US2348877A - Rivet cutter - Google Patents
Rivet cutter Download PDFInfo
- Publication number
- US2348877A US2348877A US49966843A US2348877A US 2348877 A US2348877 A US 2348877A US 49966843 A US49966843 A US 49966843A US 2348877 A US2348877 A US 2348877A
- Authority
- US
- United States
- Prior art keywords
- rivet
- holes
- plate
- cutting
- openings
- 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.)
- Expired - Lifetime
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23D—PLANING; SLOTTING; SHEARING; BROACHING; SAWING; FILING; SCRAPING; LIKE OPERATIONS FOR WORKING METAL BY REMOVING MATERIAL, NOT OTHERWISE PROVIDED FOR
- B23D29/00—Hand-held metal-shearing or metal-cutting devices
- B23D29/02—Hand-operated metal-shearing devices
- B23D29/023—Hand-operated metal-shearing devices for cutting wires
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T83/00—Cutting
- Y10T83/404—By means to misalign aligned apertured tools
- Y10T83/416—Rotary relative movement solely about a single pivot
- Y10T83/42—With plural apertures in one or both carriers
Definitions
- My invention relates to a rivet cutter particularly adapted for cutting rivets, bolts, screws etc. employed for riveting 0r fastening aircraft and other sheet metal.
- the present invention constitutes an improvef ment over my Patent No. 2,288,385, dated June 30, 1942.
- a stepped top shearing plate is superimposed upon and pivoted to a base shearing plate, both plates being formed with transverse rows of rivet holes, the holes of each row being graduated in size and the holes of the top plate being similar inrsize to and registering with the corresponding holes of the bottom plate when the plates are longitudinally aligned.
- This construction proved objectionable due to the fact that the rivet holes of one plate must be in complete register with the corresponding holes of the companion plate, thus necessitating perfect centering of plates.
- the shearing action due to the tight fit of the rivets in the top and bottom registering holes of the two plates, is not suiciently smooth to meet certain manufacturing requirements.
- the necessity for duplicating in the base plate the large number of rivet holes required in the top plate material ly increased the cost ⁇ of manufacture.
- the objects of the present invention are to obviate the ⁇ foregoing objections. This is accomplished by providing the bottom or base plate with two longitudinal rows of staggered openings, of considerably greater size than the corresponding rivet holes of the top.plateand two or more of the rivet holes of the latter plate being adapted to be conveniently moved into operative registering relation with a corresponding hole in the bottom plate, thus reducing the number of holes required in the bottom plate, eliminating the necessity of accurately centering the plates one with respect to the other and insuring a free and smooth shearing cut.
- Figure 1 is a plan View of the rivet cutter in rivet receiving position, and showing, in dotted lines, the position it assumes after performing the rivet cutting operation
- Figure 2 is a bottom plan view of the rivet cutter showing the top and bottom cutting plates in substantial alinement;
- Figure 3 is a longitudinal sectional view of the rivet cutter.
- Figure 4 is a section on the line 4-4 of Figure 1 showing a rivet in place and before being cut;
- Figure 5 is a side view of a rivet after being severed by the rivet cutter.
- numeral I designates a relatively at, substantially rectangular base cutting plate having the openings 2 for the reception of screws 3 to enable the plate to be removably secured to a flat work bench 4, or other suitable surface. If desired, the plate i may also be clamped in a bench vise and the like of airplane field service trucks, in an obvious manner not shown.
- the plate I is provided with two substantially longitudinally extending .rows of rivet holes 5, there being preferably four spaced holes in one row, and five spaced holes in the other and the holes of one row being irregularly staggered with respect to the holes of the other row.
- the holes 5 are preferably of equal size and are relatively large, that is, much larger than would be necessary to snugly accommodate a standard aircraft rivet of maximum size.
- the holes extend from the flat top face I of the plate I downwardly therethrough and terminate in a substantially U-shaped, groove 8, in the underside of the plate, which provides clearance for the lower ends of the rivets and permits of the severed ends thereof dropping onto the working surface 4.
- the bottom face I2 of the plate II is relatively flat and slidably engages with the flat top face I'of the base plate and is adapted to be pivotally moved or rotated thereover either in a counterclockwise or clockwise direction, viewing Figure l,v by means of a suitable rod or handle I3, mounted in a recess I4 in one end of the plate Il.
- the top face of the cutter plate II is provided with a series of preferably seven, substantially fiat steps or offsets I5 ranging in depth from the rearmost one I6 which is approximately nineteen thirty-seconds to the forwardmost one I'I which is approximately five thirty-seconds of an inch.
- a series of transversely arranged spaced relatively small rivet holes I8 are formed in each of the steps I5, the holes of each series or transverse row being in substantial alinement with each other and of considerably smaller diameter than the larger rivet holes 5, in the base cutting plate I I.
- each row contains from four to live holes I8, and when the top plate I I is centered or substantially centered with respect to the base plate I, at least one of the small holes I3 of each transverse row will be directly above and therefore will register with one of the large holes 5.
- the handle I3 By manipulating the handle I3 in anI appropriate direction any one of the small holes I8 can be caused to register with one of the larger holes 5.
- the two communicating holes 5 and I8, constitute an opening for the insertion of a standard size rivet 6, or bolts and screws of corresponding size.
- each of the coinciding or registering holes 5 and I8 correspondingly vary in height to' accommodate the standard sizes of aircraft rivets.
- the steps I5 and holes I8 are preferably marked or graduated to readily indicate' to the operator the proper holes within which to insert a rivet to assure of the same being sheared or severed to the required length.
- a rivet 6, ci the desired standard diameter is selected and, after determining the length to which the same is to be cut, is inserted in the proper rivet hole I8 which is marked to designate diameter and height.
- the handle I3 With the rivetin position, the handle I3 is moved either in a clockwise or a counterclockwise direction, viewing Figure l, so that the rivet hole i8, having the rivet arranged therein, is moved relative to the corresponding hole 5 in the xed base plate l, for example, from the full line to the dotted line position of Figure l.
- This rotary movement oi the top cutting plate i, about its pivot 9, causes the bottom and top peripheral edges i9 and 2i) ci the rivet holes I8 and 5, respectively, to impart a rotary cut around the circumference of the rivet shank, resulting in the rivet being uniformly and evenly cut without leaving any objectionable burr or uneven area on the face or the sides of the cut.
- the initial relative rotaryr movement of the top and bottom cutting plates causes the rivet to be initially scored or slightly sheared circumferentially, which cutting is continued, throughout the rotary movement of the top cutter plate I i, until the rivet is completely sheared.
- This cutting action is distinguished from that effected by bolt cutters, pliers, shears and other cutting tools.
- the heads 24 of the rivets 6 are caused to overhang the side walls of the adjacent ⁇ oiset thus facilitating removal of the rivets by enabling the operator to engage the extended portion of the head 24 and lift the rivet from its hole.
- a rivet 6, sheared in the cutting plate in the manner just described, will be assured of accurately fitting a standard size hole drilled in aircraft metal, without the necessity of driving or otherwiseforcing the same through the metal with consequent danger of deforming the latter and creating a Weak spot.
- a cutting tool for rivets and other fasteners comprising a xed base member having a plurality of longitudinally arranged rows of rivet receiving openingstherein, the openings of one row being staggered with respect to the-openings of the next adjacent row,.a cutting member'rotatably mounted on said base and being formed with a plurality of offset portions each having a transverse row of rivet receiving openings therein of varying length and diameter, said openings in the base member being oi considerably greater diameter than the largest opening in the cutting member and arranged in the path of movement of said last mentioned openings so that any one of several of the openings of each of saidtransverse rows of openings can be caused to register with one of the openings in said base member, and means for rotating said cutting member relative to said base member for shearing a rivet arranged in two of said registering openingsl 2.
- a cutting tool for rivets and other fasteners comprising a iixed base member having twolongitudinally arranged rows of substantially aligned relatively large rivet receiving openings therein, a cutting member normally longitudinally substantially aligned with and rotatably mounted on said base member and being formed'with a plurality of oiset portionseach having a transverse row of substantially aligned relatively small rivet receiving openings therein, said last mentioned openings being of varying lengthandldiev ameter and at least one of said openings in each of said transverse rows coinciding and ⁇ fully regiV istering with one of said relatively large openings in the base member when the cutting'member is in substantial longitudinal alignmentwitl'rthe base member, each of the openings in the *base memberl being in the path of movementfofn a plurality of the openings in each row ⁇ ofopenings formed in the cutting memberjand means', for rotating said cuttingmember relative rto said base member for shearing a rivet arranged i'rtwf
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Connection Of Plates (AREA)
Description
Patented May 16, 1944 UNITED STATES PATENT OFFICE 2,348,877' RIvET CUTTER Charles L. Beard, Lancaster, Pa.
Application August 23, 1943, Serial No. 499,668
2 ClamS. (Cl. 164-40) My invention relates to a rivet cutter particularly adapted for cutting rivets, bolts, screws etc. employed for riveting 0r fastening aircraft and other sheet metal.
The present invention constitutes an improvef ment over my Patent No. 2,288,385, dated June 30, 1942. In the patented tool a stepped top shearing plate is superimposed upon and pivoted to a base shearing plate, both plates being formed with transverse rows of rivet holes, the holes of each row being graduated in size and the holes of the top plate being similar inrsize to and registering with the corresponding holes of the bottom plate when the plates are longitudinally aligned. This construction proved objectionable due to the fact that the rivet holes of one plate must be in complete register with the corresponding holes of the companion plate, thus necessitating perfect centering of plates. Furthermore, the shearing action, due to the tight fit of the rivets in the top and bottom registering holes of the two plates, is not suiciently smooth to meet certain manufacturing requirements. Moreover, the necessity for duplicating in the base plate the large number of rivet holes required in the top plate materially increased the cost `of manufacture.
The objects of the present invention are to obviate the `foregoing objections. This is accomplished by providing the bottom or base plate with two longitudinal rows of staggered openings, of considerably greater size than the corresponding rivet holes of the top.plateand two or more of the rivet holes of the latter plate being adapted to be conveniently moved into operative registering relation with a corresponding hole in the bottom plate, thus reducing the number of holes required in the bottom plate, eliminating the necessity of accurately centering the plates one with respect to the other and insuring a free and smooth shearing cut.
The foregoing objects and advantages will be apparent as the specification is considered with the accompanying drawing, wherein:
Figure 1 is a plan View of the rivet cutter in rivet receiving position, and showing, in dotted lines, the position it assumes after performing the rivet cutting operation Figure 2 is a bottom plan view of the rivet cutter showing the top and bottom cutting plates in substantial alinement;
Figure 3 is a longitudinal sectional view of the rivet cutter.
Figure 4 is a section on the line 4-4 of Figure 1 showing a rivet in place and before being cut; and
Figure 5 is a side view of a rivet after being severed by the rivet cutter.
Referring more particularly to the drawing, wherein like reference characters refer to similar parts throughout the several views, numeral I designates a relatively at, substantially rectangular base cutting plate having the openings 2 for the reception of screws 3 to enable the plate to be removably secured to a flat work bench 4, or other suitable surface. If desired, the plate i may also be clamped in a bench vise and the like of airplane field service trucks, in an obvious manner not shown. The plate I is provided with two substantially longitudinally extending .rows of rivet holes 5, there being preferably four spaced holes in one row, and five spaced holes in the other and the holes of one row being irregularly staggered with respect to the holes of the other row. The holes 5 are preferably of equal size and are relatively large, that is, much larger than would be necessary to snugly accommodate a standard aircraft rivet of maximum size. The holes extend from the flat top face I of the plate I downwardly therethrough and terminate in a substantially U-shaped, groove 8, in the underside of the plate, which provides clearance for the lower ends of the rivets and permits of the severed ends thereof dropping onto the working surface 4.
Pivotally mounted on the base plate I, by means of an inset screw 9 and nut I5, is a substantially rectangular, top cutter or size plate II, somewhat smaller in area than the base plate. The bottom face I2 of the plate II is relatively flat and slidably engages with the flat top face I'of the base plate and is adapted to be pivotally moved or rotated thereover either in a counterclockwise or clockwise direction, viewing Figure l,v by means of a suitable rod or handle I3, mounted in a recess I4 in one end of the plate Il. The top face of the cutter plate II is provided with a series of preferably seven, substantially fiat steps or offsets I5 ranging in depth from the rearmost one I6 which is approximately nineteen thirty-seconds to the forwardmost one I'I which is approximately five thirty-seconds of an inch. A series of transversely arranged spaced relatively small rivet holes I8 are formed in each of the steps I5, the holes of each series or transverse row being in substantial alinement with each other and of considerably smaller diameter than the larger rivet holes 5, in the base cutting plate I I. There are preferably seven such translongitudinal slot or verse rows and each row contains from four to live holes I8, and when the top plate I I is centered or substantially centered with respect to the base plate I, at least one of the small holes I3 of each transverse row will be directly above and therefore will register with one of the large holes 5. By manipulating the handle I3 in anI appropriate direction any one of the small holes I8 can be caused to register with one of the larger holes 5. When this has been eiected, the two communicating holes 5 and I8, constitute an opening for the insertion of a standard size rivet 6, or bolts and screws of corresponding size. As the steps I5 vary in height from approximately iive thirty-seconds to approximately seventeen thirty-seconds of an inch, it will be noted that each of the coinciding or registering holes 5 and I8 correspondingly vary in height to' accommodate the standard sizes of aircraft rivets.
The steps I5 and holes I8 are preferably marked or graduated to readily indicate' to the operator the proper holes within which to insert a rivet to assure of the same being sheared or severed to the required length. When it is desired to perform the cutting operation, a rivet 6, ci the desired standard diameter, is selected and, after determining the length to which the same is to be cut, is inserted in the proper rivet hole I8 which is marked to designate diameter and height. With the rivetin position, the handle I3 is moved either in a clockwise or a counterclockwise direction, viewing Figure l, so that the rivet hole i8, having the rivet arranged therein, is moved relative to the corresponding hole 5 in the xed base plate l, for example, from the full line to the dotted line position of Figure l. This rotary movement oi the top cutting plate i, about its pivot 9, causes the bottom and top peripheral edges i9 and 2i) ci the rivet holes I8 and 5, respectively, to impart a rotary cut around the circumference of the rivet shank, resulting in the rivet being uniformly and evenly cut without leaving any objectionable burr or uneven area on the face or the sides of the cut. In other words, the initial relative rotaryr movement of the top and bottom cutting plates causes the rivet to be initially scored or slightly sheared circumferentially, which cutting is continued, throughout the rotary movement of the top cutter plate I i, until the rivet is completely sheared. This cutting action is distinguished from that effected by bolt cutters, pliers, shears and other cutting tools.
While in the interest of clarity I have only shown the top cutter plate in the position assumed when the handle I3 has been moved in a counter-clockwise direction, it will be understood that the cutting operation can be accomplished by rotating the top plate in either direction relatively to the base plate'. Y
Due to the steps I5 being formed in the top plate II, and separating the series of rivets receiving holes I8 the heads 24 of the rivets 6 are caused to overhang the side walls of the adjacent `oiset thus facilitating removal of the rivets by enabling the operator to engage the extended portion of the head 24 and lift the rivet from its hole.
A rivet 6, sheared in the cutting plate in the manner just described, will be assured of accurately fitting a standard size hole drilled in aircraft metal, without the necessity of driving or otherwiseforcing the same through the metal with consequent danger of deforming the latter and creating a Weak spot.
It is to be understood that various changes and improvements may be made in the present rivet cutting tool without departing from the scope and spirit of the appended claims.
Having thus described my invention, what I claim is:
1. A cutting tool for rivets and other fasteners comprising a xed base member having a plurality of longitudinally arranged rows of rivet receiving openingstherein, the openings of one row being staggered with respect to the-openings of the next adjacent row,.a cutting member'rotatably mounted on said base and being formed with a plurality of offset portions each having a transverse row of rivet receiving openings therein of varying length and diameter, said openings in the base member being oi considerably greater diameter than the largest opening in the cutting member and arranged in the path of movement of said last mentioned openings so that any one of several of the openings of each of saidtransverse rows of openings can be caused to register with one of the openings in said base member, and means for rotating said cutting member relative to said base member for shearing a rivet arranged in two of said registering openingsl 2. A cutting tool for rivets and other fasteners comprising a iixed base member having twolongitudinally arranged rows of substantially aligned relatively large rivet receiving openings therein, a cutting member normally longitudinally substantially aligned with and rotatably mounted on said base member and being formed'with a plurality of oiset portionseach having a transverse row of substantially aligned relatively small rivet receiving openings therein, said last mentioned openings being of varying lengthandldiev ameter and at least one of said openings in each of said transverse rows coinciding and `fully regiV istering with one of said relatively large openings in the base member when the cutting'member is in substantial longitudinal alignmentwitl'rthe base member, each of the openings in the *base memberl being in the path of movementfofn a plurality of the openings in each row` ofopenings formed in the cutting memberjand means', for rotating said cuttingmember relative rto said base member for shearing a rivet arranged i'rtwfo'f2 said coinciding openings. f'
VCHARLES I+ man
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US49966843 US2348877A (en) | 1943-08-23 | 1943-08-23 | Rivet cutter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US49966843 US2348877A (en) | 1943-08-23 | 1943-08-23 | Rivet cutter |
Publications (1)
Publication Number | Publication Date |
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US2348877A true US2348877A (en) | 1944-05-16 |
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ID=23986198
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US49966843 Expired - Lifetime US2348877A (en) | 1943-08-23 | 1943-08-23 | Rivet cutter |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4548111A (en) * | 1984-08-02 | 1985-10-22 | Sperry Corporation | Spiral orbital shear apparatus |
WO2023211892A1 (en) * | 2022-04-25 | 2023-11-02 | Ppc Broadband, Inc. | Coaxial cable connector pin cutting tool configured to provide one or more predetermined cut pin length settings |
-
1943
- 1943-08-23 US US49966843 patent/US2348877A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4548111A (en) * | 1984-08-02 | 1985-10-22 | Sperry Corporation | Spiral orbital shear apparatus |
WO2023211892A1 (en) * | 2022-04-25 | 2023-11-02 | Ppc Broadband, Inc. | Coaxial cable connector pin cutting tool configured to provide one or more predetermined cut pin length settings |
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