RIVETING DEVICE FOR METAL SHEETS

Abstract

The invention provides a device that joins together several metal sheets in a single step. The device features a mechanism which simultaneously punctures a plurality of substrates and folds back extrusions produced when the substrates are punctured. The mechanism automatically retracts from the metal sheets once the folding of the extrusions occurs.

Description

BACKGROUND OF THE INVENTION

1. Field of the Invention

This invention relates to the field of devices for joining metal objects and, more particularly, to a device used in riveting together studs and thin sheets of metal.

2. Background of the Invention

Devices for attaching or riveting together studs and thin sheets of metal have been available. However, they suffer from several disadvantages. To begin with, their use requires that the operation be carried out in three steps: first the studs or sheets of metal must be perforated at the junction point; second a rivet or the like must be inserted through the perforation; and third the rivet must be compressed or, at the very least, the extrusions or hanging chads resulting from the perforation of the metal sheets must be hammered down.

Quite often, another device serving as an anvil must be placed on the side opposite to that where the perforating device engages the work pieces. If the workpiece is large and therefore unwieldy, positioning of the workpiece on an anvil or other support structure may require several workers.

A need exists in the art for a device that rivets a plurality of plates in one single step without recourse to a support structure such as an anvil. The device should be modular such that it is easily carried. Also, the device should be comprised of common materials so as to minimize cost.

SUMMARY OF THE INVENTION

An object of this invention is to provide a metal-plate riveting device that overcomes many of the disadvantages in the prior art.

Another object of the invention is to provide a labor-saving metal-plate riveting device that rivets a plurality of plates. A feature of this invention is a combination of a puncturing device with a means to automatically fold back extrusions, burrs and hanging chads produced as the plates are punctured. An advantage of this invention is that it provides a riveting device that rivets a plurality of substrates such as plates in one single step.

Yet another object of the invention is to provide a riveting device that enables the joining of multiple substrates through folded extrusions and the insertion of a plurality of rivets into the substrates without recourse to any backstop or support structure or other device positioned on the back side of the substrate (i.e., the side opposite to the side initially contacted by the invented device). A feature of this invention is that it comprises a combination of a puncturing device and a means to fold substrate-extrusions, chards or hanging chads (which are produced when the plates are punctured) to the back side of the plates. This folding means engages the substrate on the same side as does the puncturing device. An advantage of this invention is that it provides a riveting device that is capable of being operated from solely one side of the substrates to be riveted such that no substrate support or backstop is required during use.

Another object of the invention is to facilitate permanent attachment of a plurality of metal substrates at points away from the edge of the substrates. A feature of the invention is that the puncturing device may fasten the substrates at any location on the surface of the substrates. A benefit of the invention is that it may join substrates at any accessible location, especially with access to only one surface, and not merely the edge of the substrates.

In brief, in one embodiment, this invention provides a device for fastening together a plurality of substrates having a front side and a back side in one step by combining a puncturing mechanism means with a means to fold back extrusions produced when the plates are punctured wherein said puncturing mechanism and said folding back means operate from only one side of each of said substrates. In another embodiment, this invention provides a method for fastening a plurality of substrates in a single step said method comprising combining a puncturing mechanism with a means for folding back extrusions produced when said substrates are punctured.

BRIEF DESCRIPTION OF THE DRAWING

The foregoing and other objects, aspects, and advantages of this invention will be better understood from the following detailed description of the preferred embodiments of the invention with reference to the drawing, in which:

FIG. 1 is an overall cross-sectional view of an exemplary embodiment of a device for perforating and riveting metal plates, in accordance with features of the present invention;

FIG. 2 is a perspective view of a piston component of an embodiment of a device for perforating and riveting metal plates depicted in FIG. 1, in accordance with features of the present invention;

FIG. 3 a is a perspective view of a riveting component of an embodiment of a device for perforating and riveting metal plates depicted in FIG. 1, in accordance with features of the present invention;

FIG. 3 b is a perspective view of a plate in the rivet component of an embodiment of a device for perforating and riveting metal plates depicted in FIG. 1, in accordance with features of the present invention;

FIG. 3 c is a plan view of a base for a rivet component of an embodiment of a device for perforating and riveting metal plates depicted in FIG. 1, in accordance with features of the present invention;

FIG. 4 a is a profile view of a hammer component of an embodiment of a device for perforating and riveting metal plates depicted in FIG. 1, in accordance with features of the present invention;

FIG. 4 b is an elevation view of a hammer component of an embodiment of a device for perforating and riveting metal plates depicted in FIG. 1 in accordance with features of the present invention;

FIG. 4 c is a view of FIG. 1 taken along line 4c-4c, in accordance with features of the present invention

FIG. 4 d is a detailed view of a hinge arrangement for an embodiment of the invented device depicted in FIG. 1, in accordance with features of the present invention

FIG. 5 a is an overall cross-sectional view of the invented device during perforation of a plurality of substrates, in accordance with features of the present invention;

FIG. 5 b is an overall cross-sectional view the invented device in post-perforation stage, in accordance with features of the present invention;

FIGS. 6 a through 6c are schematic views of stages in the operation of the invented device, in accordance with features of the present invention;

FIG. 7 a is a perspective view of an alternate embodiment of the invented device, in accordance with features of the present invention;

FIG. 7 b is a perspective view of a piston component of the device depicted in FIG. 7a, in accordance with features of the present invention;

FIG. 7 c is a perspective view of a rivet component of the device depicted in FIG. 7a, in accordance with features of the present invention;

FIG. 7 d is a cross-sectional view of FIG. 7a, taken along lines 7-7;

FIG. 7 e is a perspective view of a deployed configuration of the device depicted in FIG. 7a, in accordance with features of the present invention;

FIG. 8 a is a perspective view of another embodiment of the invented device, in accordance with features of the present invention;

FIG. 8 b is a perspective view of a piston component of the device depicted in FIG. 8a, in accordance with features of the present invention;

FIG. 8 c is an exploded view of a riveting component and a piston component for the device depicted in FIG. 8a, in accordance with features of the present invention;

FIG. 8 d is a cross-sectional view of FIG. 8c taken along lines 8-8; and

FIG. 9 is a perspective view of another embodiment of the cap of the invented device.

DETAILED DESCRIPTION OF THE INVENTION

The present invention provides a labor-saving metal plate riveting device that rivets a plurality of plates in one single step. It combines a puncturing device with a means for folding back extrusions produced when the plates are first punctured.

The present invention discloses a method and a device such that given an unsupported side of a stack comprising a plurality of substrates coplanarly arranged, the user can, by applying the invented tool to the other side of the configuration, perforate the entire configuration transversely and rivet the substrates together in a single step.

The present invention is a substrate-piercing device comprising a piercing mechanism and a riveting mechanism. Initially, upon positioning of the device upon a plurality of substrates to be fastened together, a charge deploys a piston outwardly toward the substrate. Suitable charges are those originating from coiled spring, voltage potential, compressed air, fluid or a chemical charge such as propane or gunpowder.

Upon deployment, the piston simultaneously transversely pierces the substrates while causing the rivet mechanism to laterally bend the shards defining the resulting aperture upon the back of the last substrate. For example, when air pressure deploys the piston toward a first surface of a stack of plates, a polygonal aperture is formed transversely through the stack, whereby the tip of the rivet mechanism acts as a punch. Said polygonal aperture is bounded by triangular extrusions or shards extending through the aperture and toward the rear of the stack of plates. Simultaneous with the tip of the riveting mechanism forming the aperture, mid portions of the riveting mechanism defining hammer heads laterally force the shards against the back surface of the stack so that the shards establish intimate irreversible contact with the back surface of the stack. This deployment is achieved when the piston, coaxially arranged with a sleeve defining the rivet mechanism is thrust in the sleeve so as to cause the hammer heads to deploy laterally. The hammer heads are defined by longitudinally extending portions of the sleeve which are separated from each other by longitudinally extending slits.

Structure of the One Embodiment of the Device

FIG. 1 shows a cross-sectional view of the invented device 10 removably received by a means for actuating the device in an axial direction. The aforementioned actuating means includes, but is not limited to, pressurized air, chemical charge, mechanical actuation, such as spring loading, and a combination thereof.

The device defines a first or distal end 16 and a second or proximal end 18 when it is enclosed in a housing 11. The device 10 comprises a piston portion 25 coaxially aligned with a riveting tool portion 40. This coaxial arrangement is spring biased toward the proximal end 18 of the device by one or a plurality of springs 20 and 30. The proximal end 18 of the housing 11 snaps on or is otherwise removably received by said actuation device or is fully integrated into another device.

At this juncture, it should be noted that the device 10 can be seamlessly integrated into existing nail guns, such as those pneumatically actuated or electrically actuated. The housing 11 of the invented device in such instances is defined by the nailing end of such guns. For example, the nailing end of pneumatically-or electrically-actuated guns typically encircle a piston within the gun, that piston charged by air, a voltage potential, or coiled spring.

A proximal facing surface 36 of the piston is adapted to contact the effect of the actuating means, such as a bolus of fluid from a pressurized line or chemical charge, or mechanical contact with a rapidly expanding spring,

For example, FIG. 1 depicts a piston spring 30 positioned between the base of the piston 25 and the base of the riveting tool 40. Specifically, the pertinent portion of the base of the piston defines a distally facing surface 27 while the pertinent portion of the base of the riveting tool defines a proximally facing surface 28. These surfaces, when placed in opposition to each other, form a chamber 33 in which the piston spring 30 resides.

A second spring 20, dubbed herein as a rivet spring, is positioned between a distally facing surface 38 of the rivet portion and medially extending surface of the generally perpendicular to the longitudinal axis a of the device. In an embodiment of the device, the medially extending surface is defined by a proximally-facing surface 14 of a threaded collar 17 which is adapted to be threadably received by the distal most end of the housing 11. This collar provides a means for axial adjustment of the device to vary the protrusion of the riveting mechanism from the distal end of the device. In one embodiment, this inside surface defines a circumferentially arranged, medially extending ring surface 12.

In operation of one embodiment of the device, pressurized air (e.g. 50-150 psig) impacts the resting position of the proximal facing surface 36 of the piston to propel the piston in a distally extending direction. A circumferentially extending groove 19 along a proximal periphery of the piston 25 is adapted to receive an o-ring gasket 21 so as to provide a means for hermetically sealing the proximal end of the barrel to the proximal end of the piston while maintaining slidable communication between the piston and the barrel, similar to the configuration of a piston in a cylinder of an engine. At the opposite (i.e., distal) end of the device, the stop 12 limits motion of the riveting tool 40 by contacting distal surface 38. A threaded surface 24 of the distal end 16 of the housing is adapted to receive the complementary threaded spacer 17 so that one may adjust the distance the tip 39 of the rivet portion 40 protrudes from the first end 16 of the housing 11 after compressed air is applied by varying the length of the spacer 17. This spacer 17 may also communicate with the housing 11 in a snap fit arrangement or some other reversible attachment means.

FIG. 2 is a perspective view of an exemplary embodiment of the piston portion 25 depicted in FIG. 1. Preferably, this piston section 25 is manufactured from a single piece of high impact resistant material such as SAE Grade S Tool steel. The piston portion 25 comprises a cylindrical shaft 29 emanating from a base 32. The shaft 29 defines a longitudinally extending portion 29s having a polygonal cross-section bounded by planes 23. A distal portion 29c defines a circular cross-section. The shaft terminates in a tip 26, which is depicted as a hemisphere in FIG. 2. However, the tip can also be frusto-conical as depicted in FIG. 1. A hemispherical tip 26 reduces frictional wear on the piston. (See Operation of the Device infra).

While in general the cross-section of the portion 29s can be an arbitrary polygon, for illustration purposes, in the remainder of this description this cross-section will be taken to be a square and in some embodiments (such as the one depicted in FIG. 2) this square cross-section excludes sharp corners. A medially facing surface of the base 32 defines a channel 31 circumscribing the shaft 29 and adapted to receive the piston spring 30 and a peripheral wall 34 comprising the o-ring groove 19. As noted supra, the floor of the channel (i.e., the distal facing surface 27 of the piston portion) is adapted to support the piston spring 30.

FIG. 3 a is a perspective view of an exemplary embodiment of the riveting portion. The riveting portion comprises a base 57 and four hammers 59 emanating from the base 57 and attached to the base 57 as described infra. The base 57 comprises a top plate 82 and a bottom plate 84, with the top plate 82 secured to the bottom plate 84 by fastening means 83 such as screws. FIGS. 4a and 4b provide profile and face views of a hammer 59. Each hammer 59 comprises a cam surface 45 at its proximal end, a hammer head 53 at its distal end, and a generally elongate flat substrate or panel 47 positioned intermediate, and integrally formed with, the cam surface and the hammer head. A plurality of hammers are symmetrically arranged about the longitudinal axis a of the device to form a sleeve 49 defining a longitudinally extending interior surface. This surface is adapted to slidably receive the portion 29s of the piston. (See FIG. 1).

Each panel terminates in a hammer head 53 such that when four hammer heads 53 are symmetrically arranged about the longitudinal axis, the resulting configuration resembles a pyramid 48. Each hammer head has an interior face 51 so that the four hammer heads 53 form within the pyramid 48 an interior cavity 46 configured to receive the piston tip 26.

Each pyramid face comprises a base edge 50, two slanted edges 71, and a mid-face section 77. As shown in FIG. 4a, the base-edge 50 is rounded. (See Operation of the Device infra concerning this feature.) To facilitate use of the device to perforate metal plates, the pyramid faces are concave with edges 71 protruding from the face and the mid-face section 77 being recessed, as is shown in FIG. 4c which is a cross-sectional view of FIG. 1 along the line 4c-4c.

FIG. 4 d depicts a hinge arrangement for a hammer 59 (shown in FIG. 3a). The cam surface 45 and the panel leg 54 are positioned between the shaft 29s and a peripheral region 81 of the top plate 82 of the piston portion. An L-shaped substrate or rubber elbow 89 is positioned intermediate the cam surface and the top plate region 81, with a horizontally disposed region 98 of the elbow further positioned in an annular channel formed by a depending surface of the top plate 82 which is overhanging an upwardly facing surface of the bottom plate 84 of the piston base. The cam surface 45 is supported by a peripheral portion 92 of the bottom plate 84 not overhung by the top plate 82. The rubber elbow 89 consists of reversibly deformable material. The elbow 89 further comprises a vertically disposed section 99 that is sandwiched between the top plate region 81 and the hammer leg 54 and cam surface 45. The horizontally disposed section 98 (which is perpendicular the vertical section 99) is frictionally held or sandwiched between the plate 82 and the surface 92 by means of one or more fasteners 83. A torque T applied to the hammer 59 results in a swing in the direction T by the hammer but the laterally biasing force provided by rubber elbow 89 forces the hammer 59 to return to its original substantially vertical position once the torque T terminates.

FIG. 3 b is a perspective view of the top plate 82 of the base 57 (appearing in FIG. 3a) while FIG. 3c is a face view of the bottom plate 84 of the base 57. The top plate 82 defines a centrally disposed bore 87 having an x-shaped cross section. The center of the cross section defines a square bore 85 adapted to slidably communicate the piston shaft 29s (See FIG. 3c). As depicted in FIG. 3c, rectangular bores 88 are contiguous to the square bores 85. Each rectangular bore 88 is designed to accommodate the vertically disposed section 99 of the rubber elbow 89 and the hammer leg 54 depicted in FIG. 4d. Also, the plate 82 defines clearance countersunk bores 97 dimensioned to receive the fasteners 83.

The bottom plate 84 defines a square through bore 85 to allow slidable communication with the piston shaft 29s. The bottom plate also defines four shallow rectangular cavities 86 bordering the bore 85, each of said bordering cavities designed to accommodate a cam surface 45. The cavities 86 are contiguous to cavities 88 of the same depth, each designed to accommodate the horizontally disposed section 98 of a rubber elbow 89. Also the plate 84 comprises threaded bores 91 dimensioned to receive the fasteners 83. FIGS. 5a and 5b depict the base 57 assembled with the rubber elbows and the cam surface.

Operation Details

The device is intended for piercing simultaneously one or more sheets of metal or other suitable material, folding back extrusions produced when the sheets are pierced, and pressing back the extrusions on the back side of the last sheet being riveted. With two or more sheets so acted upon, the sheets are crimped to each other so that they cannot be separated nor rotated with respect to the other.

As shown in FIG. 1 the device is operated with an air gun. Alternatively, one may use a device where an air-fuel mixture is ignited by an ignition source. Such a device provides much higher pressure than standard compressed air devices. A spring gun or a rod and lever are also suitable. For the sake of specificity, an air gun is assumed in the remainder of this description.

When pressure is applied between the piston base 32 and the proximal end 18 of the housing 11, the piston is propelled forward, i.e., towards the distal or first end 16 of the barrel. This forward piston motion actuates the axial and lateral movement of the hammerheads of the rivet portion. The axial movement of the rivet portion terminates when the spring 20 is fully compressed and distal facing surface 38 contacts stop 12. Simultaneously, the rivet tool pyramid 48 pierces the sheets of metal 41, 42, forming roughly triangular extrusions 43 or chads. (See FIG. 5a)

The axial-extending length of the spacer 17 is chosen so that the edge 50 of the hammer head comes to rest at a medial position 44 in the extrusions 43. At this point the tapered tip 26 of the piston is instantaneously at rest with respect to the mating cavity 46 in the riveting portion and the piston spring 20 is fully compressed while the rivet spring 30 is at or near equilibrium. Yet at this point the region 13 in the gun barrel is still pressurized and this pressure acting on the base 32 is transmitted to the section 26 of the piston which in turn acts on the cavity 46.

Stop 12 prevents the over-extension of the rivet portion 40. The rivet portion 40 is not stopped by a substrate external to the device nor is the operation of the device dependent on any of the puncture elements resting against or impacting an external substrate. When the forward motion of the rivet portion 40 is stopped by the stop 12, the pressure in the housing 11 urges the piston assembly further forward. This forces the tip section 26 of the piston to force its way into the cavity 46 in the pyramid 48 in the rivet portion. (See FIG. 5b). This action imparts a lateral force to interior surfaces of the four hammer head sections 53 and the sleeve panels 47, thereby leading to their separation (akin to the opening of flower petals) so as to form a four-pronged hydra. The hammer heads 53 of the pyramid sections in turn apply a lateral force on the extrusions 43 and in a direction that is approximately perpendicular from the longitudinal axis of the piston. This action causes the hammer heads to thereby slide laterally across proximal ends of the extrusions, thereby folding the extrusions back against the surface of the last sheet of metal in the stack. (Note that the sliding of the hammer heads 53 on the extrusions 43 is facilitated by the fact that the edge 50 of the hammer heads 53 is rounded.) At this point air pressure is lost from the housing 11 through exhaust slots 35 (See FIG. 5b) in the cylinder or via an external bypass valve. This allows the piston spring 30 to exert a force backward (i.e. towards the end 18 of the housing). This causes the four hammer heads 53 to retract towards the axis. Then the springs bring back the rivet/piston combination to the position depicted in FIG. 1.

Experimentation by the inventor has determined that a hemispherical shape for the piston tip 26 minimizes frictional wear on that tip. With a hemispherical tip 26, as the tip 26 advances in the rivet cavity 46 different regions 26a, 26b, 26c of the tip 26 (See FIG. 2) come into contact with the inner face 51 of the hammer head 53 so that different regions of both the tip 26 and the hammer heads 53 experience wear in a single stroke. (See FIGS. 6a, 6b, 6c)

Alternative Embodiments

Alternative embodiments may differ in several respects from the preceding embodiment.

FIG. 7 a depicts an alternate exemplary embodiment 110 comprising a piston portion 125 and a rivet portion 140. The piston portion 125, which is manufactured from a single piece of high impact resistant material such as steel, is depicted in FIG. 7b. The piston portion 125 comprises a shaft 129 emanating from a base 132. The shaft 129 comprises a section 129s with a polygonal cross-section and a proximal section 129c with a circular cross-section, the latter terminating in a frusto-conical section 128 followed by a narrower shaft 127 which in turn terminates in a cone tip 126. (A circle 133 defines the transition between the shaft 127 and the cone 126). The base 132 comprises a channel 131 circumscribing the shaft 129 and adapted to receive a piston spring 30 and a peripheral wall 134 comprising an o-ring groove 119. The shaft portion 129s with a polygonal cross-section is bounded by planes 123 and the tip 126 is a pyramid 126s the faces of which are aligned with the planes 123. While in general the cross-section of the portion 129s can be an arbitrary polygon, in the remainder of this description this cross-section will be taken to be a square.

FIG. 7 c is a perspective view of an exemplary embodiment of the rivet portion 140 which is intended for use with the square cross-section piston portion 125 depicted in FIG. 7b. The rivet portion 140 is manufactured from a single piece of high impact reversibly deformable material such as tool steel. The rivet portion 140 comprises four sections separated by slits 162. Each section comprises a panel 161 and a head 153, such that the four sections form a hollow cylindrical shaft constituting a sleeve 149 emanating from the base 157 with the sleeve terminating in a pyramid 148. The rectangular panels 161 originate from the base 157 at regions 158 at the base of each panel. The panel regions 158 are very thin and since they are composed of reversibly deformable material they serve as reversible hinges. The slits 162 extend the entire length of the rivet section above its base and into the pyramid 148, to allow for separation of the four heads 153 upon actuation of the piston which is received by internal surfaces of the rivet portion.

FIG. 7 d shows a cross-section of the device 110 taken along the line 7-7 in FIG. 7a. The rivet portion comprises a longitudinally extending bore 151 adapted to slidably receive the shaft 129 of the piston. As such, the bore and the shaft have similar cross sections, with the shaft dimensioned slightly smaller to facilitate substantially frictionless sliding within the bore.

The pyramid section comprises a conical bore 146 adapted to slidably receive the conical section 128 and a cylindrical bore 156 adapted to slidably receive the shaft 127. The pyramid 148 terminates in an aperture with rim 154 through which can protrude the shaft 127 terminating in the cone 126. Each pyramid face comprises a base edge 150 defining a radius, two slanted edges 171, and a mid-face section 177. To facilitate penetration of the metal plates 41, 42 by the device, the pyramid faces are concave with edges 171 protruding from the face and the mid-face section 177 being recessed or depressed (See FIG. 4c for an identical construction).

In this embodiment, springs identical to the springs 20 and 30 depicted in FIG. 1 are utilized. In the equilibrium situation, i.e. before the device is propelled forward, the rim 154 coincides with the circle 133.

The piston depicted in FIG. 2 could also be used in this embodiment, in which case there is no aperture at the tip of the pyramid.

The operation of this device is identical to that of the embodiment depicted in FIG. 1. FIG. 7e is a perspective view of the embodiment 110 when the heads 153 are deployed as the piston 129 is thrust into the pyramid 146,

FIGS. 8 a, 8b, and 8c describe yet another embodiment of the present invention. FIG. 8a is a perspective view of the device 200 and FIG. 8b is a perspective view of the piston section. This embodiment features a circular cross-section cylindrical piston 230 that comprises a base 231 from which emanates a cylinder 233 that terminates in a first frusto-conical section 234. Superior to and integrally molded with the first frusto-conical section 234 is a cylindrical section 235 that terminates in a second frusto-conical section 236. Superior to and integrally molded with this second frusto-conical section is a cylindrical section 237 that terminates in a conical tip 238. The first and second frusto-conical sections 234 and 236 have the same inclination angle and the same height. This piston 230 is intended for use with a rivet portion 210 that comprises four separate sections 211, 212, 213, and 214 that are juxtaposed to each other and held together by o-rings or split rings 215, 216 received in grooves 225, 226.

FIG. 8 c is an exploded profile view of the rivet portion 210 positioned superior to the piston portion 230. Each rivet section 211, 212, 213, and 214 comprises a base portion 241, a sleeve portion 242 that is one quarter of a circular cross-section cylindrical sleeve and a pyramid portion 243. FIG. 8d is a cross-sectional view taken along line 8d-8d of FIG. 8c of the rivet portion 210 and of the piston portion 230. When the rivet portions are held together by the o-rings 215 and 216, they define frusto-conical cavities 254, 256 dimensioned to receive piston conical sections 236 and 234.

The operation of this piston/rivet combination differs from the previous two embodiments in that when the piston 230 is thrust into the four-component rivet portion 210, with the piston conical sections thrust into the cavities 254, 256 the four sections 211, 212, 213, and 214 are forced to displace laterally, perpendicular to the axis y of the piston, with no rotational movement of the rivet sections at all.

FIG. 9 is a depiction of an alternative embodiment of the invention comprising a cap 300 attached to the first or distal end 16 of the device 10 as shown in FIG. 1. In the alternative embodiment shown in FIG. 9, the cap 300 includes an integral electromagnet 310. The electromagnet is connected to power leads 315 which can energize the electromagnet 310. When the electromagnet 310 is energized, the cap 300 will be magnetically attracted to the metallic substrate undergoing fastening. The energized electromagnet 310 will assist to maintain the tool in place and removably engaged with the substrate, especially in instances where a high amount of lateral pressure is needed to puncture a heavy substrate. In one embodiment, the power leads 315 are connected to a direct current voltage source comprising a battery. In another embodiment, the power leads 315 are connected to an alternating current source, such as household current, wherein the alternating current source is adapted to function with the electromagnet 315.

While the invention has been described in the foregoing with reference to details of the illustrated embodiments, these details are not intended to limit the scope of the invention as defined in the appended claims.

Claims

1. A device for fastening together a plurality of substrates having a front side and a back side in one step by combining a puncturing mechanism means with a means to fold back extrusions produced when the plates are punctured wherein said puncturing mechanism and said folding back means operate from only one side of each of said substrates.

2. The device as recited in claim 1 wherein the device forms a rectilinear aperture in each substrate.

3. The device as recited in claim 2 wherein said puncturing mechanism and said folding back means are contained in a housing that is removably attached to an actuation means.

4. The device as recited in claim 3 wherein said extrusions are folded away from the aperture so as to fasten the substrates.

5. The device as recited in claim 1 comprising; a riveting mechanism to fold back extrusions, said riveting mechanism comprising a plurality of separable sections forming a cavity; anda piston member comprising a shaft dimensioned to be received in said cavity.

6. The device as recited in claim 1 wherein said puncturing mechanism means further comprises a plurality of springs.

7. The device as recited in claim 1 wherein said puncturing mechanism means further comprises a spacer for adjusting an amount of extension of the puncturing means.

8. The device as recited in claim 5 wherein said riveting mechanism further comprises four hammers emanating from a base wherein said hammers are symmetrically arranged about a longitudinal axis of said device.

9. The device as recited in claim 8 wherein said four hammers form a pyramid shape having an interior surface and an exterior surface, and wherein said interior surface contacts a tip of said piston member.

10. The device as recited in claim 9 wherein said four hammers further comprise a hinge activated by said piston member.

11. The device as recited in claim 9 wherein said hinge further comprises a rubber elbow wherein said elbow returns the hinge to a pre-activation configuration

12. The device as recited in claim 5 wherein penetration of the piston member into the riveting mechanism cavity causes deployment of the riveting sections with said sections impacting said extrusions.

13. The device as recited in claim 12 wherein said cavity has a frusto-conical shape.

14. The device as recited in claim 12 further comprising springs causing retraction of the riveting mechanism and of the piston from said substrates once said folding has been effected.

15. The device as recited in claim 14 wherein said piston member further comprises a base having a channel adapted to receive at least one of said springs.

16. A method for fastening a plurality of substrates in a single step said method comprising combining a puncturing mechanism with a means for folding back extrusions produced when said substrates are punctured.

17. The method recited in claim 16 further comprising ensuring that said puncturing mechanism forms rectilinear apertures.

18. The method recited in claim 16 further comprising placing said puncturing mechanism and said folding means in a housing and adapting said housing to be removably attachable to an activation means.

19. The method recited in claim 16 further comprising ensuring that said folding means comprises separable sections that form a cavity and that said folding is initiated by thrusting a piston into said cavity and thus separating said sections so that said sections impact said extrusions.

20. The method recited in claim 19 further comprising employing springs to cause retraction of the riveting mechanism and of the piston from said substrates once said folding has been effected.