US2924312A - Punch and die assembly for making interlocking integral fasteners - Google Patents

Punch and die assembly for making interlocking integral fasteners Download PDF

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US2924312A
US2924312A US710832A US71083257A US2924312A US 2924312 A US2924312 A US 2924312A US 710832 A US710832 A US 710832A US 71083257 A US71083257 A US 71083257A US 2924312 A US2924312 A US 2924312A
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pieces
incisions
punch
fastener
segments
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D39/00Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
    • B21D39/03Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders of sheet metal otherwise than by folding
    • B21D39/035Joining superposed plates by slitting
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49833Punching, piercing or reaming part by surface of second part
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49915Overedge assembling of seated part
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49936Surface interlocking
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49938Radially expanding part in cavity, aperture, or hollow body
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/49Member deformed in situ
    • Y10T403/4974Member deformed in situ by piercing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/71Rod side to plate or side

Definitions

  • the resulting fastener resists separation of the overlying pieces of material by a force exerted perpendicular to the plane of the material and by a force exerted in a plane parallel to the plane thereof but transversely of the fastener, it does not resist to so great an extent their separation by the application of a force exerted in the plane of the material but longitudinally of the fastener.
  • the overlying displaced section may be slipped along the underlying displaced section, thereby separating the pieces.
  • a force of 2000 pounds is required to separate the pieces when applied in a direction normal to the plane thereof, a force of about 1100 pounds may be sucient to separate them if it is applied in the plane of the pieces but longitudinally of the fastener.
  • Still another object of this invention is the provision of an integral fastener for uniting overlying pieces of material which is characterized by the presence of interlocking edges which lock the pieces together so that they are resistant to separation by a force applied from any direction.
  • Still another object of this invention is the provision of a method of forming an integral, interlocking fastener for uniting overlying pieces of material which method may be carried out rapidly and eiiiciently.
  • Figure 1 is a view in end elevation of a punch and die which may be used for forming the presently described fastener
  • Figure 2 is a view in side elevation of the punch and die of Figure 1;
  • Figure 3 is an end view of the die of Figures 1 and 2 as viewed from the line 3 3 of Figure 2;
  • Figure 4 is a plan view of the interlocked fastener which is produced by the operation of the punch and die of Figures l-3;
  • Figure 5 is a longitudinal sectional view of the fastener of Figure 4 taken along the line 5 5 of that ligure;
  • Figure 6 is a transverse sectional view of the fastener of Figure 4 taken along the line 6--6 of that ligure;
  • Figures 7 and 8 are plan v1ews of alternate forms of fasteners which may be produced by the presently described method.
  • the presently described method for forming an integral fastener through overlying pieces of material comprises first forming laterally spaced apart, substantially aligned incisions through the pieces, the distance between selected opposite segments of the incisions being greater than that between other opposite segments thereof.
  • the incisions may be outwardly offset so that the distance between the central segments thereof will be greater than that between the terminal segments.
  • FIG. l-3 A punch and die assembly which may be employed in forming the presently described fastener is illustrated in Figures l-3.
  • the assembly comprises a die member and a punch member.
  • Plhe die member includes a body 10, one end of which is formed with a pair of spaced apart shoulders 12, 14. This end lof the die body also has a pair of spaced apart recesses 16, 18 lying p outside of the shoulders and a central longitudinal opening 20.
  • An anvil 22 is connected to the body of the die,
  • cutting elements 34, 36 Positioned against side faces 26, 28 respectively of the anvil are cutting elements 34, 36. These are formed with recesses 38, 40 which are complementary to projections 30, 32 on the anvil.
  • the inner ends of the cutters abut against shoulders 12, 14 of the die body.
  • Means are provided for maintaining cutters 34, 36 pressing resiliently against the side' ⁇ faces of the anvil and for releasably securing them tothe die body.
  • a preferred means of accomplishing these functions comprises attaching the cutters to resilient tongues 46, 50.
  • the latter preferably are formed integrally with the cutters, as by recessing the latter at 52, 54 and forming the material defined in part by the recesses into outwardly bowed tongues in Vthe manner indicated.
  • the punch sectionV of the assembly which cooperates withv the die in forming fasteners through the, Aoverlying pieces of material includes a body portion 60 and a punch portion 62.
  • the latter is formed with a working surface 64, angular forming sections 66, 68 and longitudinal projections 70, 72 along its opposite side faces.
  • the configuration of the working surface of the punch thus conforms generally to that of the working surface of the anvil.
  • overlying pieces of material for example, sheets of aluminum 80, 82 are placed between the punch and die.
  • the punchthen is advanced towards the die whereupon its forms a pair of laterally spaced apart, substantially aligned incisions completely through the overlying pieces of material.
  • the pattern of these incisions is particularly apparent from Figure 4. Y
  • one pai-r of overlying incisions comprises the outer segment 84, 86 and a central,
  • outwardly offset segment 88 These segments are inter ⁇ connected by the angled connecting segments 90, 92, the angle preferably being about 45.
  • the configuration of the companion pair of overlying incisions is similar. Accordingly, it is made up of vthe terminal segments V94, 96 and the outwardly offset, central segment 98, these being interconnected by the connecting segmentV 100, 102.
  • the pattern of the incisions may be varied however, by
  • the pattern of the incisions may be as is illustrated in Figure 7.
  • one of the incisions is made up of terminal segments 104, 106 and a central segment 108, the companion incision being composed of terminal segments 110, 112I and the central segment 114.
  • the pairs 104, 110 and 106, ⁇ 112 of the terminal segments are angled slightly toward each other, while the central segmentsA 108, 114' are maintained substantially parallel.
  • the incisions may assume the ⁇ pattern o-f Figure 8.
  • the central segments of the incisions are inwardly offset.
  • one of the incisions comprises the terminal Vsegments 116, 118, the central. segment 120 and the connecting segments 122, 124 ⁇
  • the other incision is4 complementary, being made up of the terminal segments 126, 128, the inwardly oiset itralsegment 130 and the Aconnecting segments 132,
  • contmuedadvancement of the punch causes displaQQmGIlt, f
  • edges 90,92 and 100,102 resist separation of the pieces force.l -For example, if an integral 'fastener not having the presently described interlock will withstand a lateral force of 2000. pounds and a longitudinal force of about the material betweenA the spaced incisions until sections 140, 142 are completely displaced below the plane of the bottom surface of the underlying sheet 82. During this process the end sections of the material between the spaced incisions are stretched and deformed to conform to the configuration of theforming surfaces 66, 68 of r the punch.
  • edges 144,V ⁇ 146 resist lateral separation ofthe pieces as well as separa-tion by a force exerted in the plane of the fastener, but normall to the longitudinal axis thereof. Also, the interlocked angular by a force exerted .in the plane of the ⁇ fastener but in a directionlongitudinally of the axis thereof.
  • the fastener is of substantial strength irrespective of the directionof application of a disrupting 1100 pounds without breaking, a fastener ofthe presently described class which will withstand a lateral force of 2000 pounds will withstand a longitudinal force of about 1900 pounds.
  • the longitudinal strength of the vfastener has been increased by about 70% and its usefulness augmented accordingly'.
  • a fastener-for uniting overlying pieces of material which comprises integral portions of the pieces defined ⁇ ments, the distancebetween a pair of selected opposed segments of the incisions being greater than that between the other opposed segments, said portions being dis- ⁇ i placed so that the displacedfportion of one of the pieces lies beyond the plane of the outer surface of the other of ⁇ the pieces, the displacedportion of ⁇ said one of the pieces ⁇ being. spread laterally until its margins underlie thesaid other ofthe pieces, thereby securely interlocking the piecesandl preventing their separation.
  • a fastener for ⁇ uniting overlying pieces of material which comprises integral portions' of the pieces defined by a pair of laterally spaced apart, substantially aligned incisions through the pieces, each of the incisions comprising' an" intermediate segmentand terminal segments ⁇ connected 4"thereto, the terminal ⁇ "segments beingsubsta'ntially parallel to the intermediatey segment, the intermediate' segment of at leastonerof the incisions being offset ⁇ from the terminalfsegments, thereof, said portions being displaced sio'that the displaced portion of one of thapieces lies beyondthe plane of the outersurface of the other of the pieces, theV displaced portion of said one of the pieces being spread laterally until its margins underlie the said other of the pieces, thereby securely interlocking the pieces and preventing their separation.
  • a fastener for uniting overlying pieces of material which comprises integral portions of the peces dened by a pair of laterally spaced apart, substantially aligned incisions through the pieces, each of the incisions comprising an intermediate straight-line segment and terminal straight-line segments connected thereto, the terminal segments being substantially parallel to the intermediate segment, the intermediate segments of both of the incisions being outwardly offset from the terminal segments thereof, said portio-ns being displaced so that the displaced portion of one of the pieces lies beyond the plane of the outer surface of the other of the pieces, the displaced portion of said one of the pieces being spread laterally until its margins underlie the said other of the nieces, thereby securely interlocking the pieces and preventing their separation.
  • the method of uniting overlying pieces of material through an integral fastener which comprises forming a pair of laterally spaced apart substantially aligned incisions through the pieces with each of the incisions having an intermediate segment and terminal segments connected thereto in parallel relation, the intermediate segments of both of the incisions being outwardly oiset from the terminal segments thereof, deforming the material between the incisions outwardly until the displaced portion of one of the pieces lies beyond the outer surface of the other of the pieces, spreading the displaced portion of said one of the pieces until it underlies the outer surface of the other of the pieces, thereby securely interlocking the pieces and preventing their separation.

Description

ILLIAMs 2,924,312
l. A. W PUNCH AND DIE ASSEMBLY FOR MAKING INTERLOCKING INTEGRAL FASTENERS Original Filed NOV. 29. 1954 Feb. 9, 1960 I IN VEN TOR.
United States Patent() PUNCH AND DIE ASSEMBLY FOR MAKING IN- TERLOCKING INTEGRAL FASTENERS Ivan A. Williams, Portland, Oreg.
Original application November 29, 1954, Serial No. 471,808. Divided and this application December 23, 1957, Serial No. 710,832
5 Claims. (Cl. 189-36) ing Element and Method of Making the Same, and my U.S. Letters Patent 2,288,308, issued June 3.0, 1942 for Punch and Die. This application is a division of my abandoned application Serial No. 471,808, filed November 29, 1954.
rl`he aforesaid Letters Patent disclose a method of uniting overlying sheets of material by means of a punch and die which operate to form spaced incisions entirely through both thicknesses of the material. Next the sections of the material between the incisions are deformed in the direction of motion of the advancing punch until substantial portions lie beyond the plane of that surface of the material which is adjacent the die. This deformation is accompanied by stretching and bending portions of the material at the end zones between the spaced incisions in a pattern conforming to the shape of the punch.
The central sections of the deformed portions then are pressed against the anvil of the die by the punch with the result that they are swaged and extruded laterally. In this manner there are formed laterally extending edges which span the incisions and underlie the undisplaced material on each side thereof, preventing retraction of the displaced material through the opening 'between the incisions. This locks the pieces together.
Although the resulting fastener resists separation of the overlying pieces of material by a force exerted perpendicular to the plane of the material and by a force exerted in a plane parallel to the plane thereof but transversely of the fastener, it does not resist to so great an extent their separation by the application of a force exerted in the plane of the material but longitudinally of the fastener.
In other words, if a sufficiently great force is applied longitudinally of the fastener, the overlying displaced section may be slipped along the underlying displaced section, thereby separating the pieces. For example, if a force of 2000 pounds is required to separate the pieces when applied in a direction normal to the plane thereof, a force of about 1100 pounds may be sucient to separate them if it is applied in the plane of the pieces but longitudinally of the fastener.
Accordingly, it is the primary object of the present invention to provide an integral fastener for overlying pieces of material, which fastener has substantially increased resistance to force applied in a direction longitudinally of the fastener.
It is another object of the-present invention to provide an integral fastener for uniting overlying pieces of material which may be formed lwith minimum thinning 'of the material and which, as a result, is of increased strength.
Still another object of this invention is the provision of an integral fastener for uniting overlying pieces of material which is characterized by the presence of interlocking edges which lock the pieces together so that they are resistant to separation by a force applied from any direction.
Still another object of this invention is the provision of a method of forming an integral, interlocking fastener for uniting overlying pieces of material which method may be carried out rapidly and eiiiciently.
The manner in which the foregoing and other objects of this invention are accomplished will be apparent from the accompanying specitication and claims considered `together with the drawings, wherein:
Figure 1 is a view in end elevation of a punch and die which may be used for forming the presently described fastener; Y
Figure 2 is a view in side elevation of the punch and die of Figure 1;
Figure 3 is an end view of the die of Figures 1 and 2 as viewed from the line 3 3 of Figure 2;
Figure 4 is a plan view of the interlocked fastener which is produced by the operation of the punch and die of Figures l-3;
Figure 5 is a longitudinal sectional view of the fastener of Figure 4 taken along the line 5 5 of that ligure;
Figure 6 is a transverse sectional view of the fastener of Figure 4 taken along the line 6--6 of that ligure; and
Figures 7 and 8 are plan v1ews of alternate forms of fasteners which may be produced by the presently described method.
Broadiy stated, the presently described method for forming an integral fastener through overlying pieces of material comprises first forming laterally spaced apart, substantially aligned incisions through the pieces, the distance between selected opposite segments of the incisions being greater than that between other opposite segments thereof. For example, the incisions may be outwardly offset so that the distance between the central segments thereof will be greater than that between the terminal segments.
'l'he material between the incisions then is bent until the displaced portion of one of the pieces lies beyond the outer surface of the other of the pieces. The displaced portion next is spread laterally until it underlies the adjacent surface, thereby interlocking the pieces through a plurality of interengaging edge surfaces.
Considering the foregoing in greater detail and with particular reference to the drawings:
A punch and die assembly which may be employed in forming the presently described fastener is illustrated in Figures l-3. As is apparent, the assembly comprises a die member and a punch member. Plhe die member includes a body 10, one end of which is formed with a pair of spaced apart shoulders 12, 14. This end lof the die body also has a pair of spaced apart recesses 16, 18 lying p outside of the shoulders and a central longitudinal opening 20. An anvil 22 is connected to the body of the die,
as by being frictionally received in longitudinal opening 20 of the die body. 1t has a work surface 24 and a pair of opposite side faces 26, 28 formed with outwardly extending projecting portions 30, 32 respectively. The
latter may extend the full length of the anvil.
Positioned against side faces 26, 28 respectively of the anvil are cutting elements 34, 36. These are formed with recesses 38, 40 which are complementary to projections 30, 32 on the anvil. The inner ends of the cutters abut against shoulders 12, 14 of the die body. Their outer ends, on which are the cutter surfaces 42, 44, extend a spaced distance beyond the work surface 24 of the anvil, this distance being predetermined to accommodate the particular thickness of the material which is to be theV subject matter of the fastening operation.
Means are provided for maintaining cutters 34, 36 pressing resiliently against the side' `faces of the anvil and for releasably securing them tothe die body. A preferred means of accomplishing these functions comprises attaching the cutters to resilient tongues 46, 50. The latter preferably are formed integrally with the cutters, as by recessing the latter at 52, 54 and forming the material defined in part by the recesses into outwardly bowed tongues in Vthe manner indicated.
This in effect accomplishes attaching the tongues to the central portion o f the cutters, which in turn makes possible abutting the inner edges of the cutters against shoulders 12, 14 of the die body while contemporaneously providing arcuate spring members which may be in- Y serted into recesses 16, :18, therein.` These frictionally engage the side walls of the recessesand secure the cutters to the body of the die, while maintaining them `pressing yieldably against the side faces of the anvil.
The punch sectionV of the assembly which cooperates withv the die in forming fasteners through the, Aoverlying pieces of material includes a body portion 60 and a punch portion 62. The latteris formed with a working surface 64, angular forming sections 66, 68 and longitudinal projections 70, 72 along its opposite side faces. The configuration of the working surface of the punch thus conforms generally to that of the working surface of the anvil.
' Operation v The manner in which the above described punch and die cooperate in forming the novel fastener of the present invention will be apparent from a consideration of Figures 4 6.
First, overlying pieces of material, for example, sheets of aluminum 80, 82 are placed between the punch and die. The punchthen is advanced towards the die whereupon its forms a pair of laterally spaced apart, substantially aligned incisions completely through the overlying pieces of material. The pattern of these incisions is particularly apparent from Figure 4. Y
As will be seen from that figure, one pai-r of overlying incisions comprises the outer segment 84, 86 and a central,
outwardly offset segment 88. These segments are inter` connected by the angled connecting segments 90, 92, the angle preferably being about 45. The configuration of the companion pair of overlying incisions is similar. Accordingly, it is made up of vthe terminal segments V94, 96 and the outwardly offset, central segment 98, these being interconnected by the connecting segmentV 100, 102.
The pattern of the incisions may be varied however, by
using punches and dies of Vdifferent' configurations, provided a pattern is retained in` which the distance between selected opposite segments of the incisions is greater than that between other opposite segments thereof. Thus the pattern of the incisions may be as is illustrated in Figure 7. In this pattern one of the incisions is made up of terminal segments 104, 106 and a central segment 108, the companion incision being composed of terminal segments 110, 112I and the central segment 114. In this embodiment, the pairs 104, 110 and 106,` 112 of the terminal segments are angled slightly toward each other, while the central segmentsA 108, 114' are maintained substantially parallel.
Similarly the incisions may assume the `pattern o-f Figure 8. In this. configuration the central segments of the incisions are inwardly offset. Thus` one of the incisions comprises the terminal Vsegments 116, 118, the central. segment 120 and the connecting segments 122, 124` The other incision is4 complementary, being made up of the terminal segments 126, 128, the inwardly oiset itralsegment 130 and the Aconnecting segments 132, Referring again to the embodiment of Figures 4 6, contmuedadvancement of the punch causes displaQQmGIlt, f
. edges 90,92 and 100,102 resist separation of the pieces force.l -For example, if an integral 'fastener not having the presently described interlock will withstand a lateral force of 2000. pounds and a longitudinal force of about the material betweenA the spaced incisions until sections 140, 142 are completely displaced below the plane of the bottom surface of the underlying sheet 82. During this process the end sections of the material between the spaced incisions are stretched and deformed to conform to the configuration of theforming surfaces 66, 68 of r the punch.
lFurther advancement of the punch causes the swaging and lateral extrusion of `the displaced material against the anvil, the cutters 34,36 moving outwardly against the tension of resilient members 46, V50 attached thereto as required to accommodate the extruded material. As a result there are formed laterally extending edges 144,`
146 indicated in dotted outline in Figure 4, which fasten the sheets together.
As a result of the foregoing operation there is formed a fastener which is strong in alldirections because of the presence of the'interlocking edges ofthe incised and displaced material.. Thus edges 144,V `146 resist lateral separation ofthe pieces as well as separa-tion by a force exerted in the plane of the fastener, but normall to the longitudinal axis thereof. Also, the interlocked angular by a force exerted .in the plane of the `fastener but in a directionlongitudinally of the axis thereof.
Accordingly the fastener is of substantial strength irrespective of the directionof application of a disrupting 1100 pounds without breaking, a fastener ofthe presently described class which will withstand a lateral force of 2000 pounds will withstand a longitudinal force of about 1900 pounds. Hence the longitudinal strength of the vfastener has been increased by about 70% and its usefulness augmented accordingly'.
It is to be understood that .the form` of my invention, herewith shown and described, is -to be taken as a pre- `ferred example of the same, and that various changes in the shape, size and arrangement of parts may be resorted to, without departing from the spirit of my invention, or the scope of the subjoined claims. Thus although a particular form of mounting the cutters on the diehas been described herein, this may be modified in accordance with disclosures contained `in my various U.S; patents including U.S. 2,254,558 and 2,288,308-, these pertaining to methods for forming integral fasteners of the class described herein and to apparatus for. forming: the same.
Having now described my invention, I claim:
l. A fastener-for uniting overlying pieces of material which comprises integral portions of the pieces defined` ments, the distancebetween a pair of selected opposed segments of the incisions being greater than that between the other opposed segments, said portions being dis-` i placed so that the displacedfportion of one of the pieces lies beyond the plane of the outer surface of the other of` the pieces, the displacedportion of `said one of the pieces` being. spread laterally until its margins underlie thesaid other ofthe pieces, thereby securely interlocking the piecesandl preventing their separation.
2. A fastener for` uniting overlying pieces of material which comprises integral portions' of the pieces defined by a pair of laterally spaced apart, substantially aligned incisions through the pieces, each of the incisions comprising' an" intermediate segmentand terminal segments` connected 4"thereto, the terminal `"segments beingsubsta'ntially parallel to the intermediatey segment, the intermediate' segment of at leastonerof the incisions being offset `from the terminalfsegments, thereof, said portions being displaced sio'that the displaced portion of one of thapieces lies beyondthe plane of the outersurface of the other of the pieces, theV displaced portion of said one of the pieces being spread laterally until its margins underlie the said other of the pieces, thereby securely interlocking the pieces and preventing their separation.
3. A fastener for uniting overlying pieces of material which comprises integral portions of the peces dened by a pair of laterally spaced apart, substantially aligned incisions through the pieces, each of the incisions comprising an intermediate straight-line segment and terminal straight-line segments connected thereto, the terminal segments being substantially parallel to the intermediate segment, the intermediate segments of both of the incisions being outwardly offset from the terminal segments thereof, said portio-ns being displaced so that the displaced portion of one of the pieces lies beyond the plane of the outer surface of the other of the pieces, the displaced portion of said one of the pieces being spread laterally until its margins underlie the said other of the nieces, thereby securely interlocking the pieces and preventing their separation.
4. The method of uniting overlying pieces of material through an integral fastener which comprises forming a pair of laterally spaced apart substantially aligned incisions through the pieces with each of the incisions having an intermediate segment and terminal segments connected thereto in parallel relation, the intermed'ate segment of at least one of said incisions being oiset from the terminal segments thereof, deforming the material between the incisions outwardly until the displaced portion of one of the pieces lies beyond the outer surface of the other of the pieces, spreading the displaced portion of said one of the pieces until it underlies the outer surface of the other of the pieces, thereby securely interlocking the pieces and preventing their separation.
5. The method of uniting overlying pieces of material through an integral fastener which comprises forming a pair of laterally spaced apart substantially aligned incisions through the pieces with each of the incisions having an intermediate segment and terminal segments connected thereto in parallel relation, the intermediate segments of both of the incisions being outwardly oiset from the terminal segments thereof, deforming the material between the incisions outwardly until the displaced portion of one of the pieces lies beyond the outer surface of the other of the pieces, spreading the displaced portion of said one of the pieces until it underlies the outer surface of the other of the pieces, thereby securely interlocking the pieces and preventing their separation.
References Cited in the le of this patent UNITED STATES PATENTS 56,494 Gordon July 17, 1866 977,178 Ferguson Nov. 29, 1910 2,288,308 Williams June 30, 1942 2,426,670 Cooley Sept. 2, 1947
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Cited By (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3222779A (en) * 1963-02-28 1965-12-14 Kaiser Aluminium Chem Corp Stitching apparatus
US3900937A (en) * 1974-08-05 1975-08-26 Louis C Schleicher Spot clinch means and method
US3924378A (en) * 1973-08-01 1975-12-09 Otto P Hafner Interlocking joint for overlying sheet material
US4080768A (en) * 1976-04-21 1978-03-28 Consecco A.G. Connecting arrangement
US4264663A (en) * 1978-04-10 1981-04-28 Licentia Patent-Verwaltungs-G.M.B.H. Laminated pack comprising a plurality of closely superposed sheets and method and device for forming the pack
DE3106313A1 (en) * 1980-09-08 1982-04-22 BTM Corp., 48079 St. Clair, Mich. DEVICE AND METHOD FOR JOINING SHEETS
US4394794A (en) * 1981-01-19 1983-07-26 Donn Incorporated Metal fastening system and method
USRE31535E (en) 1974-08-05 1984-03-13 Spot clinch means and method
US4459735A (en) * 1980-09-08 1984-07-17 Btm Corporation Joining sheet metal
USRE31737E (en) * 1972-07-28 1984-11-20 Adjustable die and punch for sheet material fastening machines
US4521953A (en) * 1984-04-10 1985-06-11 General Electric Company Method of assembling a dynamoelectric machine
US4574453A (en) * 1982-04-30 1986-03-11 Btm Corporation Self-attaching fastener and method of securing same to sheet material
US4584753A (en) * 1984-03-22 1986-04-29 Eckold Gerd Juergen Apparatus for connecting sheet metal pieces
US4614017A (en) * 1981-10-28 1986-09-30 Walter Eckold Gmbh & Co. Kg Device for joining metal sheets by a rivetting-type method
US4658502A (en) * 1984-03-22 1987-04-21 Eckold Gerd Juergen Sheet metal joining apparatus
US4757609A (en) * 1980-09-08 1988-07-19 Btm Corporation Apparatus for joining sheet material
US4835850A (en) * 1986-11-29 1989-06-06 Eckold Gerd Juergen Apparatus for joining pieces of sheet metal
US4910853A (en) * 1980-09-08 1990-03-27 Btm Corporation Apparatus for joining sheet material
US5027503A (en) * 1980-09-08 1991-07-02 Btm Corporation Apparatus for joining sheet material
US5031442A (en) * 1985-06-03 1991-07-16 Btm Corporation Punch anvils for sheet fastening systems
US5131258A (en) * 1985-06-03 1992-07-21 Btm Corporation Punch anvils for sheet fastening systems
US5177861A (en) * 1980-09-08 1993-01-12 Btm Corporation Apparatus for joining sheet material
US5207086A (en) * 1985-06-03 1993-05-04 Btm Corporation Punch anvils for sheet fastening systems
US5208973A (en) * 1980-09-08 1993-05-11 Btm Corporation Apparatus for joining sheet material
US5208974A (en) * 1980-09-08 1993-05-11 Btm Corporation Apparatus for attaching a fastener to sheet material
US5509290A (en) * 1993-05-04 1996-04-23 Faivre; Jean-Claude Tools for cold flow forming of assembly points in sheet metal
US5528815A (en) * 1990-04-03 1996-06-25 Webb; Edward L. T. Clinching tool for sheet metal joining
US5577313A (en) * 1995-01-17 1996-11-26 Guido; Anthony Method and apparatus for joining deformable sheet stock
US5581860A (en) * 1980-09-08 1996-12-10 Btm Corporation Apparatus for joining sheet material
US5678946A (en) * 1994-08-05 1997-10-21 Enami Seiki Mfg. Co., Ltd. Joint structure for metal plates
EP0879658A4 (en) * 1995-11-20 1998-11-25
US5979055A (en) * 1993-01-08 1999-11-09 Worthington Armstrong Venture Process for producing rollformed sections
US5984563A (en) * 1994-07-22 1999-11-16 Btm Corporation Apparatus for joining sheet material and joint formed therein
US6430794B1 (en) 2000-05-17 2002-08-13 Mckee James E. Female crimping die and system for crimping metal sheets
US20090311551A1 (en) * 2006-08-22 2009-12-17 Japan Metal Gasket Co., Ltd. Connecting Structure of Metal Plates
US20100077687A1 (en) * 2008-09-26 2010-04-01 Jankovec Scott G Rotary stitch for joining sheet metal stock
US20100212131A1 (en) * 2009-02-23 2010-08-26 Btm Corporation Clinching tool
US20110076510A1 (en) * 2009-09-25 2011-03-31 Yazaki Corporation Metal joint body and apparatus for manufacturing the metal joint body
US20110318598A1 (en) * 2009-03-10 2011-12-29 Yazaki Corporation Joined metal member, metal joining method and metal joining apparatus
WO2012157501A1 (en) * 2011-05-18 2012-11-22 矢崎総業株式会社 Metal joint part
US9845599B2 (en) 2014-04-23 2017-12-19 Nucor Corporation Structural steel decking system and method of securing
US9863146B2 (en) 2015-05-14 2018-01-09 Nucor Corporation Structural panel systems with a nested sidelap and method of securing
US10328481B2 (en) 2014-03-18 2019-06-25 Btm Company Llc Clinching punch and apparatus
US10370851B2 (en) 2016-03-21 2019-08-06 Nucor Corporation Structural systems with improved sidelap and buckling spans

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Publication number Priority date Publication date Assignee Title
US56494A (en) * 1866-07-17 Improvement in machines for securing the ends of strips of sheet metal together
US977178A (en) * 1910-02-09 1910-11-29 Empire Novelty Company Metal-clenching machine.
US2288308A (en) * 1941-04-07 1942-06-30 Ivan A Williams Punch and die
US2426670A (en) * 1945-12-19 1947-09-02 David N Cooley Apparatus for connecting metallic strips

Cited By (58)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3222779A (en) * 1963-02-28 1965-12-14 Kaiser Aluminium Chem Corp Stitching apparatus
USRE31737E (en) * 1972-07-28 1984-11-20 Adjustable die and punch for sheet material fastening machines
US3924378A (en) * 1973-08-01 1975-12-09 Otto P Hafner Interlocking joint for overlying sheet material
USRE31535E (en) 1974-08-05 1984-03-13 Spot clinch means and method
US3900937A (en) * 1974-08-05 1975-08-26 Louis C Schleicher Spot clinch means and method
US4080768A (en) * 1976-04-21 1978-03-28 Consecco A.G. Connecting arrangement
US4264663A (en) * 1978-04-10 1981-04-28 Licentia Patent-Verwaltungs-G.M.B.H. Laminated pack comprising a plurality of closely superposed sheets and method and device for forming the pack
US4459735A (en) * 1980-09-08 1984-07-17 Btm Corporation Joining sheet metal
US4910853A (en) * 1980-09-08 1990-03-27 Btm Corporation Apparatus for joining sheet material
DE3106313A1 (en) * 1980-09-08 1982-04-22 BTM Corp., 48079 St. Clair, Mich. DEVICE AND METHOD FOR JOINING SHEETS
US5581860A (en) * 1980-09-08 1996-12-10 Btm Corporation Apparatus for joining sheet material
US5339509A (en) * 1980-09-08 1994-08-23 Btm Corporation Method for attachment of fastener to sheet material
US5208974A (en) * 1980-09-08 1993-05-11 Btm Corporation Apparatus for attaching a fastener to sheet material
US5208973A (en) * 1980-09-08 1993-05-11 Btm Corporation Apparatus for joining sheet material
US5177861A (en) * 1980-09-08 1993-01-12 Btm Corporation Apparatus for joining sheet material
US4757609A (en) * 1980-09-08 1988-07-19 Btm Corporation Apparatus for joining sheet material
US5027503A (en) * 1980-09-08 1991-07-02 Btm Corporation Apparatus for joining sheet material
US4394794A (en) * 1981-01-19 1983-07-26 Donn Incorporated Metal fastening system and method
US4614017A (en) * 1981-10-28 1986-09-30 Walter Eckold Gmbh & Co. Kg Device for joining metal sheets by a rivetting-type method
US4574453A (en) * 1982-04-30 1986-03-11 Btm Corporation Self-attaching fastener and method of securing same to sheet material
US4658502A (en) * 1984-03-22 1987-04-21 Eckold Gerd Juergen Sheet metal joining apparatus
US4584753A (en) * 1984-03-22 1986-04-29 Eckold Gerd Juergen Apparatus for connecting sheet metal pieces
US4521953A (en) * 1984-04-10 1985-06-11 General Electric Company Method of assembling a dynamoelectric machine
US5031442A (en) * 1985-06-03 1991-07-16 Btm Corporation Punch anvils for sheet fastening systems
US5131258A (en) * 1985-06-03 1992-07-21 Btm Corporation Punch anvils for sheet fastening systems
US5207086A (en) * 1985-06-03 1993-05-04 Btm Corporation Punch anvils for sheet fastening systems
US4835850A (en) * 1986-11-29 1989-06-06 Eckold Gerd Juergen Apparatus for joining pieces of sheet metal
US5528815A (en) * 1990-04-03 1996-06-25 Webb; Edward L. T. Clinching tool for sheet metal joining
US5979055A (en) * 1993-01-08 1999-11-09 Worthington Armstrong Venture Process for producing rollformed sections
US5509290A (en) * 1993-05-04 1996-04-23 Faivre; Jean-Claude Tools for cold flow forming of assembly points in sheet metal
US5984563A (en) * 1994-07-22 1999-11-16 Btm Corporation Apparatus for joining sheet material and joint formed therein
US5678946A (en) * 1994-08-05 1997-10-21 Enami Seiki Mfg. Co., Ltd. Joint structure for metal plates
US5577313A (en) * 1995-01-17 1996-11-26 Guido; Anthony Method and apparatus for joining deformable sheet stock
EP0879658A4 (en) * 1995-11-20 1998-11-25
EP0879658A1 (en) * 1995-11-20 1998-11-25 Japan Metal Gasket Co., Ltd. Method for connecting laminated metal plates and press mold
US6115905A (en) * 1995-11-20 2000-09-12 Japan Metal Gasket Co., Ltd. Method for connecting laminated metal plates and press mold
US6430794B1 (en) 2000-05-17 2002-08-13 Mckee James E. Female crimping die and system for crimping metal sheets
US20090311551A1 (en) * 2006-08-22 2009-12-17 Japan Metal Gasket Co., Ltd. Connecting Structure of Metal Plates
US8240678B2 (en) * 2006-08-22 2012-08-14 Japan Metal Gasket Co., Ltd. Connecting structure of metal plates
US20100077687A1 (en) * 2008-09-26 2010-04-01 Jankovec Scott G Rotary stitch for joining sheet metal stock
US7762034B2 (en) 2008-09-26 2010-07-27 Chicago Metallic Corporation Rotary stitch for joining sheet metal stock
US20100212131A1 (en) * 2009-02-23 2010-08-26 Btm Corporation Clinching tool
US8650730B2 (en) 2009-02-23 2014-02-18 Btm Corporation Clinching tool
US20110318598A1 (en) * 2009-03-10 2011-12-29 Yazaki Corporation Joined metal member, metal joining method and metal joining apparatus
US20110076510A1 (en) * 2009-09-25 2011-03-31 Yazaki Corporation Metal joint body and apparatus for manufacturing the metal joint body
US10343207B2 (en) 2009-09-25 2019-07-09 Yazaki Corporation Metal joint body and apparatus for manufacturing the metal joint body
WO2012157501A1 (en) * 2011-05-18 2012-11-22 矢崎総業株式会社 Metal joint part
JP2012240079A (en) * 2011-05-18 2012-12-10 Yazaki Corp Metal joint part
CN103582533A (en) * 2011-05-18 2014-02-12 矢崎总业株式会社 Metal joint part
CN103582533B (en) * 2011-05-18 2016-03-23 矢崎总业株式会社 Metal bonded body
US9327336B2 (en) 2011-05-18 2016-05-03 Yazaki Corporation Metal joint
US10328481B2 (en) 2014-03-18 2019-06-25 Btm Company Llc Clinching punch and apparatus
US9845599B2 (en) 2014-04-23 2017-12-19 Nucor Corporation Structural steel decking system and method of securing
US10465384B2 (en) 2014-04-23 2019-11-05 Nucor Corporation Structural decking system
US10316519B2 (en) 2015-05-14 2019-06-11 Nucor Corporation Structural panel systems with a nested sidelap and method of securing
US9863146B2 (en) 2015-05-14 2018-01-09 Nucor Corporation Structural panel systems with a nested sidelap and method of securing
US10370851B2 (en) 2016-03-21 2019-08-06 Nucor Corporation Structural systems with improved sidelap and buckling spans
US10808403B2 (en) 2016-03-21 2020-10-20 Nucor Corporation Structural systems with improved sidelap and buckling spans

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