020 can be deformed or compacted by an applied force such as a compressive force applied by clamps triggers as shown in Figure 150C. Additionally, the fabric thickness compensator 52020 can be sufficiently resilient that it produces a flexing force when deformed by the applied force and can subsequently recover when the applied force is removed. Now referring to Figures 150D and 150E, the 52020 Fabric Thickness Compensator can recover to different configurations in different 30039 staple gripping areas to properly accommodate the captured tissue T.

[000499] Referring to Figures 151 to 156, a fabric thickness compensator 53020 can comprise a plurality of vertically positioned tubular elements 53080. Optionally, each tubular element 53080 can comprise a tubular axis that is substantially perpendicular to the top platform surface 30011 of the rigid support portion 30010 of the staple cartridge 30000. Additionally, the first end of each tubular member 53080 may be positioned adjacent the top platform surface 30011, for example. Tubular elements 53080 may be deformable and may comprise an elastomeric polymer, for example. Optionally, as illustrated in Figure 152, the tubular elements 53080 can be compacted when captured in a staple gripping area 30039 with the stapled fabric T. A tubular element 53080 can comprise an elastic material so that deformation of the tubular element 53080 generates a restoring force as the 53080 tubular element seeks to recover from the deformed configuration. The deformation of tubular member 53080 can be at least partially elastic and at least partially plastic. The tubular member 53080 can be configured to act as a spring under an applied force and can be configured not to twist. Referring to Figure 153, tubular elements 53080 may be substantially cylindrical. Referring to Figure 154, a tubular member 53180 may comprise a torsional region 53112. The tubular member 53180 may be configured to twist or deform in the torsional region 53112 when a compressive force is applied thereto. The tubular member 53180 can deform elastically and/or plastically and then be designed to suddenly twist in the twist region 53112 under a preselected twisting force.

[000500] Referring primarily to Figure 155, a first tubular element 53080 can be positioned at a first end of a clamp cavity 30012 and another tubular element 53080 can be positioned at a second end of the clamp cavity 30012. illustrated in Figure 153, tubular member 53080 may comprise a lumen 53084 extending therethrough. Again with reference to Figure 152, when the clamp 30030 is moved from the home position to the fired position, each clamp leg 30032 may be configured to traverse a lumen 53084 of each tubular member 53080. Alternatively, referring primarily to Figure 156, the vertically positioned tubular elements 54080 may be arranged on a fabric thickness compensator 54020 so that the tubular elements 54080 are in a boundary position or are in contact with each other. In other words, the 54080 tubular elements can be grouped or joined. Tubular elements 54080 can be systematically arranged on fabric thickness compensator 54020; however, in other cases, the tubular elements 54080 may be randomly arranged.

[000501] Again with reference to Figures 151, 155 and 156, the fabric thickness compensator 53020 may also comprise a sheet of material 53024 that holds or retains the tubular elements 53080 in the fabric thickness compensator 53020. The material sheet 53024 may be positioned above and/or below tubular elements 53080 and may securely retain each tubular element 53080 on fabric thickness compensator 53020. Fabric thickness compensator 53020 may comprise first and second sheets of material 53024. tubular elements 53080 may be positioned between the first and second sheets of material 53024. Additionally, the sheet of material 53024 may be secured to the top platform surface 30011 of the rigid support portion of the staple cartridge 30000 so that the clip compensator fabric thickness 53020 is securely positioned on the end actuator 12. Alternatively, a sheet of material 53024 can be attached to the anvil 30060 or otherwise retained in end actuator 12. Sheet of material 53024 may be sufficiently deformable so that sheet of material 53024 deforms as springs 55080 in fabric thickness compensator are deformed.

[000502] Referring to Figures 157 and 158, a fabric thickness compensator 55020 may comprise at least one spring 55080 that is sufficiently resilient such that it has the ability to produce a flexing force when deformed. Referring primarily to Figure 157, the fabric thickness compensator 55020 may comprise a plurality of springs 55080 such as, for example, three rows of springs 55080. The springs 55080 may be systematically and/or randomly arranged on the thickness compensator of fabric 55020. Springs 55080 may comprise an elastomeric polymer, for example. The shape of the 55080 springs can allow deformation of the springs. The 55080 springs can be deformed from an initial configuration to a deformed configuration. For example, when a portion of the fabric thickness compensator 55020 is captured in a staple gripping area 30039, the springs 55080 within and/or around the staple gripping area 30039 may be deformed. 55080 springs can twist or flatten under a compressive force applied by a 30030 fired clamp and 55080 springs can generate a restoring force that is a function of the spring coefficient of the deformed spring 55080 and/or the amount by which the spring 55080 is deformed, for example. Spring 55080 may act as a sponge under a compressive force applied by a fired clamp 30030. Additionally, spring 55080 may comprise a compensating material, as described in greater detail throughout the present disclosure.

[000503] Fabric thickness compensator 55020 may additionally comprise one or more sheets of material 55024 that hold or retain at least one spring 55080 on fabric thickness compensator 55020. Sheets of material 55024 may be positioned above and/or or below springs 55080 and may securely retain springs 55080 in fabric thickness compensator 55020. Fabric thickness compensator 55020 may comprise a first sheet of material 55024a and a second sheet of material 55024b. Tubular elements 52080 can be positioned between the first and second sheets of material 55024a, 55024b. Referring primarily to Figure 158, the fabric thickness compensator 55020 may additionally comprise a third sheet of material 55024c positioned adjacent to any of the first or second sheets of material 55024a, 55024b. Optionally, at least one sheet of material 55024 may be secured to the top platform surface 30011 of the rigid support portion of the staple cartridge 30000 so that the fabric thickness compensator 55020 is securely positioned on the end actuator 12 Alternatively, at least one sheet of material 55024 may be attached to anvil 30060 or otherwise retained in end actuator 12.

[000504] Now referring to Figure 158, when a staple 30030 is fired from the staple cartridge 30000 (Figure 156), the staple 30030 can engage the fabric thickness compensator 55020. The fired staple 30030 can capture tissue T and a portion of fabric thickness compensator 55020 in staple gripping area 30039. Springs 55080 may be deformable so that fabric thickness compensator 55020 will compact when captured by a fired staple 30030. Springs 55080 may be positioned between fired staples 30030 in fabric thickness compensator 55020. Alternatively, at least one spring 55080 may be captured in staple gripping area 30039.

[000505] Referring to Figure 159, a fabric thickness compensator 60020 may comprise at least two compensation layers 60022. The fabric thickness compensator 60020 may comprise a plurality of compensation layers 60022 that can be stacked on top of a the other, positioned side by side or a combination thereof. As described in more detail herein, the compensating layers 60022 of the fabric thickness compensator 60020 may comprise different geometric and/or material properties, for example. Furthermore, as described in more detail - in this document, pockets and/or channels may exist between adjacently stacked compensation layers 60022. For example, a fabric thickness compensator 62020 may comprise six compensation layers 62022a, 62022b, 62022c, 62022d, 62022e, 62022f, which can be stacked adjacently on top of each other (Figure 174).

[000506] Referring to Figures 160, 161 and 163-168, a fabric thickness compensator may comprise a first balance layer 60122a and a second balance layer 60122b. First compensating layer 60122a may be adjacently stacked on top of second compensating layer 60122b. Adjacently stacked compensating layers 60122 may be separated by a gap or divider pocket 60132. Referring primarily to Figure 160, a fabric thickness compensator 60120 may also comprise at least one support or support beam 60124 positioned between the first and the second compensation layers 60122a, 60122b. Support 60124 can be configured to position first compensation layer 60122a with respect to second compensation layer 60122b so that compensation layers 60122 are separated by separation gap 60132. As described in more detail in this document, the deformation of support 60124 and/or the compensation layers 60122a, 60122b, for example, can reduce the separation gap 60132.

[000507] The support beam of a fabric thickness compensator can comprise various geometries and dimensions. For example, the support beam may be a single i-beam centered single bending support beam 60124 (Figure 160), an off centered single bending support beam 60224 (Figure 161), an elliptical support beam 60324 (Figure 163). ), a multi-flex support beam 60424 (Figure 164) and/or a symmetrical double cantilever fixed support beam 60524 (Figure 165). Furthermore, again referring to Figures 160, 166 and 167, a support beam 60624 may be thinner than at least one compensating layer 60122 (Figure 166), a support beam 60724 may be thicker than at least at least one balancing layer 60122 (Figure 167) and/or a supporting beam 60124 can be substantially the same thickness as at least one balancing layer 60122 (Figure 160), for example. The material, geometry and/or dimensions of the support beam 60124, for example, can affect the deformability and springback resilience of the fabric thickness compensator 60120.

[000508] Still referring to Figure 160, the compensating layers 60122 and the support beam 60124 of the fabric thickness compensator 60120 can comprise different materials such as, for example, structural material, biological material and/or electrical material, for example. For example, at least one compensation layer 60122 may comprise a polymeric composition. The polymeric composition may comprise an at least partially elastic material so that the deformation of the compensating layer 60122 and/or the support beam 60124 can generate a flexing force. The polymeric composition of the 60122 make-up layer can comprise non-absorbable polymers, absorbable polymers, or combinations thereof. Absorbable polymers may include bioabsorbable biocompatible elastomeric polymers, for example. Furthermore, the polymeric composition of the 60122 compensation layer may comprise synthetic polymers, non-synthetic polymers, or combinations thereof. Examples of synthetic polymers include, but are not limited to, poly(glycolic acid) (PGA), poly(lactic acid) (PLA), polycaprolactone (PCL), polydioxanone (PDO) and copolymers thereof. Examples of non-synthetic polymers include, but are not limited to, polysaccharides, glycoprotein, elastin, proteoglycan, gelatin, collagen, and oxidized regenerated cellulose (ORC). Optionally, similar to the polymeric compositions described elsewhere herein, the polymeric composition of the 60122 make-up layers can include varying amounts of absorbable polymers, non-absorbable polymers, synthetic polymers and non-synthetic polymers, for example by weight. Optionally, each balancing layer 60022 in the fabric thickness compensator 60120 can comprise a different polymeric composition, or alternatively, at least two balancing layers 60122 can comprise the same polymeric composition.

[000509] Again referring to Fig. 159, at least one compensation layer 60022 may comprise a therapeutic agent 60098 such as a medicament or pharmaceutically active agent, for example. The buffer layer 60022 may release a therapeutically effective amount of the therapeutic agent 60098. The therapeutic agent 60098 may be released as the buffer layer 60022 is absorbed. Examples of 60098 therapeutics may include, but are not limited to, hemostatic agents and drugs such as, for example, fibrin, thrombin and/or oxidized regenerated cellulose (ORC), anti-inflammatory drugs such as, for example, diclofenac, aspirin , naproxen, sulindac and/or hydrocortisone, drugs or antibiotic and antimicrobial agents such as, for example, triclosan, ionic silver, ampicillin, gentamicin, polymyxin B and/or chloramphenicol and/or anticancer agents such as, for example, cisplatin, mi - tomycin and/or adriamycin. The therapeutic agent 60098 may comprise a biological agent, such as a stem cell, for example. Optionally, each buffer layer 60022 in a fabric thickness buffer 60020 may comprise a different therapeutic agent 60098, or alternatively, at least two buffer layers 60022 may comprise the same therapeutic agent 60098. A buffer layer 60022 comprising an agent therapeutic 60098, as a biological agent, for example, can be confined between two structural compensation layers 60022 that comprise a polymeric composition such as, for example, poly(glycolic acid) (PGA) foam, for example. In accordance with the invention, a compensation layer 60022 may also comprise an electrically conductive material such as copper.

[000510] Again referring to Figure 174, the compensation layers 62022 in the fabric thickness compensator 62020 can have different geometries. When layers 62022 are positioned adjacent to fabric thickness compensator 62020, compensation layers 62022 may form at least one three-dimensional conduit 62032 between layers 62022. For example, when a second compensation layer 62022b comprising a channel is positioned above of a substantially flat third trim layer 62022c, the groove and the flat surface of the third trim layer 62022c may define a three-dimensional conduit 62032a therebetween. Similarly, for example, when a fifth compensation layer 62022e that comprises a channel is positioned below a fourth compensation layer 62022d that comprises a corresponding channel, the channels can form a three-dimensional conduit 62032b defined by the channels in the layers of adjacently stacked offset 62022d, 62022e. The 62032 conduits can direct therapeutic agents and/or body fluids as the fluids flow through the 62020 tissue thickness compensator.

[000511] Referring to Figure 170, a fabric thickness compensator 61020 may comprise compensating layers 61022, such as layers 60122a and 21022b, configured to receive staples 30030 installed from staple cartridge 20000 (Figure 169). As a clamp 30030 is moved from a home position to a triggered position, the geometry of at least one compensation layer 61022 can guide clamp legs 30032 to the triggered position. Optionally, at least one compensation layer 61022 may comprise apertures 61030 extending therethrough, wherein apertures 61030 may be arranged to receive staple legs 30032 of installed staples 30030 when staples 30030 are fired from staple cartridge 20000 (Figure 169), as described in more detail in this document. Alternatively, again referring to Fig. 174, the clamp legs 30032 may pierce through at least one compensation layer, such as the compensation layer 62022f, for example, and may be received through openings 62030 in at least one compensation layer. such as the compensation layer 62022a.

[000512] Referring primarily to Figure 170, the fabric thickness compensator 60120 may comprise at least one support flap 61026 on one of the compensating layers 61022a, 61022b. Support tab 61026 may project into separation gap 61032 defined between adjacent compensation layers, such as gap 61032 between first compensation layer 61020a and second compensation layer 61020b. Support tab 61026 may project from a longitudinal side of a first compensation layer 61022a. Additionally, support tab 61026 may extend along the length of the longitudinal side or only along a portion thereof. Optionally, at least one support flap 61026 may project from two longitudinal sides of the compensation layer 61022a, 61022b. Additionally, adjacently positioned compensation layers 61022a, 61022b may comprise corresponding support flaps 60126, so that support flap 60126 extending from first compensation layer 60122a can at least partially align with supporting flap 60126 which extends from the second compensation layer 60122b. Referring again to Figure 168, a fabric thickness compensator 60820 may comprise a stopper plate 60828 between adjacent compensating layers 60122a, 60122b. The stopper plate 60828 may be positioned in the gap 60132 defined between the first compensation layer 60122a and the second compensation layer 60122b, for example. As described in more detail in this document, the support tab(s) 61026 and/or the stop plate(s) 60828 can control the deformation and/or deflection of a support 60124 and/or of the compensation layers 60122a, 60122b.

[000513] As described herein, the compensating layers 60022 of the fabric thickness compensator 60020 may comprise different materials, geometries and/or dimensions. Such 60020 fabric thickness compensators can be assembled using a variety of fabrication techniques. Referring primarily to Figure 159, the fabric thickness compensator 60022 can be manufactured using lithographic, stereolithographic (SLA) or screen printing processes. For example, a stereolithographic fabrication process may create a fabric thickness compensator 60020 in which each compensating layer 60022 comprises different materials and/or geometric features. For example, an ultraviolet light in a stereolithography machine can draw the geometry of a first compensation layer 60022 such that the first compensation layer 60022 comprising a first material, geometry and/or dimensions is cured by the UV light. The ultraviolet light may subsequently design the geometry of a second compensation layer 60022 such that the second compensation layer 60022 comprising a second material, geometry and/or dimensions is cured by the UV light. In accordance with the invention, a stereolithography machine can draw compensation layers 60022 on top of each other, side by side, or a combination thereof. Additionally, 60022 offset layers can be designed so that there are pockets 60132 between adjacent 60022 offset layers. Due to the fact that a stereolithography machine can create very thin layers that have unique geometries, a 60020 fabric thickness compensator manufactured by means of a stereolithographic process it can comprise a very complex three-dimensional geometry.

[000514] Referring to Figure 169, the tissue thickness compensator 60920 can be positioned on the end actuator 12 of a surgical instrument 10 (Figure 1). The fabric thickness compensator 60920 can be positioned relative to the staple cartridge 20000 of the end actuator 12. For example, the fabric thickness compensator 60920 can be releasably attached to the staple cartridge 20000. At least one Compensation layer 60922 of fabric thickness compensator 60920 may be positioned adjacent to the top platform surface 20011 (Figure 79) of staple cartridge 20000. For example, a second compensation layer 60922b may be secured to the top platform surface. 20011 by means of an adhesive or by means of a wrapper, similar to at least one of the wrappers described herein (Figure 16). The fabric thickness compensator 60920 can form a single piece with the staple cartridge 20000 so that the staple cartridge 20000 and the fabric thickness compensator 60920 are formed as a unitary construction. For example, staple cartridge 20000 may comprise a first body portion, such as rigid support portion 20010 (Figure 79) and a second body portion, such as fabric thickness compensator 60920.

[000515] Still referring to Figure 169, the fabric thickness compensator 60920 may comprise a first compensator portion 60920a and a second compensator portion 60920b. The first compensator portion 60920a may be positioned on a first longitudinal side of the staple cartridge 20000 and the second compensator portion 60920b may be positioned on a second longitudinal side of the staple cartridge 20000. Optionally, when the fabric thickness compensator 60920 is positioned with respect to the staple cartridge 20000, the longitudinal slot 20015 (Figure 78) in the rigid support portion 20010 (Figure 78) may extend between the first compensator portion 60920a and the second compensator portion 60920b. When the cutting element 20052 on the clip-firing slider 20050 (Figure 78) translates through the end actuator 12, the cutting element 20052 may pass through the longitudinal slot 20015 between the first trimmer portion 60920a and the second trimmer portion. 60920b without separating a portion of the fabric thickness compensator 60920, for example. Alternatively, the cutting element 20052 may be configured to separate a portion of the fabric thickness compensator 60920.

[000516] Now referring to Figure 162, a tissue thickness compensator 63020 can be configured to fit the actuator 12' end of a circular surgical instrument. Fabric thickness compensator 62030 may comprise a first circular compensation layer 63022a and a second circular compensation layer 63022b. Second compensating layer 63022b may be positioned on a circular top platform surface 20011' of a circular staple cartridge 20000', wherein second compensating layer 63022b may comprise a geometry corresponding to the geometry of the platform surface 20011'. For example, the platform surface 20011' may comprise a staggered portion and the second compensating layer 63022b may comprise a corresponding staggered portion. The fabric thickness compensator may additionally comprise at least one support 63024 and/or support tabs 63026, for example, extending around the fabric thickness compensator 63020.

[000517] Again with reference to Figure 170, the fired staples 30030 can be configured to engage the fabric thickness compensator 60920. As described throughout the present disclosure a fired staple 30030 can capture a portion of the thickness compensator of fabric 60920 and the fabric T and applying a compressive force to the fabric thickness compensator 60920. Additionally, referring primarily to Figures 171 to 173, the fabric thickness compensator 60920 may be deformable. Optionally, as described herein, a first balancing layer 60920a may be separated from a second balancing layer 60920b by a separation gap 60932. Referring to Figure 171, prior to compaction of the fabric thickness compensator 60920, the gap 60932 may understand a first distance. When a compressive force A is applied to fabric thickness compensator 60920 and fabric T, for example, by a fired staple 30030 (Figure 170), support 60924 can be configured to deform. Referring now to Fig. 172, the single bending support beam 60924 can flex under the compressive force A so that the separation gap 60932 between the first compensating layer 60920a and the second compensating layer 60920b is reduced to a second distance. Referring primarily to Fig. 173, the first and second compensation layers 60922a, 60922b can also deform under the compressive force A. The support tabs 60926 can control the deformation of the compensation layers 60920. For example, the tabs support 60926 can prevent excessive bending of the compensation layers 60920 by supporting the longitudinal sides of the compensation layer 60920 when they come into contact with each other. Support tabs 60926 can also be configured to flex or bend under compressive force A. Additionally, or alternatively, the stopper plate 60128 (Figure 168) described in greater detail in this document can limit the deformation of the layers of Compensation 60920 when Compensation Layers 60920 and/or Support Tabs 60926 make contact with Boundary Plate 60128.

[000518] Furthermore, similar to various tissue thickness compensators described herein, the 60920 tissue thickness compensator can generate a flexing or restoring force when deformed. The restoring force generated by the deformed fabric thickness compensator may depend at least on the orientation, dimensions, material and/or geometry of the 60920 fabric thickness compensator, as well as the amount by which the 60920 fabric thickness compensator is deformed by the applied force. In addition, at least a portion of the fabric thickness compensator 60920 may be resilient so that the fabric thickness compensator 60920 generates a flexing load or restoring force when deformed by a fired clamp 30030. Support 60924 may purchase -endering an elastic material and/or at least one compensating layer 60922 may comprise an elastic material so that the fabric thickness compensator 60920 is resilient.

[000519] Now referring to Figure 175, an end actuator of a surgical stapling instrument may comprise a first jaw and a second jaw, wherein at least one of the first jaw and the second jaw may be configured to be moved in relationship to each other. The end actuator may comprise a first jaw including a staple cartridge channel 19070 and a second jaw including an anvil 19060, wherein the anvil 19060 may be pivoted toward and/or away from the staple cartridge channel 19070 , for example. The staple cartridge channel 19070 may be configured to receive a staple cartridge 19000, for example, which, for example, may be detachably retained within the staple cartridge channel 19070. The staple cartridge 19000 may comprise a body cartridge 19010 and a fabric thickness compensator 19020, wherein the fabric thickness compensator 19020 may be removably secured to the cartridge body 19010. Referring now to Figure 176, the cartridge body 19010 may comprise a plurality of cavities clip 19012 and a clip 19030 positioned within each clip cavity 19012. Additionally, clips 19030 may be supported by clip drivers 19040 positioned within the cartridge body 19010, wherein a slider and/or the trigger element, for example, may advance through the staple cartridge 19000 to lift the staple drivers 19040 within the staple cavities 19012, as per i 177, and eject the 19030 clamps from the 19012 clamp cavities.

[000520] Referring primarily to Figures 175 and 176, fabric thickness compensator 19020 may comprise resilient elements 19022 and a vessel 19024 that encapsulates resilient elements 19022. Vessel 19024 may be sealed and may define a cavity containing an internal atmosphere which has a pressure that is different from the surrounding atmospheric pressure. The pressure of the inner atmosphere may be greater than a pressure of the surrounding atmosphere while, alternatively, the pressure of the inner atmosphere may be lower than the pressure of the surrounding atmosphere. In embodiments in which vessel 19024 contains a pressure less than the pressure of the surrounding atmosphere, the side wall of vessel 19024 may confine a vacuum. In such cases, the vacuum can cause the vessel 19024 to distort, flatten and/or flatten, whereby the resilient elements 19022 positioned within the vessel 19024 may be resiliently compacted within the vessel 19024. When a vacuum is created by suction in vessel 19024, resilient elements 19022 may deflect or deform downwardly and may be held in position by the side walls of vessel 19024 in a compacted vacuum packed state.

[000521] Resilient element 19022 and vessel 19024 are comprised of biocompatible materials. Optionally, resilient member 19022 and/or vessel 19024 may be comprised of bioabsorbable materials such as PLLA, PGA and/or PCL, for example. Resilient member 19022 may be comprised of a resilient material. Resilient member 19022 may also comprise structural resilience. For example, resilient member 19022 may be in the form of a hollow tube.

[000522] In addition to the above, the fabric thickness compensator 19020 may be positioned against or adjacent to the platform surface 19011 of the cartridge body 19010. When the staples 19030 are at least partially fired, now with reference to Figure 177 , the legs of the clamps 19030 may puncture or rupture the vessel 19024. The vessel 19024 may comprise a central portion 19026 which may be positioned over a cutting slot 19016 of the cartridge body 19010 so that when a cutting element 19080 is advanced into incising the T tissue positioned between the staple cartridge 19000 and the anvil 19060, the cutting element 19080 can also incise the central portion 19026 of the vessel 19024, thereby puncturing or rupturing the vessel 19024. In either case, once that vessel 19024 has been ruptured, the internal atmosphere in vessel 19024 can equalize to the atmosphere surrounding fabric thickness compensator 19020 and allow resilient elements 19 022 resiliently expand to win again, or win again at least partially, their undistorted and/or unflattened configuration. In such circumstances, the resilient elements 19022 can apply a tampering force to the fabric T captured by the deformed staples 19020. More specifically, after being deformed by the pocket forming surfaces 19062 defined in the anvil 19060, the legs of the staples 19030 can capture the fabric T and at least a portion of a resilient member 19022 within the staples 19030 so that when the vessel 19024 ruptures, the tissue thickness compensator 19020 can compensate for the thickness of tissue T captured by the staples 19030. For example, when tissue T captured by a staple 19030 is thinner, a resilient element 19022 captured by that staple 19030 can expand to fill gaps within the staple 19030 and apply sufficient compaction force to the T fabric. Correspondingly, when the captured T fabric because a clamp 19030 is thicker, a resilient element 19022 captured by that clamp 19030 can remain compacted. o to make room for the thicker fabric within the staple 19030 and similarly to apply sufficient compaction force to the T fabric.

[000523] When vessel 19024 is pierced, as outlined above, resilient elements 19022 may expand in an attempt to resiliently return to their original configuration. Under certain circumstances, the portion of resilient elements 19022 that have been captured by the clamps 19030 may not be able to return to their original undistorted shape. In such circumstances, the resilient member 19022 may comprise a spring that can apply a compaction force to the fabric T captured by the staples 19030. In accordance with the invention, a resilient member 19022 may emulate a linear spring, wherein the compaction force applied by the resilient element 19022 is linearly proportional to the amount, or distance, by which the resilient element 19022 remains deflected within the clamp 19030. Alternatively, a resilient element 19022 may emulate a non-linear spring, wherein the compaction force applied by the resilient element 19022 is not linearly proportional to the amount, or distance, by which the resilient member 19022 remains deflected within the clamp 19030.

[000524] Referring primarily to Figures 178 and 179, a staple cartridge 19200 may comprise a tissue thickness compensator 19220 which may comprise one or more sealed vessels 19222 therein. Each of the 19222 vessels may be sealed and may contain an internal atmosphere. The internal atmosphere pressure within a sealed vessel 19222 may exceed atmospheric pressure while the internal atmosphere pressure within a sealed vessel 19222 may be below atmospheric pressure. Where the pressure of the internal atmosphere inside a vessel 19222 is below atmospheric pressure, vessel 19222 can be described as containing a vacuum. Optionally, one or more of the vessels 19222 may be encased in or contained in a covering, container, casing, and/or outer film 19224, for example, wherein the fabric thickness compensator 19220 may be positioned above a platform surface. 19011 of cartridge body 19010. Each vessel 19222 may be manufactured from a tube having a circular, or at least substantially circular, cross-section, for example, having a closed end and an open end. A vacuum can be drawn from the open end of the tube, and when a sufficient vacuum is achieved inside the tube, the open end can be closed and sealed. For example, the tube may be comprised of a polymeric material, for example, the open end of the tube may be thermally stacked in order to close and seal it. In either case, the vacuum within each vessel 19222 can pull the side walls of the tube inward and resiliently distort and/or flatten the tube. The 19222 vessels are illustrated in an at least partially flattened state in Figure 179.

[000525] When the 19030 staples are in their unfired position, as illustrated in Figure 179, the tips of the 19030 staples can be positioned below the 19220 fabric thickness compensator. For example, the 19030 staples can be positioned inside their respective clamp cavities 19012 so that the clamps 19030 do not contact the vessels 19222 until the clamps 19030 are moved from the unfired positions, illustrated in Figure 179, to their fired positions, illustrated in Figure 180. tissue thickness compensator 19220 can prevent vessels 19220 from being prematurely punctured by staples 19030. When staples 19030 are at least partially fired, now referring to Figure 180, legs of staples 19030 can puncture or rupture vessels 19222 Under such circumstances, the internal atmospheres within the 19222 vessels can equalize with the atmosphere surrounding the 19222 vessels and if and xpanda resiliently to win again, or win again at least partially, its configuration not distorted and/or not flattened. Under such circumstances, the perforated vessels 19222 can apply an altering force to the tissue captured by the deformed staples 19030. More specifically, after being deformed by the pocket forming surfaces 19062 defined in the anvil 19060, the legs of the staples 19030 can capture the tissue T and at least a portion of a vessel 19222 within the staples 19030 so that when the vessels 19222 rupture, the vessels 19222 can compensate for the thickness of T tissue captured by the staples 19030. For example, when T tissue captured by a clamp 19030 is thinner, a vessel 19222 captured by that clamp 19030 can expand to fill the gaps within the clamp 19030 and, at the same time, apply sufficient compaction force to the fabric T. Correspondingly, when the clamp 19030 T tissue captured by a 19030 staple is thicker, a 19222 vessel captured by that 19030 staple can remain compacted to make room for the thicker tissue in the inside the clamp 19030 and at the same time to apply sufficient compaction force to the T fabric.

[000526] When the 19222 vessels are pierced, as outlined above, the 19222 vessels may expand in an attempt to resiliently return to their original configuration. The portion of the 19222 vessels that were captured by the 19030 clamps may not have the ability to return to their original undistorted shape. In such circumstances, the vessel 19222 may comprise a spring that can apply a compaction force to the tissue T captured by the clamps 19030. In accordance with the invention, a vessel 19222 may emulate a linear spring, wherein the compaction force applied by the vessel 19222 is linearly proportional to the amount, or distance, by which the 19222 vessel remains deflected within the 19030 clamp. Alternatively, a 19222 vessel may emulate a non-linear spring, in which the compaction force applied by the 19222 vessel is not linearly proportional to the amount, or distance, by which the vessel 19222 remains deflected within the clamp 19030. The vessels 19222 may be hollow and empty when they are in their sealed configuration. Alternatively, each of the vessels 19222 may define a cavity and may further include at least one drug contained therein. Vessels 19222 can be comprised of at least one drug that can be released and/or bioabsorbed, for example.

[000527] Vessels 19222 of tissue thickness compensator 19220 may be arranged in any suitable manner. As illustrated in Figure 178, the staple cavities 19012 defined in the cartridge body 19010 and the staples 19030 positioned in the staple cavities 19012 may be arranged in rows. As illustrated, clip cavities 19012 may be arranged in six longitudinal linear rows, for example; however, any suitable arrangement of 19012 clamp cavities could be used. Also as illustrated in Figure 178 , the tissue thickness compensator 19220 may comprise six vessels 19222, wherein each of the vessels 19222 may be aligned or positioned over a row of clip cavities 19012. Each of the clips 19030 within a row of clamp cavities 19012 may be configured to pierce the same vessel 19222. In certain situations, some of the clamp legs of clamps 19030 may not pierce vessel 19222 positioned thereon; however, where the vessel 19222 defines a continuous internal cavity, for example, the cavity may be sufficiently perforated by at least one of the clamps 19030 to allow the pressure of the internal cavity atmosphere to equal the atmospheric pressure surrounding the vessel. vessel 19222. Now referring to Figure 185, a fabric thickness compensator may comprise a vessel, such as vessel 19222', for example, which may extend in a direction that is transverse to a staple line 19030. For example, a 19222' vessel can span multiple rows of clamps. Referring now to Figure 186, a fabric thickness compensator 19220" may comprise a plurality of vessels 19222" that extend in a direction that is perpendicular, or at least substantially perpendicular, to a staple line 19030. For example, some of vessels 19222" may be pierced by clamps 19030 while others may not be pierced by clamps 19030. Vessels 19222" may extend along or across a cutting path in which a cutting element could transection and rupture vessels 19222 ", for example.

[000528] Optionally, as described above, a tissue thickness compensator, such as the tissue thickness compensator 19220, for example, may comprise a plurality of sealed vessels, such as the vessels 19222, for example. Also as described above, each of the sealed vessels 19222 may comprise a separate internal atmosphere. The 19222 vessels can have different internal pressures. For example, a first vessel 19222 may comprise an internal vacuum that has a first pressure and a second vessel 19222 may comprise an internal vacuum that has a different second pressure, for example. For example, the amount of distortion or flatness of a 19222 vessel may be a function of the vacuum pressure of the internal atmosphere contained therein. For example, a 19222 vessel that has a higher vacuum may be distorted or flattened a greater amount compared to a 19222 vessel that has a lower vacuum. The cavity of a vessel may be segmented into two or more separate sealed cavities, wherein each separate sealed cavity may comprise a separate internal atmosphere. For example, some of the staples within a row of staples may be configured and arranged to pierce a first defined cavity in the vessel while other staples within the row of staples may be configured and arranged to pierce a second defined cavity in the vessel, for example. example. In such cases, specifically in embodiments in which the staples in a row of staples are sequentially fired from one end of the row of staples to the other as described above, one of the cavities can remain intact and can maintain its internal atmosphere when another cavity is broken. The first cavity can have an internal atmosphere that has a first vacuum pressure and the second cavity can have an internal atmosphere that has a different second vacuum pressure, for example. In accordance with the invention, a cavity that remains intact can maintain its internal pressure until the vessel is bioabsorbed thereby creating a timed pressure release.

[000529] Now referring to Figures 181 and 182, a fabric thickness compensator, such as the fabric thickness compensator 19120, for example, can be attached to an anvil 19160. Similar to the above, the compensator of fabric thickness 19120 may comprise a vessel 19124 and a plurality of resilient elements 19122 positioned therein. Also similar to the above, the 19124 vessel may define a cavity containing an internal atmosphere that has a pressure that is less than or greater than the pressure of the atmosphere surrounding the 19120 fabric thickness compensator. Where the internal atmosphere in the interior of vessel 19124 comprises a vacuum, vessel 19124 and resilient elements 19122 positioned therein may be distorted, flattened and/or flattened by the difference in pressure between the vacuum in vessel 19124 and atmospheric pressure outside vessel 19124. In use, anvil 19160 can be moved to a closed position in which it is positioned opposite a staple cartridge 19100 and in which a tissue engagement surface 19121 on vessel 19124 can engage tissue T positioned intermediate the tissue thickness compensator 19120 and a 19100 staple cartridge. In use, the 19080 firing element can be advanced distally to fire the 19030 staples as described above, while at the same time making the tissue incision T. Tissue thickness compensator 19120 may additionally comprise an intermediate portion 19126 which may be aligned with a cutting slot defined in anvil 19160 in which, when trigger element 19080 advances distally through thickness compensator of tissue 19120, the trigger element 19080 can puncture or rupture the vessel 19124. Also, similar to the above, the trigger element 19080 can lift the staple drivers 19040 and fire the staples 19030 so that the staples 19030 can contact the anvil 19160 and can be deformed to its deformed configuration, as illustrated in Figure 183. When the 19030 clamps are fired, the 19030 clamps can puncture the T tissue and then puncture or rupture the vessel 19124 so that the resilient elements 19122 positioned within the vessel 19124 can expand at least partially, as outlined above.

[000530] In addition to the above, a tissue thickness compensator may be comprised of a biocompatible material. The biocompatible material, such as a foam, may comprise tackifiers, surfactants, fillers, crosslinkers, pigments, dyes, antioxidants and other stabilizers and/or combinations thereof to provide the desired properties of the material. A biocompatible foam may comprise a surfactant. The surfactant can be applied to the surface of the material and/or dispersed in the material. Without being bound by any particular theory, the surfactant applied to the biocompatible material can reduce the surface tension of fluids in contact with the material. For example, the surfactant can reduce the surface tension of the water in contact with the material in order to accelerate the penetration of water into the material. Water can act as a catalyst. The surfactant can increase the hydrophilic capacity of the material.

[000531] The surfactant may comprise an anionic surfactant, a cationic surfactant and/or a non-ionic surfactant. Examples of surfactants include, but are not limited to, polyacrylic acid, metallose, methyl cellulose, ethyl cellulose, propyl cellulose, hydroxyethyl cellulose, carboxymethyl cellulose, polyoxyethylene cetyl ether, polyoxyethylene lauryl ether, polyoxyethylene octyl ether, polyoxyethylene phenyl ether , polyoxyethylene oleyl ether, polyoxyethylene sorbitan monolaurate, polyoxyethylene stearyl ether, polyoxyethylene nonylphenyl ether, dialkylphenoxy poly(ethyleneoxy)ethanol and polyoxamers and combinations thereof. The surfactant may comprise a copolymer of polyethylene glycol and polypropylene glycol. The surfactant may comprise a phospholipid surfactant. The phospholipid surfactant may provide antibacterial stabilizing properties and/or disperse other materials in the biocompatible material.

[000532] The tissue thickness compensator may comprise at least one drug. The fabric thickness compensator may comprise one or more natural materials, non-synthetic materials and/or synthetic materials described herein. The tissue thickness compensator may comprise a biocompatible foam comprising gelatin, collagen, hyaluronic acid, oxidized regenerated cellulose, polyglycolic acid, polycaprolactone, polylactic acid, polydioxanone, polyhydroxyalkanoate, polyglecaprone and combinations thereof. The fabric thickness compensator may comprise a film comprising the at least one drug. The fabric thickness compensator may comprise a biodegradable film comprising the at least one drug. The medicament may comprise a liquid, a gel and/or a powder. Medicaments may comprise anti-cancer agents, for example cisplatin, mitomycin and/or adriamycin.

[000533] The tissue thickness compensator may comprise a biodegradable material to provide controlled elution of the at least one drug as the biodegradable material degrades. Biodegradable material can degrade, decompose or lose its structural integrity when it comes into contact with an activator, for example an activator fluid. The activating fluid may comprise saline or any other electrolyte solution, for example. The biodegradable material may come into contact with the activating fluid through conventional techniques, including, but not limited to, spraying, dipping and/or brushing. In use, for example, a surgeon may immerse an end actuator and/or staple cartridge comprising the tissue thickness compensator comprising the at least one drug in an activating fluid comprising a saline solution such as sodium chloride. , calcium chloride and/or potassium chloride. The tissue thickness compensator can release the drug as the tissue thickness compensator degrades. Drug elution from the tissue thickness compensator can be characterized by a rapid initial elution rate and a slower prolonged elution rate.

[000534] According to the invention, a tissue thickness compensator, for example, may be comprised of a biocompatible material which may comprise an oxidizing agent. The oxidizing agent may be an organic peroxide and/or an inorganic peroxide. Examples of oxidizing agents may include, but are not limited to, hydrogen peroxide, urea peroxide, calcium peroxide and magnesium peroxide, and sodium percarbonate. The oxidizing agent may comprise peroxygen-based oxidizing agents and hypoalite-based oxidizing agents, for example hydrogen peroxide, hypochlorous acid, hypochlorites, hypocodes and percarbonates. The oxidizing agent may comprise alkali metal chlorites, hypochlorites and perborates, for example sodium chlorite, sodium hypochlorite and sodium perborate. The oxidizing agent may comprise vanadate. The oxidizing agent may comprise ascorbic acid. The oxidizing agent may comprise an active oxygen generator. In accordance with the invention, a fabric scaffold may comprise biocompatible material which comprises an oxidizing agent.

[000535] The biocompatible material may comprise a liquid, a gel and/or a powder. The oxidizing agent may comprise microparticles and/or nanoparticles, for example. For example, the oxidizing agent can be ground into microparticles and/or nanoparticles. The oxidizing agent can be incorporated into the biocompatible material by suspending the oxidizing agent in a polymer solution. The oxidizing agent can be incorporated into the biocompatible material during the lyophilization process. After lyophilization, the oxidizing agent can be attached to the cell walls of the biocompatible material to interact with the tissue upon contact with it. The oxidizing agent may not be chemically bonded to the biocompatible material. A dry percarbonate powder can be incorporated into a biocompatible foam to provide a prolonged biological effect through the slow release of oxygen. A dry powder of percarbonate can be incorporated into a polymer fiber in a non-woven structure to provide a prolonged biological effect through the slow release of oxygen. The biocompatible material may comprise an oxidizing agent and a medicament, for example doxycycline and ascorbic acid.

[000536] The biocompatible material may comprise a rapid release oxidizing agent and/or a slower sustained release oxidizing agent. Elution of the oxidizing agent from the biocompatible material can be characterized by a rapid initial elution rate and a slower prolonged elution rate. The oxidizing agent can generate oxygen when the oxidizing agent comes into contact with body fluid, for example water. Examples of bodily fluids may include, but are not limited to, blood, plasma, peritoneal fluid, cerebrospinal fluid, urine, lymphatic fluid, synovial fluid, vitreous fluid, saliva, gastrointestinal luminal contents, and/or bile. Without being bound by any particular theory, the oxidizing agent can reduce cell death, improve tissue viability and/or maintain the mechanical strength of tissue that can be damaged during cutting and/or stapling.

[000537] The biocompatible material may comprise at least one microparticle and/or a nanoparticle. The biocompatible material may comprise one or more of the natural materials, non-synthetic materials and synthetic materials described herein. The biocompatible material may comprise particles having an average diameter of about 10 nm to about 100 nm and/or about 10 mm to about 100 mm, for example 45 to 50 nm and/or 45 to 50 mm. The biocompatible material may comprise biocompatible foam which comprises at least one microparticle and/or nanoparticle incorporated therein. The microparticle and/or nanoparticle may not be chemically bonded to the biocompatible material. The microparticle and/or the nanoparticle can provide controlled drug release. the microparticle and/or the nanoparticle may comprise at least one drug. The microparticle and/or nanoparticle may comprise a hemostatic agent, an antimicrobial agent and/or an oxidizing agent, for example. The tissue thickness compensator may comprise a biocompatible foam comprising a hemostatic agent comprising oxidized regenerated cellulose, an antimicrobial agent comprising doxycycline and/or gentamicin, and/or an oxidizing agent comprising a percarbant. The microparticle and/or nanoparticle can provide controlled drug release for up to three days, for example.

[000538] The microparticle and/or the nanoparticle can be incorporated into the biocompatible material during a manufacturing process. For example, a biocompatible polymer, for example a PGA/PCL, can be contacted with a solvent, for example dioxane to form a mixture. The biocompatible polymer can be ground to form particles. The dry particles, with or without ORC particles, can be contacted with the mixture to form a suspension. The suspension can be lyophilized to form a biocompatible foam comprising PGA/PCL which has dry particles and/or ORC particles incorporated therein.

[000539] The fabric thickness compensators or layers disclosed herein may be comprised of an absorbable polymer, for example. A fabric thickness compensator may be comprised of foam, film, fibrous fabric, fibrous non-woven PGA, PGA/PCL (poly(glycolic acid-co-caprolactone)), PLA/PCL (poly(lactic acid-co-polycaprolactone) ), PLLA/PCL, PGA/TMC (poly(glycolic acid-trimethylene co-carbonate)), PDS, PEPBO or other absorbable polyurethane, polyester, polycarbonate, polyorthoesters, polyanhydrides, polyesteramides and/or polyoxaesters, for example. According to the invention, a tissue thickness compensator can be comprised of PGA/PLA (poly(glycolic acid-co-lactic acid)) and/or PDS/PLA (poly(p-dioxanone-co-lactic acid)) , for example. According to the invention, a fabric thickness compensator may be comprised of an organic material, for example. A tissue thickness compensator can be comprised of carboxymethyl cellulose, sodium alginate, cross-linked hyaluronic acid and/or oxidized regenerated cellulose, for example. In accordance with the invention, a fabric thickness compensator may comprise a durometer in the ranges 3-7 Shore A (30-50 Shore OO) with a maximum hardness of 15 Shore A (65 Shore OO), for example. A fabric thickness compensator may be subjected to 40% compression under a load of 13 N (3 lbf), 60% compression under a load of 27 N (6 lbf), and/or 80% compression under a load of of 89 N (20 lbf), for example. One or more gases, such as air, nitrogen, carbon dioxide and/or oxygen, for example, may be bubbled through and/or contained within the fabric thickness compensator. A fabric thickness compensator may comprise microspheres therein that comprise between approximately 50% and approximately 75% of the hardness of material comprising the fabric thickness compensator.

[000540] According to the invention, a tissue thickness compensator may comprise hyaluronic acid, nutrients, fibrin, thrombin, platelet-rich plasma, sulfasalazine (Azulfidine® - 5ASA+Sulfapyridine diazo binding))- bacterial prodrug colonic (Azoreductase), mesalamine (5ASA with different prodrug configurations for delayed release), asacol® (5ASA + coated Eudragit-S - pH > 7 (coating dissolution)), Pentasa® (5ASA + coated ethyl cellulose - slow release pH/time dependent), Mesasal® (5ASA + coated Eudragit-L - pH > 6), Olsalazine (5ASA + 5ASA - bacterial colonic (Azoreductase)), Balsalazide (5ASA + 4Aminobenzoyl-B-alanine) - bacterial colonic (Azoreductase)), mesalamine granulated, Lialda (delay and SR formulation of mesalamine), HMPL-004 (herbal blend that can inhibit the activation of TNF-alpha, interleukin-1 beta and nuclear-kappa B), CCX282- B (oral chemokine receptor antagonist that interferes with lymphocyte trafficking T cells in the intestinal mucosa), Rifaximin (non-absorbable broad-spectrum antibiotic), infliximab, murine chimeric (monoclonal antibody directed against TNF-alpha-approved for the reduction of signs/symptoms and maintenance of clinical remission in adult/pediatric patients with moderate/severe luminal and fistula-producing Crohn's disease who had an inadequate response to conventional therapy), adalimumab, Total Human IgG1 (anti-TNF-alpha monoclonal antibody - approved for reducing signs/symptoms of Crohn's disease) and for the induction and maintenance of clinical remission in adult patients with moderately/severely active Crohn's disease who have inadequately responded to conventional therapies or who have become intolerant to infliximab), Certolizumab pegoll, humanized anti-TNF' FAB (monoclonal antibody fragment bound a poly(ethylene glycol)- approved for the reduction of signs/symptoms of Crohn's disease and for the induction and maintenance of a response in adult patients with moderate disease severe/severe with inadequate response to conventional therapies), Natalizumab, first non-TNF-alpha inhibitor (approved biological compound for Crohn's disease), humanized monoclonal IgG4 antibody (targeted against alpha-4 integrin - FDA approved for induction and maintenance clinical response and remission in patients with moderate/severe disease with evidence of inflammation and who had an inadequate response or were unable to tolerate conventional therapies against Crohn's disease and TNF-alpha inhibitors), concomitant immunomodulators data potentially with infliximab, azathioprine 6-Mercaptopurine (purine synthesis inhibitor - pro-drug), methotrexate (binds the dihydrofolate reductase (DHFR) enzyme that participates in the synthesis of hydrofolate-tetraencephalopathy, inhibits all purine synthesis ), allopurinol and thioprine therapy, PPI, H2 for acid suppression to protect the healing line, C-Diff - Flagyl, Vancomycin (faecal translocation treatment; probiotics; repopulation of normal endoluminal flora), and/or Rifaximin (treatment of excessive bacterial proliferation (notably, hepatic encephalopathy); not absorbed in the GI tract with action on intraluminal bacteria), for example.

[000541] As described herein, a fabric thickness compensator can compensate for variations in the thickness of fabric that is captured in staples ejected from a staple cartridge and/or contained in a row of staples, for example. In other words, certain staples in a staple line can capture thick pieces of fabric, while other staples in the staple line can capture thin pieces of fabric. Under such circumstances, the fabric thickness compensator can assume different heights or thicknesses on the staples and apply a compressive force to the tissue captured by the staples regardless of whether the captured tissue is thick or thin. In accordance with the invention, a fabric thickness compensator can compensate for variations in fabric hardness. For example, certain staples in a staple line can capture highly compressible portions of tissue, while other staples in the staple line can capture portions of tissue that are less compressible. Under such circumstances, the fabric thickness compensator may be configured to assume a lower height on staples that have captured tissue that has a lower compressibility or higher hardness, and correspondingly a greater height on staples that have captured tissue. that has a higher compressibility or lower hardness, for example. In any event, a fabric thickness compensator, regardless of whether it compensates for variations in fabric thickness and/or variations in fabric hardness, for example, may be called a 'fabric compensator' and/or 'compensator', for example.

[000542] The devices described here may be designed to be discarded after a single use, or they may be designed to be used multiple times. In either case, however, the device may be refurbished for reuse after at least one use. Overhaul may include any combination of the steps of disassembling the device, followed by cleaning or replacing particular parts, and subsequent reassembly. In particular, the device may be dismantled, and any number of particular parts or parts of the device may be selectively exchanged or removed, in any combination. After cleaning and/or changing particular parts, the device can be reassembled for subsequent use in a refurbishment facility or by a surgical team immediately prior to a surgical procedure. Those skilled in the art will appreciate that refurbishing a device can use a variety of techniques for disassembly, cleaning/replacement, and reassembly. The use of such techniques, and the resulting refurbished device, are all within the scope of this application.

[000543] Preferably, the invention described herein will be processed prior to surgery. First, a new or used instrument is obtained and, if necessary, cleaned. The instrument can then be sterilized. In a sterilization technique, the instrument is placed in a closed and sealed container, such as a plastic or TYVEK bag. The container and instrument are then placed in the field of radiation that can penetrate the container, such as gamma radiation, X-rays, or high-energy electrons. Radiation kills bacteria on the instrument and container. The sterilized instrument can then be stored in a sterile container. The sterile container keeps the instrument sterile until it is opened in the medical facility.

[000544] Any patent, publication or other descriptive material, in whole or in part, which is said to be incorporated by reference into the present invention is incorporated into the present invention only to the extent that the materials incorporated do not come into conflict with existing definitions, statements or other descriptive material presented in this description. Accordingly, and to the extent necessary, the description as explicitly set forth herein supersedes any conflicting material incorporated herein by reference. Any material, or portion thereof, which is incorporated by reference in the present invention, but which conflicts with existing definitions, statements, or other descriptive materials set forth herein, will be incorporated herein only to the extent that no conflict will appear between the embedded material and the existing description material.

[000545] While this invention has been described as having exemplary designs, the present invention may be further modified within the spirit and scope of the description. This application is therefore intended to cover any variations, uses, or adaptations of the invention using its general principles. Additionally, this application is intended to cover deviations from the present disclosure that may occur with known or customary practice in the art to which this invention relates.

Claims (10)

1. Fastener cartridge assembly (20000) for a surgical instrument, the fastener cartridge assembly (20000) comprising: a support portion (20010) comprising a fastener cavity (20012); a non-woven compensator (20020) positioned with respect to the support portion (20010), wherein the non-woven compensator (20020) comprises a plurality of non-crimp fibers (20084), wherein the non-woven compensator (20020) comprises a plurality of crimped fibers (20086), and wherein the plurality of crimped fibers (20086) are dispersed therein, characterized in that the crimped fibers (20086) are heat formed to retain a substantially spring-like shape; and a fastener (20030) movable between a home position and a fired position, wherein the fastener (20030) is at least partially positioned in the fastener cavity (20012) when the fastener (20030) is in its home position, and wherein the fastener (20030) is configured to compress the non-woven compensator (20020) when the fastener (20030) is moved between its home position and its triggered position; wherein the crimp fibers (20086) comprise a resilient material, and wherein the crimp fibers (20086) are adapted to be deformed when the fastener (20030) compresses the non-woven compensator (20020). 2. Fastener cartridge assembly (20000), according to claim 1, characterized in that the fastener (20030) comprises: a base (20031); a first leg (20032) extending from the base (20031); and a second leg (20032) extending from the base (20031), wherein the first leg (20032) and second leg (20032) are configured to curve towards the base (20031) when the fastener (20030) ) is moved to its triggered position; wherein the fastener (20030) captures a portion of the non-woven tab (20020) between the base (20031) and at least one of the first leg (20032) and the second leg (20032) when the fastener (20030) is moved to its triggered position. 3. Fastener cartridge assembly (20000), according to claim 2, characterized in that it further comprises: a slot (20015) that extends through at least a portion of the support portion (20010); and a trigger member (20050) configured to translate within the slot (20015), wherein the trigger member (20050) is configured to engage the base (20031) of the fastener (20030) when the trigger member (20050) translates so that the fastener (20030) is ejected from the fastener cavity (20012). 4. Fastener cartridge assembly (20000) according to any one of claims 1 to 3, characterized in that the non-woven compensator (20020) is releasably attached to a platform of the support portion (20010) by a sticker. 5. Fastener cartridge assembly (20000), according to any one of claims 1 to 4, characterized in that the crimped fibers (20086) are randomly dispersed and randomly oriented along the non-woven compensator (20020). 6. Fastener cartridge assembly (20000), according to any one of claims 1 to 5, characterized in that the crimped fibers (20086) comprise a bioabsorbable synthetic material. 7. Fastener cartridge assembly (20000), according to any one of claims 1 to 6, characterized in that the crimped fibers (20086) comprise a material selected from a group comprising poly(dioxanone) (PDO), polylactides (APL), polyglycolides (PGA), polycaprolactones (PCL), polycarbonates, and their copolymers. 8. Fastener cartridge assembly (20000), according to any one of claims 1 to 7, characterized in that the non-woven compensator (20020) is needle-punched and comprises a hemostatic material. 9. End actuator assembly (12) for a surgical instrument, the end actuator assembly (12) characterized in that it comprises: an anvil (20060); and the fastener cartridge assembly (20000) as defined in any one of claims 1 to 8. 10. End actuator assembly (12) according to claim 9, characterized in that the non-woven compensator (20020) is configured to disengage from the end actuator assembly (12) when the fastener (20030) compresses the non-woven compensator portion (20020).

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