US20140203478A1 - System and method for molding soft fluid-filled implant shells - Google Patents

System and method for molding soft fluid-filled implant shells Download PDF

Info

Publication number
US20140203478A1
US20140203478A1 US14/223,875 US201414223875A US2014203478A1 US 20140203478 A1 US20140203478 A1 US 20140203478A1 US 201414223875 A US201414223875 A US 201414223875A US 2014203478 A1 US2014203478 A1 US 2014203478A1
Authority
US
United States
Prior art keywords
mandrel
dispersion
axis
rod
spinning
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US14/223,875
Inventor
Feargal Judge
Kevin J. Dempsey
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Allergan Inc
Original Assignee
Allergan Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Allergan Inc filed Critical Allergan Inc
Priority to US14/223,875 priority Critical patent/US20140203478A1/en
Publication of US20140203478A1 publication Critical patent/US20140203478A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61FFILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
    • A61F2/00Filters implantable into blood vessels; Prostheses, i.e. artificial substitutes or replacements for parts of the body; Appliances for connecting them with the body; Devices providing patency to, or preventing collapsing of, tubular structures of the body, e.g. stents
    • A61F2/02Prostheses implantable into the body
    • A61F2/12Mammary prostheses and implants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C41/00Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
    • B29C41/02Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor for making articles of definite length, i.e. discrete articles
    • B29C41/04Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C41/00Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
    • B29C41/02Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor for making articles of definite length, i.e. discrete articles
    • B29C41/04Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould
    • B29C41/042Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould by rotating a mould around its axis of symmetry
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C41/00Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
    • B29C41/02Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor for making articles of definite length, i.e. discrete articles
    • B29C41/04Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould
    • B29C41/06Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould about two or more axes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C41/00Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
    • B29C41/02Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor for making articles of definite length, i.e. discrete articles
    • B29C41/08Coating a former, core or other substrate by spraying or fluidisation, e.g. spraying powder
    • B29C41/085Coating a former, core or other substrate by spraying or fluidisation, e.g. spraying powder by rotating the former around its axis of symmetry
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C41/00Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
    • B29C41/02Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor for making articles of definite length, i.e. discrete articles
    • B29C41/14Dipping a core

Definitions

  • the present invention relates to systems and methods for molding shells for fluid-filled prosthetic implants and, more particularly, to techniques for forming uniform thickness shell walls, especially useful for breast implants.
  • Implantable prostheses are commonly used to replace or augment body tissue. In the case of breast cancer, it is sometimes necessary to remove some or all of the mammary gland and surrounding tissue, creating a void that can be filled with an implantable prosthesis.
  • the implant serves to support surrounding tissue and to maintain the appearance of the body.
  • the restoration of the normal appearance of the body has an extremely beneficial psychological effect on post-operative patients, eliminating much of the shock and depression that often follows extensive surgical procedures.
  • Implantable prostheses are also used more generally for restoring the normal appearance of soft tissue in various other areas of the body, such as the buttocks, chin, calf, etc.
  • Soft implantable prostheses typically include a relatively thin and quite flexible hollow envelope or shell made of vulcanized (cured) silicone elastomer.
  • the shell is filled either with a silicone gel or with a normal saline solution. The filling of the shell takes place before or after the shell is inserted through an incision in the patient.
  • FIGS. 1A-1C illustrate one early process for dip-molding flexible implant shells for implantable prostheses and tissue expanders, involving dipping a suitably shaped mandrel 20 into a silicone elastomer dispersion 22 of a silicone solution and a solvent.
  • the mandrel 20 is withdrawn from the dispersion and the excess dispersion is allowed to drain from the mandrel.
  • the solvent typically xylene
  • the process is then repeated several times until a shell of the desired thickness is formed.
  • the layered structure characteristic of some silicone elastomer shells can be made by sequentially dipping the mandrel in different dispersions.
  • FIG. 2 illustrates an exemplary cross-section of a basic gel-filled breast implant 28 , in which a shell 30 is initially formed by a process such as the above-described mandrel dipping process.
  • the outer silicone elastomer shell 30 has an anatomical configuration, in this case matching the breast, and comes off a mold with a shell hole 32 .
  • a patch over the shell hole 32 includes an uncured portion 34 directly over the hole and a cured portion 36 covering that and adhered to the inner surface of the shell 30 .
  • the patch is cured and then the hollow interior of the shell 30 is filled with an appropriate gel 38 , such as via a needle hole in the patch.
  • the silicone gel is supplied as a two-part liquid system with a primary gel component and a cross-linking component.
  • the needle hole in the patch is then sealed with a silicone adhesive or plug, and the implant oven cured to achieve cross-linking of the gel.
  • U.S. Patent Publication No. 2004/0245671 to Smit discloses an automated system for dip molding silicone covers (shells) for breast implants in which an arm positions a mold to immerse an upper portion prior to total immersion thereof, ostensibly to eliminate air inclusions in the molded product.
  • the system includes, in sequence, a cleaning station, a dipping station, an evaporating oven, and a curing oven.
  • U.S. Patent Publication No. 2008/0208336 to Job includes the technique of spraying the silicone dispersion onto mandrels, one embodiment of which results in a nonuniform shell thickness.
  • Rotational molding provides a number of advantages to dip- or spray-molding, though the latter are currently more common in the industry.
  • the present application discloses methods and systems for molding soft shells for fluid-filled prosthetic implants, including spinning and rotating dip- or spray-mandrels during a devolatilization step to ensure an even covering.
  • the mandrels may be spun during the dipping or spraying step, and/or afterward while a solvent evaporates until a gum state is formed.
  • the techniques are particularly useful for forming hollow shells from silicone dispersions for soft implants, such as breast implants.
  • One method disclosed herein for molding a mammary prosthesis shell includes providing a mandrel and rod assembly, the rod defining a first axis and the mandrel being in the shape of a breast implant shell.
  • a silicone dispersion is applied to the mandrel, which is spun about the first axis. While being spun, the mandrel is moved from an upright position to an inverted position and back to the upright position. Furthermore, the spinning is performed while the silicone dispersion is solidifying on the mandrel.
  • the spinning may be performed at a speed of about 5-15 rpm.
  • the first axis may be at an angle of about 20° from a horizontal plane.
  • the step of moving comprises moving the mandrel and rod in a plane substantially perpendicular to a horizontal plane.
  • the step of applying may be moving the mandrel through a curtain of the silicone dispersion, moving the mandrel through a spray of the silicone dispersion, or dipping the mandrel in the silicone dispersion.
  • Another method disclosed herein for molding a soft implant shell include providing a molding system including a devolatilization chamber, a plurality of mandrel and elongated holder assemblies, a conveyor to which the mandrel and elongated holder assemblies are mounted for translation, and a spray assembly capable of providing a silicone dispersion spray.
  • the conveyors include a subsystem that can spin each mandrel about its respective central axis and rotate each mandrel within a vertical plane.
  • Each mandrel translates into the path of the spray assembly and silicone dispersion spray is applied to the respective mandrels to form coated mandrels.
  • Each coated mandrel then translates into the devolatilization chamber while the coated mandrel spins about its respective central axis and rotates within a vertical plane.
  • each coated mandrel is desirably spun about its respective central axis at a rate of about 5-15 rpm. Further, each mandrel may be spun about its respective central axis while in the path of the spray assembly.
  • the spray assembly is located outside of the devolatilization chamber.
  • the conveyor may be located within the devolatilization chamber which includes an aperture through which each mandrel passes into the path of the spray assembly.
  • the spray assembly may have a spigot that produces a dispersion curtain through which the mandrels pass.
  • the conveyor includes a pair of chain drives that engage a gripper attached to each elongated holder, and the chain drives are actuated at different speeds so as to spin each mandrel about its central axis.
  • the mandrels may be continually spun about their central axes and tilted from a nominal horizontal orientation while in the devolatilization chamber.
  • a system for manufacturing breast implant shells comprising:
  • a plurality of mandrel/rod assemblies a rotating assembly capable of rotating the mandrel/rod assemblies about a plurality of different axes; a curing chamber containing the plurality of mandrel/rod assemblies; a spray assembly capable of providing a silicone dispersion spray; and a drive assembly capable of moving the each of the mandrel/rod assemblies into the silicone dispersion spray provided by the spray assembly and into the curing chamber.
  • the drive assembly desirably spins each of the mandrels about a central axis thereof.
  • the drive assembly may include two chain drives that engage a gripper attached to each mandrel, wherein the chain drives are actuated at different speeds so as to spin each mandrel about its central axis.
  • the differential speeds of the chain drives may be such that each mandrel spins at a rate of about 5-15 rpm.
  • the system may further include a load/unload chamber and a dipping/drying chamber, the wherein drive assembly moves each mandrel in a circuit including, in series, the load/unload chamber, the dipping/drying chamber, and the curing chamber.
  • FIGS. 1A-1C show several steps in a manual PRIOR ART process of dip-forming the shell of a breast implant prosthesis
  • FIG. 2 is a sectional view through a typical gel-filled breast implant prosthesis
  • FIGS. 3A-3C are schematic views of different modes of moving a mandrel used in the dip-or spray-forming methods of the present application;
  • FIGS. 4A-4C are schematic views of a shell forming method of the present application using a dispersion curtain
  • FIG. 5 is a schematic view of an overall system of the present application for forming implant shells utilizing a dispersion curtain and a conveyor apparatus through a dipping hood;
  • FIGS. 6A-6E are schematic views of a sequence of steps in an exemplary dip-molding technique of the present application.
  • FIG. 7 is a schematic view of an overall system of the present application for forming implant shells utilizing a dip-molding technique.
  • FIG. 8 is a schematic view of a shell-forming mandrel rotated and translated between two chain drives.
  • the present invention provides improvements to previous dip- and spray-molding methods for forming soft, hollow implant shells, none of which reliably ensure that a uniform wall thickness is provided in the finished shell. Moreover, some of the methods disclosed are relatively complex, and therefore costly to implement.
  • the hollow implant shells formed by the methods disclosed herein are intended to be filled with a fluid, such as saline, or a gel such as silicone gel.
  • Implant refers to long and short-term implanted devices.
  • the methods of the invention improve conventional dip and spray-molding techniques used to create shells for soft tissue implants. Because the flow of the silicone dispersion as it drains from a mandrel depends on the shape and orientation of the mandrel, the resulting shell can vary substantially in thickness if the orientation of the mandrel remains stationary. For example, the thickness of a breast implant shell formed by conventional dip casting on a stationary mandrel might vary from 0.009 to 0.024′′ from one region to another, a variation of more than 100%. Importantly, the thickness of various regions of the shell is dictated for the most part by the shape of the mandrel and the orientation of the mandrel during the period that the silicone dispersion drains from the mandrel.
  • the mandrel In dip molding the mandrel is held such that the portion corresponding to the anterior face of the shell faces downward.
  • the bracket or rod used to hold the mandrel as it is dipped into the dispersion extends outward from that portion of the mandrel corresponding to the posterior face of the shell, such as seen in FIG. 1B for a manual process.
  • the dispersion drains relatively rapidly from the perimeter region of the mandrel, and as a result the shell in the perimeter region tends to be thinner than the shell in the polar regions. For this reason, additional dips are required to create an adequate shell thickness in the perimeter region. This can result in shell that is thicker than desired in the polar regions, especially the anterior face. The same problems occur, though to a lesser extent because of the thinner application, with spray molding.
  • the present application describes mechanical equipment that, after the mandrel is immersed in silicone dispersion, rotates the mandrel about one or more different axes so that the dispersion spreads evenly across the mandrel surface utilizing the centrifugal forces obtained from the various spinning actions. More particularly, a preferred method is to spin the mandrel about its own axis while rotating it about one or more other axes.
  • silicone is provided as a dispersion within a solvent such as xylene.
  • a solvent such as xylene.
  • the basic manufacturing process for forming a breast implant shell involves coating the mandrel in the uncured silicone dispersion, driving off the solvent (devolatilization), and then curing the material to convert it into an elastomer. It is during the step of driving off the solvent that most manufacturing issues occur, at least in terms of uneven thickness.
  • the mandrel in the context of a heat-cure silicone, the mandrel is immersed in the silicone dispersion and then placed into a chamber where the temperature is slightly elevated (typically between 35° C. and 60° C.) so that the solvent evaporates, leaving the material in a “gum” state. During this process, the mandrel is held in a static upright position. Because the material is in a fluid state, a substantial amount runs off the mandrel due to gravity creating much waste, and the remaining material layer has uneven thicknesses. Multiple immersions are often required in order to achieve the desired wall thickness. After multiple immersions and devolatilization steps, the mandrel is presented for a curing process that converts the material from the gum state into a cross-linked elastomer.
  • the temperature typically between 35° C. and 60° C.
  • a mandrel 40 is supported on a rod 42 or other such elongated rigid holder.
  • the mandrel or rod is manipulated by an appropriate mechanical device that may a) rotate the mandrel and/or rod from the horizontal plane, b) rotate the mandrel and/or rod from the vertical plane, c) spin the mandrel about the rod's central axis, and/or d) transport the mandrel around the process equipment.
  • the central axis of the rod typically coincides with a central axis of the mandrel, defining an axis about which the resulting implant shell is axi-symmetric.
  • the mandrel 40 may rotate within a vertical plane about a first axis x so as to move from an upright position 180° through a horizontal plane to a fully inverted position. Also, the mandrel may translate around processing equipment along a second axis y. Furthermore, the mandrel may spin about a third axis z along the rod.
  • the mandrel and the rod are rotated, which provides some separation between the moving parts and the dipping tank or spray head.
  • various combinations, speeds, sequences of and pauses between movements are contemplated. Certain exemplary process steps are described below, but should not be considered limiting, and the present application encompasses a variety of specific steps to result in a uniform shell thickness.
  • areas of the shell may be made thicker by certain movements imparted to the mandrel, as will be appreciated by one of skill in the art, even though the most usual aim is to render uniform thickness.
  • FIGS. 4A-4C illustrate several steps in an exemplary process utilizing a dispersion curtain flow.
  • the mandrel 40 starts rotating about the rod axis at, e.g., 5-15 rpm just prior to entering a dispersion stream or curtain 50 emitted from a spigot 52 .
  • the dispersion stream curtain 50 shown may represent or otherwise be a substitute for a spray of dispersion, the terms spray and curtain being substantially synonymous in terms of defining a flow of dispersion that is directed onto or over the mandrels (as opposed to a stationary dipping tank).
  • the mandrel 40 then moves (at about 2 m/min, for example) through the dispersion curtain 50 while continuing to rotate about the rod axis, as seen in FIG. 4B .
  • the mandrel moves slowly enough so that the dispersion curtain falls on an upper generatrix thereof for at least 360° of mandrel rotation. Excess dispersion falls into a lower collection basin 54 for recycling of the dispersion material.
  • the mandrel may continue to rotate and pause while over the collection basin until no further excess drips off.
  • the mandrel is exposed to elevated devolatilization temperatures to help evaporate and drive off the solvent, again typically xylene. Continuously rotating the mandrel during the drying cycle further insures that there is no dispersion waste or drips.
  • the shell will typically be thickest at the central plane perpendicular to the axis of rotation.
  • the mandrel continues spinning about the rod axis during devolatilization, as seen in FIG. 4C , which does not illustrate an evaporating oven to indicate that devolatilization may also take place without heating.
  • the spinning motion creates centrifugal forces about the rod axis that effectively hold the dispersion on the mandrel surface, preventing material runoff and evening out the dispersion layer. This eliminates material waste and allows maximum thickness build for each pass, because thick and thin spots are evened out. That is, the volume of material that adheres to the mandrel efficiently covers the surface area, and the limiting factor that is the thinnest region extends around the mandrel (and is therefore simultaneously the thickest region).
  • the rotational speed will depend on the rheological properties of the dispersion material and surface tension between the mandrel surface and the dispersion. For example, a dispersion that has greater viscosity (thicker) will not drip from the mandrel quite as easily as one that is less viscous (thinner) and consequently will not require as fast a mandrel rotation. Likewise, the properties of both the dispersion and the mandrel surface (or the dispersion and an earlier formed layer) may affect the rotational speed. If the surface tension between the two is great, then the dispersion will be less likely to drip from the mandrel and a slower rotational speed may be utilized than if the surface tension was less.
  • dispersions of viscosities of 600 cps with low rheological properties result in much dispersion run-off and hence thin shells and those with high rheological properties result in poor dispersion flow and localized thick areas on the shell.
  • Rotational speeds in the region of about 10 rpm creates sufficient centrifugal energy to evenly spread high rheology silicone dispersions around the mandrel (whatever the mandrel shape) but is also of low enough speed not to allow the low rheology silicone dispersions to spray off the mandrel.
  • the mandrel is rotated at a speed of at least about 10 rpm for a silicone dispersion having a viscosity of about 600 centipoise.
  • rotational angles of about 0° to the horizontal will provide a substantially uniform thickness.
  • Shaped (e.g. anatomically shaped) mandrels may be positioned at a rotational angle of about +20° to about ⁇ 20°. If localized thickness if desired, the mandrel may be held at an appropriate angle while the rotation is slowed.
  • the mandrel shape may affect the design rotational speed, as well as the mandrel orientation.
  • breast implant shells may be formed to have an oval profile from the side, or more of a natural, teardrop shape.
  • the shell will be symmetric about at least one axis, which will affect the spinning speed and angular movement of the mandrel.
  • the spinning speed and angular movement of the mandrel may be altered to accommodate the contoured shape.
  • the mandrel may be held at different angles to the horizontal for periods of time to cause the dispersion to either more evenly cover the entire mandrel surface, or accumulate in one region or another.
  • FIG. 5 illustrates an overall system in accordance with the invention in which the dispersion curtain technique is employed.
  • a plurality of the mandrels 60 are mounted for translation or gross rotation on a conveyor or chain drive system, which is shown having two chains 62 , 64 that may be driven at the same or different speeds.
  • the chain drive system is shown positioned within a dipping hood 66 that provides a space in which devolatilization can occur, with or without heat.
  • External drive motors 68 outside of the dipping hood actuate the chain drive.
  • Each mandrel 60 periodically exits the dipping hood (through an aperture 70 shown on the left) and passes through a dispersion curtain 72 emitted from a spigot 74 .
  • a collection basin 76 catches runoff and provides for recycling of the dispersion material.
  • the mandrels are therefore coated in series with sequential layers of the dispersion. While waiting for another coat, the mandrels translate through the dipping hood for a period of time sufficient to evaporate at least some of the solvent from the last applied layer, preferably enough to form a gum state in the dispersion. During the evaporation process, the mandrels may be continually spun about their axes as well as tilted from a nominal horizontal orientation.
  • FIGS. 6A-6E schematically illustrate steps in a dip-molding process in accordance with the present application.
  • the mandrel commences spinning on the rod axis as well as translation and potentially other angular movement, as seen in FIG. 6A .
  • FIG. 6B shows the mandrel pausing over a container with a dispersion bath therein.
  • FIG. 6C shows the mandrel being inverted 90° from the horizontal to an orientation in which the mandrel is facing downward
  • FIG. 6D illustrates the mandrel being dipped in and out of the dispersion bath.
  • FIG. 6E shows the mandrel in its horizontal (or angled) orientation, removed from the dispersion bath and translating toward the devolatilization chamber, while continuing to rotate. The mandrel is then exposed to the elevated devolatilization temperatures in order to drive off the solvent while continually rotating about the rod axis.
  • FIG. 7 is a larger view of an entire system in accordance with an embodiment of the invention, in which a dispersion bath 80 is shown in the lower middle portion.
  • a circuit in which the mandrels travel includes first a load/unload section or chamber 82 prior to entering a dipping/drying section or chamber 84 . During the drying, the mandrels are continually or periodically spun about their axes, while optionally being tilted in other directions, again possibly depending on the mandrel shape and/or surface tension. The mandrels travel upward and then to the left through a devolatilization and curing section or chamber 86 .
  • the mandrels are desirably continuously spun to insure uniform thickness prior to evaporation of enough solvent to form a gum state in the dispersion. Finally, the mandrels descend back into the load/unload chamber 82 from where they may again enter the dipping/drying chamber 84 for application of the same or a different dispersion, or the process may be stopped if the last layer has been applied.
  • FIG. 8 shows a possible implementation of a chain drive for translating the mandrels around the several systems described herein.
  • Chain A traveling at a speed of X1 m/min acts on an upper side of a gripper 90 (through external cogs, e.g.) mounted to and rotating with the mandrel rod 92 .
  • Chain B traveling at a speed of X2 m/min acts on the lower side of the gripper 90 .
  • the overall translation direction of the mandrel is to the right, for instance at a speed of about 2 m/min, while velocity X1>X2 so that the mandrel spins about the rod/gripper axis in a clockwise direction, such as at a rate of about 5-15 rpm.
  • the entire chain drive system may be capable of tilting to reposition the mandrel at angles to the horizontal, or a mechanism within or connected to each mandrel rod may be utilized.

Abstract

Systems and methods for molding shells for fluid-filled prosthetic implants, including spinning and rotating dip- or spray-mandrels during a devolatilization step to ensure an even covering. The mandrels may be spun during the dipping or spraying step, and/or afterward while a solvent evaporates until a gum state is formed. The techniques are particularly useful for forming hollow shells from silicone dispersions for soft implants, such as breast implants.

Description

    CROSS-REFERENCE
  • This application is a continuation of U.S. patent application Ser. No. 13/867,821, filed Apr. 22, 2013, which is a continuation of U.S. patent application Ser. No. 12/621,700, filed Nov. 19, 2009, which claims the benefit of U.S. Provisional Patent Application No. 61/116,406, filed on Nov. 20, 2008, the entire disclosure of each of which is incorporated herein by this specific reference.
  • FIELD OF THE INVENTION
  • The present invention relates to systems and methods for molding shells for fluid-filled prosthetic implants and, more particularly, to techniques for forming uniform thickness shell walls, especially useful for breast implants.
  • BACKGROUND OF THE INVENTION
  • Implantable prostheses are commonly used to replace or augment body tissue. In the case of breast cancer, it is sometimes necessary to remove some or all of the mammary gland and surrounding tissue, creating a void that can be filled with an implantable prosthesis. The implant serves to support surrounding tissue and to maintain the appearance of the body. The restoration of the normal appearance of the body has an extremely beneficial psychological effect on post-operative patients, eliminating much of the shock and depression that often follows extensive surgical procedures. Implantable prostheses are also used more generally for restoring the normal appearance of soft tissue in various other areas of the body, such as the buttocks, chin, calf, etc.
  • Soft implantable prostheses typically include a relatively thin and quite flexible hollow envelope or shell made of vulcanized (cured) silicone elastomer. The shell is filled either with a silicone gel or with a normal saline solution. The filling of the shell takes place before or after the shell is inserted through an incision in the patient.
  • Traditional molding of implantable breast implant shells involves covering a mold (more typically called a mandrel) in uncured silicone dispersion through immersion into baths or by passing through a curtain of silicone dispersion and allowing the dispersion to flow over the mandrel just by utilizing gravimetric forces. Because the common method was to immerse or dip the mandrel into a bath of silicone dispersion, the process is commonly referred to as “dip-molding.” Other more recent developments are the use of spraying the dispersion onto mandrels, or by using rotational molding techniques. Whereas silicone (i.e., polysiloxane, a polymer in which the main chain consists of alternating silicon and oxygen atoms with organic side groups) is the most common material of construction, other materials such as polyurethane have been used.
  • FIGS. 1A-1C illustrate one early process for dip-molding flexible implant shells for implantable prostheses and tissue expanders, involving dipping a suitably shaped mandrel 20 into a silicone elastomer dispersion 22 of a silicone solution and a solvent. The mandrel 20 is withdrawn from the dispersion and the excess dispersion is allowed to drain from the mandrel. After the excess dispersion has drained from the mandrel at least a portion of the solvent (typically xylene) is allowed to evaporate to stabilize the silicone elastomer coating, forming a gum state. The process is then repeated several times until a shell of the desired thickness is formed. The layered structure characteristic of some silicone elastomer shells can be made by sequentially dipping the mandrel in different dispersions.
  • FIG. 2 illustrates an exemplary cross-section of a basic gel-filled breast implant 28, in which a shell 30 is initially formed by a process such as the above-described mandrel dipping process. The outer silicone elastomer shell 30 has an anatomical configuration, in this case matching the breast, and comes off a mold with a shell hole 32. In the illustrated embodiment, a patch over the shell hole 32 includes an uncured portion 34 directly over the hole and a cured portion 36 covering that and adhered to the inner surface of the shell 30. The patch is cured and then the hollow interior of the shell 30 is filled with an appropriate gel 38, such as via a needle hole in the patch. The silicone gel is supplied as a two-part liquid system with a primary gel component and a cross-linking component. The needle hole in the patch is then sealed with a silicone adhesive or plug, and the implant oven cured to achieve cross-linking of the gel.
  • Variations on the basic dip-molding technique are available. For example, U.S. Patent Publication No. 2004/0245671 to Smit discloses an automated system for dip molding silicone covers (shells) for breast implants in which an arm positions a mold to immerse an upper portion prior to total immersion thereof, ostensibly to eliminate air inclusions in the molded product. The system includes, in sequence, a cleaning station, a dipping station, an evaporating oven, and a curing oven. U.S. Patent Publication No. 2008/0208336 to Job includes the technique of spraying the silicone dispersion onto mandrels, one embodiment of which results in a nonuniform shell thickness.
  • Another process for forming implant shells is rotational molding, such as the system and methods described in U.S. Pat. No. 6,602,452 to Schuessler. The process also results in a flexible implant shell having a hole that requires a patch. Rotational molding provides a number of advantages to dip- or spray-molding, though the latter are currently more common in the industry.
  • Despite many advances in the construction of soft prosthetic implant shells, there remains a need for a simpler process that results in a more consistently uniform implant shell thickness.
  • SUMMARY OF THE INVENTION
  • The present application discloses methods and systems for molding soft shells for fluid-filled prosthetic implants, including spinning and rotating dip- or spray-mandrels during a devolatilization step to ensure an even covering. The mandrels may be spun during the dipping or spraying step, and/or afterward while a solvent evaporates until a gum state is formed. The techniques are particularly useful for forming hollow shells from silicone dispersions for soft implants, such as breast implants.
  • One method disclosed herein for molding a mammary prosthesis shell, includes providing a mandrel and rod assembly, the rod defining a first axis and the mandrel being in the shape of a breast implant shell. A silicone dispersion is applied to the mandrel, which is spun about the first axis. While being spun, the mandrel is moved from an upright position to an inverted position and back to the upright position. Furthermore, the spinning is performed while the silicone dispersion is solidifying on the mandrel. The spinning may be performed at a speed of about 5-15 rpm. The first axis may be at an angle of about 20° from a horizontal plane. Desirably, the step of moving comprises moving the mandrel and rod in a plane substantially perpendicular to a horizontal plane. Alternatively, the step of applying may be moving the mandrel through a curtain of the silicone dispersion, moving the mandrel through a spray of the silicone dispersion, or dipping the mandrel in the silicone dispersion.
  • Another method disclosed herein for molding a soft implant shell include providing a molding system including a devolatilization chamber, a plurality of mandrel and elongated holder assemblies, a conveyor to which the mandrel and elongated holder assemblies are mounted for translation, and a spray assembly capable of providing a silicone dispersion spray. The conveyors include a subsystem that can spin each mandrel about its respective central axis and rotate each mandrel within a vertical plane. Each mandrel translates into the path of the spray assembly and silicone dispersion spray is applied to the respective mandrels to form coated mandrels. Each coated mandrel then translates into the devolatilization chamber while the coated mandrel spins about its respective central axis and rotates within a vertical plane.
  • In the preceding method, each coated mandrel is desirably spun about its respective central axis at a rate of about 5-15 rpm. Further, each mandrel may be spun about its respective central axis while in the path of the spray assembly. In one embodiment, the spray assembly is located outside of the devolatilization chamber. For instance, the conveyor may be located within the devolatilization chamber which includes an aperture through which each mandrel passes into the path of the spray assembly. The spray assembly may have a spigot that produces a dispersion curtain through which the mandrels pass. In one preferred embodiment, the conveyor includes a pair of chain drives that engage a gripper attached to each elongated holder, and the chain drives are actuated at different speeds so as to spin each mandrel about its central axis. The mandrels may be continually spun about their central axes and tilted from a nominal horizontal orientation while in the devolatilization chamber.
  • A system for manufacturing breast implant shells is also disclosed herein, comprising:
  • a plurality of mandrel/rod assemblies;
    a rotating assembly capable of rotating the mandrel/rod assemblies about a plurality of different axes;
    a curing chamber containing the plurality of mandrel/rod assemblies;
    a spray assembly capable of providing a silicone dispersion spray; and
    a drive assembly capable of moving the each of the mandrel/rod assemblies into the silicone dispersion spray provided by the spray assembly and into the curing chamber.
  • The drive assembly desirably spins each of the mandrels about a central axis thereof. For example, the drive assembly may include two chain drives that engage a gripper attached to each mandrel, wherein the chain drives are actuated at different speeds so as to spin each mandrel about its central axis. The differential speeds of the chain drives may be such that each mandrel spins at a rate of about 5-15 rpm. Finally, the system may further include a load/unload chamber and a dipping/drying chamber, the wherein drive assembly moves each mandrel in a circuit including, in series, the load/unload chamber, the dipping/drying chamber, and the curing chamber.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Features and advantages of the present invention will become appreciated as the same become better understood with reference to the specification, claims, and appended drawings wherein:
  • FIGS. 1A-1C show several steps in a manual PRIOR ART process of dip-forming the shell of a breast implant prosthesis;
  • FIG. 2 is a sectional view through a typical gel-filled breast implant prosthesis;
  • FIGS. 3A-3C are schematic views of different modes of moving a mandrel used in the dip-or spray-forming methods of the present application;
  • FIGS. 4A-4C are schematic views of a shell forming method of the present application using a dispersion curtain;
  • FIG. 5 is a schematic view of an overall system of the present application for forming implant shells utilizing a dispersion curtain and a conveyor apparatus through a dipping hood;
  • FIGS. 6A-6E are schematic views of a sequence of steps in an exemplary dip-molding technique of the present application;
  • FIG. 7 is a schematic view of an overall system of the present application for forming implant shells utilizing a dip-molding technique; and
  • FIG. 8 is a schematic view of a shell-forming mandrel rotated and translated between two chain drives.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • The present invention provides improvements to previous dip- and spray-molding methods for forming soft, hollow implant shells, none of which reliably ensure that a uniform wall thickness is provided in the finished shell. Moreover, some of the methods disclosed are relatively complex, and therefore costly to implement. The hollow implant shells formed by the methods disclosed herein are intended to be filled with a fluid, such as saline, or a gel such as silicone gel.
  • One application for fluid-filled soft implants is to reconstruct or augment the female breast. Other potential applications are implants for the chin, buttocks, testes, or calf, among other areas. Moreover, though the present invention is particularly advantageous for breast implants, intragastric balloons and other implants may be formed by the methods described herein. Further, tissue expanders which may not be viewed as implants, per se, may also benefit from the concepts disclosed herein. For that matter, the term implant as used herein refers to long and short-term implanted devices.
  • The methods of the invention improve conventional dip and spray-molding techniques used to create shells for soft tissue implants. Because the flow of the silicone dispersion as it drains from a mandrel depends on the shape and orientation of the mandrel, the resulting shell can vary substantially in thickness if the orientation of the mandrel remains stationary. For example, the thickness of a breast implant shell formed by conventional dip casting on a stationary mandrel might vary from 0.009 to 0.024″ from one region to another, a variation of more than 100%. Importantly, the thickness of various regions of the shell is dictated for the most part by the shape of the mandrel and the orientation of the mandrel during the period that the silicone dispersion drains from the mandrel.
  • In dip molding the mandrel is held such that the portion corresponding to the anterior face of the shell faces downward. The bracket or rod used to hold the mandrel as it is dipped into the dispersion extends outward from that portion of the mandrel corresponding to the posterior face of the shell, such as seen in FIG. 1B for a manual process. The dispersion drains relatively rapidly from the perimeter region of the mandrel, and as a result the shell in the perimeter region tends to be thinner than the shell in the polar regions. For this reason, additional dips are required to create an adequate shell thickness in the perimeter region. This can result in shell that is thicker than desired in the polar regions, especially the anterior face. The same problems occur, though to a lesser extent because of the thinner application, with spray molding.
  • The present application describes mechanical equipment that, after the mandrel is immersed in silicone dispersion, rotates the mandrel about one or more different axes so that the dispersion spreads evenly across the mandrel surface utilizing the centrifugal forces obtained from the various spinning actions. More particularly, a preferred method is to spin the mandrel about its own axis while rotating it about one or more other axes.
  • In one embodiment, silicone is provided as a dispersion within a solvent such as xylene. The basic manufacturing process for forming a breast implant shell involves coating the mandrel in the uncured silicone dispersion, driving off the solvent (devolatilization), and then curing the material to convert it into an elastomer. It is during the step of driving off the solvent that most manufacturing issues occur, at least in terms of uneven thickness.
  • In accordance with prior art methods, in the context of a heat-cure silicone, the mandrel is immersed in the silicone dispersion and then placed into a chamber where the temperature is slightly elevated (typically between 35° C. and 60° C.) so that the solvent evaporates, leaving the material in a “gum” state. During this process, the mandrel is held in a static upright position. Because the material is in a fluid state, a substantial amount runs off the mandrel due to gravity creating much waste, and the remaining material layer has uneven thicknesses. Multiple immersions are often required in order to achieve the desired wall thickness. After multiple immersions and devolatilization steps, the mandrel is presented for a curing process that converts the material from the gum state into a cross-linked elastomer.
  • The present invention provides a process that overcomes at least some of the problems experienced in the prior art. In accordance with one embodiment, a mandrel 40 is supported on a rod 42 or other such elongated rigid holder. The mandrel or rod is manipulated by an appropriate mechanical device that may a) rotate the mandrel and/or rod from the horizontal plane, b) rotate the mandrel and/or rod from the vertical plane, c) spin the mandrel about the rod's central axis, and/or d) transport the mandrel around the process equipment. It should be noted that the central axis of the rod typically coincides with a central axis of the mandrel, defining an axis about which the resulting implant shell is axi-symmetric. Three of these potential movements are shown in FIGS. 3A-3C. For example, the mandrel 40 may rotate within a vertical plane about a first axis x so as to move from an upright position 180° through a horizontal plane to a fully inverted position. Also, the mandrel may translate around processing equipment along a second axis y. Furthermore, the mandrel may spin about a third axis z along the rod.
  • Although in some embodiments of the invention, it is the mandrel that is rotated about the rod, in other embodiments, the mandrel and the rod are rotated, which provides some separation between the moving parts and the dipping tank or spray head. Furthermore, various combinations, speeds, sequences of and pauses between movements are contemplated. Certain exemplary process steps are described below, but should not be considered limiting, and the present application encompasses a variety of specific steps to result in a uniform shell thickness. Finally, it should be understood that areas of the shell may be made thicker by certain movements imparted to the mandrel, as will be appreciated by one of skill in the art, even though the most usual aim is to render uniform thickness.
  • FIGS. 4A-4C illustrate several steps in an exemplary process utilizing a dispersion curtain flow. As seen in FIG. 4A, the mandrel 40 starts rotating about the rod axis at, e.g., 5-15 rpm just prior to entering a dispersion stream or curtain 50 emitted from a spigot 52. The dispersion stream curtain 50 shown may represent or otherwise be a substitute for a spray of dispersion, the terms spray and curtain being substantially synonymous in terms of defining a flow of dispersion that is directed onto or over the mandrels (as opposed to a stationary dipping tank).
  • The mandrel 40 then moves (at about 2 m/min, for example) through the dispersion curtain 50 while continuing to rotate about the rod axis, as seen in FIG. 4B. The mandrel moves slowly enough so that the dispersion curtain falls on an upper generatrix thereof for at least 360° of mandrel rotation. Excess dispersion falls into a lower collection basin 54 for recycling of the dispersion material. The mandrel may continue to rotate and pause while over the collection basin until no further excess drips off. After passing through the dispersion curtain, as in FIG. 4C, the mandrel is exposed to elevated devolatilization temperatures to help evaporate and drive off the solvent, again typically xylene. Continuously rotating the mandrel during the drying cycle further insures that there is no dispersion waste or drips. The shell will typically be thickest at the central plane perpendicular to the axis of rotation.
  • In some embodiments, the mandrel continues spinning about the rod axis during devolatilization, as seen in FIG. 4C, which does not illustrate an evaporating oven to indicate that devolatilization may also take place without heating. The spinning motion creates centrifugal forces about the rod axis that effectively hold the dispersion on the mandrel surface, preventing material runoff and evening out the dispersion layer. This eliminates material waste and allows maximum thickness build for each pass, because thick and thin spots are evened out. That is, the volume of material that adheres to the mandrel efficiently covers the surface area, and the limiting factor that is the thinnest region extends around the mandrel (and is therefore simultaneously the thickest region).
  • The rotational speed will depend on the rheological properties of the dispersion material and surface tension between the mandrel surface and the dispersion. For example, a dispersion that has greater viscosity (thicker) will not drip from the mandrel quite as easily as one that is less viscous (thinner) and consequently will not require as fast a mandrel rotation. Likewise, the properties of both the dispersion and the mandrel surface (or the dispersion and an earlier formed layer) may affect the rotational speed. If the surface tension between the two is great, then the dispersion will be less likely to drip from the mandrel and a slower rotational speed may be utilized than if the surface tension was less.
  • For example, it has been discovered by the present inventors that dispersions of viscosities of 600 cps with low rheological properties result in much dispersion run-off and hence thin shells and those with high rheological properties result in poor dispersion flow and localized thick areas on the shell. Rotational speeds in the region of about 10 rpm creates sufficient centrifugal energy to evenly spread high rheology silicone dispersions around the mandrel (whatever the mandrel shape) but is also of low enough speed not to allow the low rheology silicone dispersions to spray off the mandrel.
  • For example, in one embodiment, the mandrel is rotated at a speed of at least about 10 rpm for a silicone dispersion having a viscosity of about 600 centipoise. For round symmetrical mandrels, rotational angles of about 0° to the horizontal will provide a substantially uniform thickness. Shaped (e.g. anatomically shaped) mandrels may be positioned at a rotational angle of about +20° to about −20°. If localized thickness if desired, the mandrel may be held at an appropriate angle while the rotation is slowed.
  • Furthermore, the mandrel shape may affect the design rotational speed, as well as the mandrel orientation. For example, breast implant shells may be formed to have an oval profile from the side, or more of a natural, teardrop shape. In the former case, the shell will be symmetric about at least one axis, which will affect the spinning speed and angular movement of the mandrel. In the latter case, the spinning speed and angular movement of the mandrel may be altered to accommodate the contoured shape. Further, the mandrel may be held at different angles to the horizontal for periods of time to cause the dispersion to either more evenly cover the entire mandrel surface, or accumulate in one region or another.
  • FIG. 5 illustrates an overall system in accordance with the invention in which the dispersion curtain technique is employed. A plurality of the mandrels 60 are mounted for translation or gross rotation on a conveyor or chain drive system, which is shown having two chains 62, 64 that may be driven at the same or different speeds. The chain drive system is shown positioned within a dipping hood 66 that provides a space in which devolatilization can occur, with or without heat. External drive motors 68 outside of the dipping hood actuate the chain drive. Each mandrel 60 periodically exits the dipping hood (through an aperture 70 shown on the left) and passes through a dispersion curtain 72 emitted from a spigot 74. Once again, a collection basin 76 catches runoff and provides for recycling of the dispersion material. The mandrels are therefore coated in series with sequential layers of the dispersion. While waiting for another coat, the mandrels translate through the dipping hood for a period of time sufficient to evaporate at least some of the solvent from the last applied layer, preferably enough to form a gum state in the dispersion. During the evaporation process, the mandrels may be continually spun about their axes as well as tilted from a nominal horizontal orientation.
  • FIGS. 6A-6E schematically illustrate steps in a dip-molding process in accordance with the present application. The mandrel commences spinning on the rod axis as well as translation and potentially other angular movement, as seen in FIG. 6A. FIG. 6B shows the mandrel pausing over a container with a dispersion bath therein. FIG. 6C shows the mandrel being inverted 90° from the horizontal to an orientation in which the mandrel is facing downward, and FIG. 6D illustrates the mandrel being dipped in and out of the dispersion bath. As the mandrel starts to exit up from the dispersion bath, it starts spinning about the rod axis and optionally takes up an angle to the horizontal appropriate to the particular mandrel shape. Finally, FIG. 6E shows the mandrel in its horizontal (or angled) orientation, removed from the dispersion bath and translating toward the devolatilization chamber, while continuing to rotate. The mandrel is then exposed to the elevated devolatilization temperatures in order to drive off the solvent while continually rotating about the rod axis.
  • FIG. 7 is a larger view of an entire system in accordance with an embodiment of the invention, in which a dispersion bath 80 is shown in the lower middle portion. A circuit in which the mandrels travel includes first a load/unload section or chamber 82 prior to entering a dipping/drying section or chamber 84. During the drying, the mandrels are continually or periodically spun about their axes, while optionally being tilted in other directions, again possibly depending on the mandrel shape and/or surface tension. The mandrels travel upward and then to the left through a devolatilization and curing section or chamber 86. As explained above, the mandrels are desirably continuously spun to insure uniform thickness prior to evaporation of enough solvent to form a gum state in the dispersion. Finally, the mandrels descend back into the load/unload chamber 82 from where they may again enter the dipping/drying chamber 84 for application of the same or a different dispersion, or the process may be stopped if the last layer has been applied.
  • FIG. 8 shows a possible implementation of a chain drive for translating the mandrels around the several systems described herein. Chain A traveling at a speed of X1 m/min acts on an upper side of a gripper 90 (through external cogs, e.g.) mounted to and rotating with the mandrel rod 92. Chain B traveling at a speed of X2 m/min acts on the lower side of the gripper 90. The overall translation direction of the mandrel is to the right, for instance at a speed of about 2 m/min, while velocity X1>X2 so that the mandrel spins about the rod/gripper axis in a clockwise direction, such as at a rate of about 5-15 rpm. The entire chain drive system may be capable of tilting to reposition the mandrel at angles to the horizontal, or a mechanism within or connected to each mandrel rod may be utilized.
  • Although the invention has been described and illustrated with a certain degree of particularity, it is understood that the present disclosure has been made only by way of example, and that numerous changes in the combination and arrangement of parts can be resorted to by those skilled in the art without departing from the scope of the invention, as hereinafter claimed.

Claims (11)

What is claimed is:
1. A method for molding a hollow shell useful as a surgical implant, the method comprising the steps of:
providing an assembly comprising a mandrel and rod, the rod defining a first axis of the assembly;
spinning the mandrel about the first axis;
rotating the mandrel about a second axis different from the first axis;
applying a silicone dispersion to the mandrel by passing the mandrel through a silicone dispersion flow during the spinning to form a silicone dispersion coat on the mandrel; and
causing the coat to devolatize.
2. The method of claim 1 wherein the spinning is performed at a speed of about 5-15 rpm.
3. The method of claim 1 wherein the rotating comprises moving the mandrel between an upright and an inverted position.
4. The method of claim 1 wherein the step of causing the coat to devolatize is performed during the rotating.
5. The method of claim 1 wherein the step of causing the coat to devolatize is performed during the spinning.
6. The method of claim 1 wherein the step of causing the coat to devolatize is performed during the spinning and the rotating.
7. The method of claim 1 wherein the silicone dispersion flow is a silicone dispersion curtain.
8. A system for manufacturing shells useful as surgical implants, the system comprising:
a plurality of mandrel/rod assemblies, each including a rod and a mandrel;
a rotating assembly capable of rotating the mandrel/rod assemblies about a plurality of different axes including spinning each mandrel about a respective first axis;
a spray assembly capable of providing a dispersion spray;
a devolatization chamber; and
a drive assembly capable of moving the each of the mandrel/rod assemblies into the dispersion spray to form a dispersion coat on each mandrel, and capable of moving each of the mandrel/rod assemblies into the devolatization chamber such that each mandrel passes into the devolatization chamber while being rotated about the plurality of different axes.
9. The system of claim 8, wherein the drive assembly comprises chain drives which engage the mandrel/rod assemblies.
10. The system of claim 8, wherein the rotating assembly spins each mandrel about its respective first axis at a rate of about 5-15 rpm.
11. The system of claim 8 wherein the devolatization chamber provides an elevated temperature for driving off solvent from the dispersion coat.
US14/223,875 2008-11-20 2014-03-24 System and method for molding soft fluid-filled implant shells Abandoned US20140203478A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US14/223,875 US20140203478A1 (en) 2008-11-20 2014-03-24 System and method for molding soft fluid-filled implant shells

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US11640608P 2008-11-20 2008-11-20
US12/621,700 US8431179B2 (en) 2008-11-20 2009-11-19 System and method for molding soft fluid-filled implant shells
US13/867,821 US8703230B2 (en) 2008-11-20 2013-04-22 System and method for molding soft fluid-filled implant shells
US14/223,875 US20140203478A1 (en) 2008-11-20 2014-03-24 System and method for molding soft fluid-filled implant shells

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US13/867,821 Continuation US8703230B2 (en) 2008-11-20 2013-04-22 System and method for molding soft fluid-filled implant shells

Publications (1)

Publication Number Publication Date
US20140203478A1 true US20140203478A1 (en) 2014-07-24

Family

ID=42133787

Family Applications (3)

Application Number Title Priority Date Filing Date
US12/621,700 Active 2031-08-21 US8431179B2 (en) 2008-11-20 2009-11-19 System and method for molding soft fluid-filled implant shells
US13/867,821 Active US8703230B2 (en) 2008-11-20 2013-04-22 System and method for molding soft fluid-filled implant shells
US14/223,875 Abandoned US20140203478A1 (en) 2008-11-20 2014-03-24 System and method for molding soft fluid-filled implant shells

Family Applications Before (2)

Application Number Title Priority Date Filing Date
US12/621,700 Active 2031-08-21 US8431179B2 (en) 2008-11-20 2009-11-19 System and method for molding soft fluid-filled implant shells
US13/867,821 Active US8703230B2 (en) 2008-11-20 2013-04-22 System and method for molding soft fluid-filled implant shells

Country Status (11)

Country Link
US (3) US8431179B2 (en)
EP (2) EP2379298B1 (en)
KR (1) KR20110103964A (en)
CN (1) CN102256762A (en)
AR (1) AR075357A1 (en)
AU (1) AU2009316547A1 (en)
BR (1) BRPI0921104A2 (en)
CA (1) CA2744062A1 (en)
ES (1) ES2397688T3 (en)
RU (1) RU2011124178A (en)
WO (1) WO2010059834A2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016077160A1 (en) * 2014-11-12 2016-05-19 Applied Silicone Company Immersion curing process

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2333523B1 (en) 2001-04-30 2020-04-08 The General Hospital Corporation Method and apparatus for improving image clarity and sensitivity in optical coherence tomography using dynamic feedback to control focal properties and coherence gating
RU2011124178A (en) * 2008-11-20 2012-12-27 Аллерган, Инк. METHOD FOR FORMING A SOFT SHELL FOR A FILLABLE FLOW IMPLANT MEDIA AND THE RELATED INSTALLATION
US9402760B2 (en) 2010-08-18 2016-08-02 Christopher Burnside Gordon In situ molded orthotic and method for its fabrication
KR20120032392A (en) * 2010-09-28 2012-04-05 유원석 Process of silicon implant having shell improved durability
AU2012258531B2 (en) 2011-05-26 2015-07-16 Advenira Enterprises, Inc. System and process for coating an object
SG10201608125WA (en) 2012-04-02 2016-11-29 Thomas West Inc Methods and systems for centrifugal casting of polymer polish pads and polishing pads made by the methods
US10722997B2 (en) * 2012-04-02 2020-07-28 Thomas West, Inc. Multilayer polishing pads made by the methods for centrifugal casting of polymer polish pads
US10022842B2 (en) 2012-04-02 2018-07-17 Thomas West, Inc. Method and systems to control optical transmissivity of a polish pad material
US10820984B2 (en) 2012-11-14 2020-11-03 ImplantADJUST, LLC Implant with elastomeric membrane and methods of fabrication thereof
US9351824B2 (en) 2012-11-14 2016-05-31 ImplantADJUST, LLC Adjustable implant with self-sealing elastomeric membrane and methods of fabrication thereof
CA2895083A1 (en) * 2012-12-13 2014-06-19 Allergan, Inc. Device and method for making a variable surface breast implant
ITPI20130015A1 (en) 2013-03-07 2014-09-08 S M Scienzia Machinale S R L EQUIPMENT AND METHOD FOR THE PRODUCTION OF A BIO-COMPATIBLE THREE-DIMENSIONAL OBJECT
US20160052178A1 (en) * 2014-08-21 2016-02-25 Applied Silicone Corporation Automated prosthesis shell system and method
WO2017042627A1 (en) 2015-09-11 2017-03-16 S.M. Scienzia Machinale S.R.L. Apparatus and method for producing a biocompatible three-dimensional object
WO2020214328A2 (en) * 2019-03-19 2020-10-22 University Of Pittsburgh - Of The Commonwealth System Of Higher Education Automation mechanism for pre/clinical production of resorbable nerve guides
KR102580385B1 (en) * 2021-02-25 2023-09-21 오스템임플란트 주식회사 The manufacturing method of the silicone artificial breast prosthesis
KR102580384B1 (en) * 2021-02-25 2023-09-21 오스템임플란트 주식회사 The manufacturing method of the silicone artificial breast prosthesis
US11357614B1 (en) 2021-06-11 2022-06-14 Marcel Malek Breast implant

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1398131A1 (en) * 2002-09-12 2004-03-17 Polyzen, Inc. Dip-molded polymeric medical devices with reverse thickness gradient and dip molding process
US8431179B2 (en) * 2008-11-20 2013-04-30 Allergan, Inc. System and method for molding soft fluid-filled implant shells

Family Cites Families (76)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2128827A (en) 1938-03-09 1938-08-30 Frank B Killian Method and apparatus for manufacturing thin rubber articles
US2469892A (en) 1947-09-10 1949-05-10 Rempel Entpr Hollow article and method and apparatus for producing the same
GB702146A (en) 1950-11-10 1954-01-13 Chad Valley Company Ltd A new or improved process for the production of dolls and other toys
US2804643A (en) 1955-03-21 1957-09-03 Theodore A Miller Vacuum extractor apparatus for removing hollow flexible molded articles from reentrant mold cavities
US3652748A (en) 1965-05-14 1972-03-28 Arthur H Roberts Process for preparing molded hollow articles
US3439079A (en) 1966-05-16 1969-04-15 Gen Electric Molding hollow articles
GB1192360A (en) 1966-09-28 1970-05-20 Courtaulds Ltd The Centrifugal Casting of Rollers
GB1206110A (en) 1966-12-19 1970-09-23 Courtaulds Ltd Cast wheels
US4043721A (en) 1968-07-11 1977-08-23 Lemelson Jerome H Composite body molding apparatus
GB1306541A (en) 1969-01-20 1973-02-14 Ceskoslovenska Akademie Ved Method of manufacturing tubes by centrifugal casting
US3652368A (en) 1969-12-17 1972-03-28 Plastics Inc Apparatus for rotational molding of laminated hollow structures
US3584105A (en) 1970-01-14 1971-06-08 Pekor Iron Works Method of centrifugally forming hollow articles
BE757080A (en) 1970-04-03 1971-03-16 Giehler Herbert PROCESS AND DEVICE FOR THE MANUFACTURING OF HOLLOW PARTS OF HERMOPLASTIC MATERIAL BY ROTATIONAL MOLDING IN MELTED STATE
US3683062A (en) 1970-08-20 1972-08-08 Essex International Inc Rotational casting method
US3788382A (en) 1970-11-25 1974-01-29 J Richey Vacuum metal casting apparatus
DE2160124A1 (en) 1971-01-08 1972-08-24 Monster Molding Ltd Process for the rotary pressing of moldings at room temperature
US3925530A (en) 1971-02-08 1975-12-09 Phillips Petroleum Co Release coating for molds
GB1434345A (en) 1972-04-26 1976-05-05 Quraishi A H Rotational moulding
US3883902A (en) 1972-08-16 1975-05-20 Medical Eng Corp Variable volume prosthetic assembly
US3850368A (en) 1973-02-12 1974-11-26 Kennametal Inc Apparatus for centrifugal compaction
DE2530211C2 (en) 1975-07-07 1983-12-01 Elkamet-Werk Lahn-Kunststoff Gmbh, 3560 Biedenkopf Method and device for the production of hollow bodies from thermoplastic material by rotary melting
FR2397931A1 (en) 1977-07-22 1979-02-16 Thomson Brandt PROCESS FOR REPRODUCING AN INFORMATION MEDIA DISC AND DISC OBTAINED BY SUCH A PROCESS
US4285903A (en) 1977-08-29 1981-08-25 Lemelson Jerome H Molding system
DE2756384C3 (en) 1977-12-17 1981-09-10 Reitberger, Ernst, 7030 Böblingen Device for producing hollow bodies from thermoplastic material
JPS6015454B2 (en) 1980-10-29 1985-04-19 北辰工業株式会社 Manufacturing method of thin endless belt
DE3171145D1 (en) 1980-12-12 1985-08-01 Beiersdorf Ag Mammary prosthesis
US4416841A (en) 1981-03-11 1983-11-22 Corea John E Method for centrifugal casting of thermosetting plastics
US4624818A (en) 1982-03-25 1986-11-25 Allied Corporation Rotational molding process using abrasive-resistant nylon composition
US4548779A (en) 1982-11-15 1985-10-22 Allied Corporation Rotational molding multilayered articles
US4836963A (en) 1984-05-01 1989-06-06 Old Town Canoe Company Rotational molding method
US4956133A (en) 1985-08-19 1990-09-11 Le Roy Payne Continuous molding apparatus and method
US6511619B1 (en) 1985-08-19 2003-01-28 Payne Leroy Multiaxis rotational molding apparatus and method
US5316701A (en) 1985-08-19 1994-05-31 Payne Leroy Multiaxis rotational molding process
US5188845A (en) 1985-08-19 1993-02-23 Payne Leroy Multiaxis rotational molding apparatus
US6030557A (en) 1985-08-19 2000-02-29 Payne; Leroy Multiaxis rotational molding method, apparatus and structure
FR2590836B1 (en) 1985-12-02 1988-04-15 Luchaire Sa METHOD AND MACHINE FOR MANUFACTURING HOLLOW PARTS OF PLASTIC MATERIAL, BY ROTATING
US4865787A (en) 1986-07-17 1989-09-12 General Electric Company Method for the impregnation of filament wound structures with thermoplastic binders
US4796686A (en) 1986-08-20 1989-01-10 Gayso Donald W Centrifugal casting machine with venturi actuated vacuum venting
US4960425A (en) 1987-05-27 1990-10-02 Mentor Corporation Textured surface frosthesis implants
US4990299A (en) 1987-11-02 1991-02-05 Primtec Multi-parting molding system with clamping means
GB8820945D0 (en) 1988-09-07 1988-10-05 Smith & Nephew Medical articles
US4882107A (en) 1988-11-23 1989-11-21 Union Carbide Chemicals And Plastics Company Inc. Mold release coating process and apparatus using a supercritical fluid
US4992312A (en) 1989-03-13 1991-02-12 Dow Corning Wright Corporation Methods of forming permeation-resistant, silicone elastomer-containing composite laminates and devices produced thereby
CA2023922A1 (en) * 1989-09-05 1991-03-06 James M. Curtis Method of manufacturing an implantable article provided with a micropillared surface
US5035601A (en) 1990-02-21 1991-07-30 Lin Chao Tung Hollow forming machine capable of rotating mould in both horizontal and vertical direction
US5091445A (en) 1990-05-04 1992-02-25 Dow Corning Corporation Silicone sealants
US5346660A (en) 1990-09-07 1994-09-13 Toto Ltd. Method of manufacturing powder molding
US5096627A (en) 1990-09-17 1992-03-17 Minnesota Mining And Manufacturing Company Method of molding optical recording drums
US5156818A (en) 1990-11-16 1992-10-20 Alternative Technologies For Waste, Inc. Biaxial casting apparatus for isolating radioactive waste
US5795325A (en) 1991-07-16 1998-08-18 Heartport, Inc. Methods and apparatus for anchoring an occluding member
US5376117A (en) 1991-10-25 1994-12-27 Corvita Corporation Breast prostheses
EP0612333B1 (en) 1991-11-15 2001-01-10 Imperial Chemical Industries Plc Polyomerisable compositions
JP2969311B2 (en) 1992-08-31 1999-11-02 タキロン株式会社 Gel-like elastic body
US5356589A (en) 1993-03-09 1994-10-18 Essef Corporation Method and apparatus for forming rotationally cast tank liner having an end fitting
US5519082A (en) 1994-04-13 1996-05-21 Shin-Etsu Chemical Co., Ltd. Curable silicone rubber composition and method for preparing silicone rubber
DE4413076A1 (en) 1994-04-15 1995-10-19 Amoena Med Orthopaedie Tech Process for the manufacture of breast prostheses
US5525274A (en) 1994-06-29 1996-06-11 Davidson Textron Inc. Process for manufacturing plastic microspheres
JP3761222B2 (en) 1994-08-05 2006-03-29 エルカメート・クンストシユトッフテヒニック・ゲゼルシヤフト・ミト・ベシユレンクテル・ハフツング An apparatus for making hollow bodies by rotational melting from a flowable dry thermoplastic synthetic resin.
KR19990044338A (en) 1995-08-29 1999-06-25 만셀 케이쓰 로드니 Radiation-resistant polypropylene and articles made therefrom
US5665069A (en) 1996-07-19 1997-09-09 Cumer; Patricia Lynn Pressure-directed peribulbar anesthesia delivery device
US5705110A (en) 1996-09-09 1998-01-06 Centro Incorporated Process for reducing cross link vapors from rotomolded products made of cross link polyethlylene
US5935164A (en) 1997-02-25 1999-08-10 Pmt Corporaton Laminated prosthesis and method of manufacture
US6180203B1 (en) 1997-04-09 2001-01-30 Peter J. Unkles Rotational moulding process
JP3743787B2 (en) 1997-09-03 2006-02-08 東ソー株式会社 Polyethylene resin for high-purity chemical containers and high-purity chemical containers comprising the same
US6177034B1 (en) 1998-04-03 2001-01-23 A-Pear Biometric Replications Inc. Methods for making prosthetic surfaces
US6214272B1 (en) 1998-07-14 2001-04-10 Brunswick Corporation Rotational molding process
US6329444B1 (en) 1998-10-14 2001-12-11 Apex Medical Technologies, Inc. Dip-molded medical devices from cis-1,4-polyisoprene
US6231547B1 (en) 1999-02-18 2001-05-15 Abbott Laboratories External retaining device for a catheter and catheter assembly and method using same
JP2001029475A (en) 1999-07-23 2001-02-06 Kanegafuchi Chem Ind Co Ltd Hemophoresis balloon catheter
US6409954B1 (en) 1999-10-05 2002-06-25 Roto Plastics, Inc. Method of making a rotary molded plastic member with variable wall thickness
US6692527B1 (en) * 1999-12-01 2004-02-17 Howard T. Bellin Non-rotating breast implant
US6291543B1 (en) 2000-05-24 2001-09-18 Polyzen, Inc. Surfacially cross-linked elastoplastic articles, and method of making the same
US6602452B2 (en) 2001-07-18 2003-08-05 Mcghan Medical Corporation Rotational molding of medical articles
NL1019023C2 (en) * 2001-09-24 2003-03-25 Mentor Medical Systems B V Device and method for manufacturing a silicone sheath for a breast implant.
US6780366B2 (en) * 2002-08-15 2004-08-24 Mentor Corporation Drip retainer
US7758788B2 (en) * 2004-08-13 2010-07-20 Mentor Worldwide Llc Spray method for forming shells for prostheses

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1398131A1 (en) * 2002-09-12 2004-03-17 Polyzen, Inc. Dip-molded polymeric medical devices with reverse thickness gradient and dip molding process
US8431179B2 (en) * 2008-11-20 2013-04-30 Allergan, Inc. System and method for molding soft fluid-filled implant shells
US8703230B2 (en) * 2008-11-20 2014-04-22 Allergan, Inc. System and method for molding soft fluid-filled implant shells

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016077160A1 (en) * 2014-11-12 2016-05-19 Applied Silicone Company Immersion curing process

Also Published As

Publication number Publication date
WO2010059834A3 (en) 2010-11-25
KR20110103964A (en) 2011-09-21
AR075357A1 (en) 2011-03-30
US20100178414A1 (en) 2010-07-15
US8703230B2 (en) 2014-04-22
AU2009316547A1 (en) 2010-05-27
US20130234365A1 (en) 2013-09-12
RU2011124178A (en) 2012-12-27
US8431179B2 (en) 2013-04-30
CA2744062A1 (en) 2010-05-27
BRPI0921104A2 (en) 2016-02-16
CN102256762A (en) 2011-11-23
EP2511062A1 (en) 2012-10-17
ES2397688T3 (en) 2013-03-08
EP2379298A2 (en) 2011-10-26
WO2010059834A2 (en) 2010-05-27
EP2379298B1 (en) 2012-10-31

Similar Documents

Publication Publication Date Title
US8703230B2 (en) System and method for molding soft fluid-filled implant shells
US8562677B2 (en) Spray method for forming shells for prostheses
CA2733925C (en) Soft filled prosthesis shell with discrete fixation surfaces
AU617667B2 (en) Open-cell, silicone-elastomer medical implant and method for making
US5674285A (en) Mammary implant having shell with unitary rough-textured outer layer
AU2020202242A1 (en) Soft filled prosthesis shell with variable texture
US5007929A (en) Open-cell, silicone-elastomer medical implant
KR20120032392A (en) Process of silicon implant having shell improved durability
KR20110057155A (en) Soft filled prosthesis shell with discrete fixation surfaces
KR101021668B1 (en) art breast manufacture method for minimize of stress-concentration.
Luis et al. Silicone 3D printing technologies and processes: a review
EP3711709A1 (en) Soft filled prosthesis shell with variable texture

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION