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US2194458A - Compressible rivet - Google Patents

Compressible rivet Download PDF

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Publication number
US2194458A
US2194458A US211680A US21168038A US2194458A US 2194458 A US2194458 A US 2194458A US 211680 A US211680 A US 211680A US 21168038 A US21168038 A US 21168038A US 2194458 A US2194458 A US 2194458A
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US
United States
Prior art keywords
rivet
shank
rivets
serrated
head
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
Application number
US211680A
Inventor
Harlan E Eckler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bell Aircraft Corp
Original Assignee
Bell Aircraft Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bell Aircraft Corp filed Critical Bell Aircraft Corp
Priority to US211680A priority Critical patent/US2194458A/en
Application granted granted Critical
Publication of US2194458A publication Critical patent/US2194458A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B19/00Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/04Rivets; Spigots or the like fastened by riveting
    • F16B19/06Solid rivets made in one piece
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B4/00Shrinkage connections, e.g. assembled with the parts at different temperature; Force fits; Non-releasable friction-grip fastenings
    • F16B4/004Press fits, force fits, interference fits, i.e. fits without heat or chemical treatment
    • 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
    • Y10T29/49972Method of mechanical manufacture with separating, localizing, or eliminating of as-cast defects from a metal casting [e.g., anti-pipe]

Definitions

  • This invention relates to a rivet, and more particularly to a method of clamping two component parts of an assembly together by the use of a serrated rivet, the serrations of which are deep enough to make the rivet a drive t for superimposed holes formed in the assembly.
  • One of the objects of this invention is to avoid the above-mentioned disadvantages of the prior art.
  • Another object of this invention is to provide a serrated device which may be used to hold the component parts of a structure together before riveting, and which will also serve as a rivet.
  • Still another object of my invention is to provide a rivet consisting of a head and a shank, the portion of the shank next to the head being provided with serrations which are deep enough to make the rivet a drive iit in a rivet hole, the remainder of the shank being of the same diameter as the said hole.
  • a further object of this invention is to provide a method of riveting the component parts of an assembly together, by which the preliminary use of a removable holding device is eliminated.
  • Figure l is a longitudinal section taken through a fragment of metal fabrication disclosing a row of rivets, a number of which have been squeezed.
  • Figure 2 is a cross-sectional view taken along line 2 2 of Figure 1 looking in the direction of the arrows.
  • Figure 3 is a view partially in section taken along line 3-3 of Figure l looking in the direction of the arrows.
  • Figure i is a fragmentary view taken along line 4-4 of Figure 2 looking in the direction of the arrows.
  • Figure 5 is a perspective view of the rivet.
  • this invention consists of a serrated rivet, generally designated by. the lnumeral I, which consists of a head 2 and a shank 3.
  • 'I'he shank 3 includes a straight knurled porl0 .tion 4 adjacent the head 2, and a smooth portion 5 located at the lower end of the shank 3.
  • the knurled portion 4 consists of a plurality of longitudinal serrations which increase the diameter of the shank to such size as to make 15 the rivet a drive lt in a rivet hole.
  • the diameter of the smooth portion 5, on the other hand, is approximately the diameter of the hole into which the rivet is to be driven.
  • the head 2 may be formed in any desired shape.
  • FIG. 1 two structural members 9 and lil are shown in Figure 1 which are provided with rivet holes, as shown at ll.
  • these structural members may be held together by driving serrated rivets into properly spaced holes. Ordinary rivets may then be placed in the remaining holes and all the rivets squeezed in one rivet ing operation. Of course, if desired, only serrated rivets may be used for the riveting job in place of the ordinary rivets.
  • the shank 3 of the serrated rivet l is driven into the standard rivet hole H by a hammer or other means, as best shown in Figure 2.
  • the rounded portion 5 passes easily through the hole il.
  • the outer edges oi the serrations being several thousandths of an inch larger than the hole, must be driven in, thereby forming a 4o frictional engagement against the side of the hole, as shown at l2 in Figure 4.
  • the smooth portion 45 5 of the shank 3 is adapted to be squeezed to form a head I3 during the riveting operation.
  • the length of the knurled portion l of the shank is adapted to conform with the thickness of the several parts of the members being riv- 50 eted together.
  • the shank of the rivet is knurled with the exception of sumcient length to form a head on the inserted end.
  • a rivet made of ductile metal which is designed to hold metallic component parts in frictional engagement by being driven into aligned 'apertures in the said component parts, comprising a head and an annular shank, the portion adjacent the head being enlarged by longitudinal serrations which are wedge-shaped in cross section, said serrations being adapted to collapse to frictionally engage the walls of the said apertures whenthe rivet is driven into operative position, and the remainder of the shank being adapted to be formed into a head.
  • a rivet made of ductile metal which is designed to hold metallic component parts in frictional engagement by being driven into aligned apertures in the said component parts, comprising a head and an annular shank, the portion adjacent the head being enlarged by longitudinal serrations which are wedge-shaped incross section, ⁇ said serrated portion being approximately the same length as the combined widths of the component parts, and said serrations being adapted to collapse to frictionally engage the walls of the said apertures when -the rivet is driven, into operative position, the remainder of the shank being adapted to be formed into a head.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Insertion Pins And Rivets (AREA)

Description

March 26, 1940. H, E, ECKLER 2,194,458
COMPRESSIBLE RIVEI Filed June 3, 1938 :l A l n A@ Patented Mu. 26,1940
PATENT OFFICE COMPRES SIBLE RIVET Harlan E. E'ck'ler, Buffalo, N. Y., assigner to Bell Aircraft Corporation, Buffalo, N. Y., a corporation oi.' New York Application June 3, 1938, Serial No. 211,680
2 Claims.
This invention relates to a rivet, and more particularly to a method of clamping two component parts of an assembly together by the use of a serrated rivet, the serrations of which are deep enough to make the rivet a drive t for superimposed holes formed in the assembly. f
Previously, when it has been desired to fasten component parts together to form an assembly,
l it has been necessary to provide means to temporarily hold these parts in position until the riveting has been completed. This is usually accomplished by inserting removable holding de vices into a series of selected holes which are sufficiently spaced to insure the parts being held together by the insertion of these devices until rivets have been secured in the remaining holes.
This procedure necessitates the withdrawal of the devices from the spotted holes, after the preliminary riveting has been completed, and the insertion of' rivets after these holes have been cleared. Occasionally, various types of clamping devices have also been used to hold the component parts together until the riveting has been completed. These, however, must also be removed.
One of the objects of this invention is to avoid the above-mentioned disadvantages of the prior art.
Another object of this invention is to provide a serrated device which may be used to hold the component parts of a structure together before riveting, and which will also serve as a rivet.
Still another object of my invention is to provide a rivet consisting of a head and a shank, the portion of the shank next to the head being provided with serrations which are deep enough to make the rivet a drive iit in a rivet hole, the remainder of the shank being of the same diameter as the said hole.
A further object of this invention is to provide a method of riveting the component parts of an assembly together, by which the preliminary use of a removable holding device is eliminated.
In the drawing:
Figure l is a longitudinal section taken through a fragment of metal fabrication disclosing a row of rivets, a number of which have been squeezed.
Figure 2 is a cross-sectional view taken along line 2 2 of Figure 1 looking in the direction of the arrows.
Figure 3 is a view partially in section taken along line 3-3 of Figure l looking in the direction of the arrows.
Figure i is a fragmentary view taken along line 4-4 of Figure 2 looking in the direction of the arrows.
Figure 5 is a perspective view of the rivet.
As shown in Figure 5, this invention consists of a serrated rivet, generally designated by. the lnumeral I, which consists of a head 2 and a shank 3. 'I'he shank 3 includes a straight knurled porl0 .tion 4 adjacent the head 2, and a smooth portion 5 located at the lower end of the shank 3.
The knurled portion 4 consists of a plurality of longitudinal serrations which increase the diameter of the shank to such size as to make 15 the rivet a drive lt in a rivet hole. The diameter of the smooth portion 5, on the other hand, is approximately the diameter of the hole into which the rivet is to be driven. The head 2 may be formed in any desired shape.
To illustrate the use of this rivet, two structural members 9 and lil are shown in Figure 1 which are provided with rivet holes, as shown at ll. In practicing my invention these structural members may be held together by driving serrated rivets into properly spaced holes. Ordinary rivets may then be placed in the remaining holes and all the rivets squeezed in one rivet ing operation. Of course, if desired, only serrated rivets may be used for the riveting job in place of the ordinary rivets.
In order to temporarily hold the structural members 9 and l0 together, the shank 3 of the serrated rivet l is driven into the standard rivet hole H by a hammer or other means, as best shown in Figure 2. During this operation the rounded portion 5 passes easily through the hole il. However, the outer edges oi the serrations, being several thousandths of an inch larger than the hole, must be driven in, thereby forming a 4o frictional engagement against the side of the hole, as shown at l2 in Figure 4. 'Ihis tight fit enables the rivet to hold the component parts together in proper alignment until the ordinary rivets have beenkinserted. The smooth portion 45 5 of the shank 3 is adapted to be squeezed to form a head I3 during the riveting operation.
The length of the knurled portion l of the shank is adapted to conform with the thickness of the several parts of the members being riv- 50 eted together. In other words, the shank of the rivet is knurled with the exception of sumcient length to form a head on the inserted end.
From the above description it is believed apparent that, by the use of this serrated rivet, Il
two methods have been provided by which structural members may be joined. In both methods all the holes in both component parts may be drilled to standard size and are. therefore, adapted for the use of my serrated rivet. However, if desired, my rivet may be used in only acertain number of properly spaced holes and ordinary rivets lused in the remaining apertures. After the ordinary rivets have been headed, the serrated rivets which have been driven into the spotted holes may also be mechanically squeezed.
While it is apparent that these serrated rivets may be made of any type of ductile alloys or metals, I have found that serrated rivets made of aluminum alloy are very satisfactory. This is especially true when the serrated rivets are to be used in connection with aircraft construction.V
Moreover, the shape of the rivet or its length may be varied, or the whole shank may be serrated, without departing from the concept of this invention. I, therefore, wish only to be limited by the extent of the prior art and the scope of the appended claims.
I claim:
1. A rivet made of ductile metal which is designed to hold metallic component parts in frictional engagement by being driven into aligned 'apertures in the said component parts, comprising a head and an annular shank, the portion adjacent the head being enlarged by longitudinal serrations which are wedge-shaped in cross section, said serrations being adapted to collapse to frictionally engage the walls of the said apertures whenthe rivet is driven into operative position, and the remainder of the shank being adapted to be formed into a head.
2. A rivet made of ductile metal which is designed to hold metallic component parts in frictional engagement by being driven into aligned apertures in the said component parts, comprising a head and an annular shank, the portion adjacent the head being enlarged by longitudinal serrations which are wedge-shaped incross section,` said serrated portion being approximately the same length as the combined widths of the component parts, and said serrations being adapted to collapse to frictionally engage the walls of the said apertures when -the rivet is driven, into operative position, the remainder of the shank being adapted to be formed into a head. t
HARLAN E. ECKLER.
US211680A 1938-06-03 1938-06-03 Compressible rivet Expired - Lifetime US2194458A (en)

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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2542144A (en) * 1945-01-01 1951-02-20 Shellmar Products Corp Blind rivet
US2594840A (en) * 1946-04-29 1952-04-29 Grigsby Allison Company Inc Riveted joint
US2642242A (en) * 1950-10-24 1953-06-16 Diamond Expansion Bolt Co Drive ring
US2753624A (en) * 1952-02-06 1956-07-10 English Electric Co Ltd Method of assembling two components by a fastener
US2781144A (en) * 1950-04-11 1957-02-12 Grigsby Allison Company Inc Riveting apparatus
US3154841A (en) * 1961-04-17 1964-11-03 Coro Inc Of Rhode Island Method of manufacture of article of jewelry
US3240100A (en) * 1963-05-09 1966-03-15 Standard Screw Drive pin
DE1540644B1 (en) * 1963-02-22 1971-08-12 Aerpat Ag Connection part for electrical lines that can be inserted and locked in a hole in a strip or plate
US3827004A (en) * 1972-05-10 1974-07-30 Du Pont Circuit board pin
US3980367A (en) * 1975-03-19 1976-09-14 Sealectro Corporation Electrical connector for joining conductors attached to printed circuit boards
US4012884A (en) * 1971-09-21 1977-03-22 Kaynar Mfg. Co., Inc. Prestressed connection and fastener therefor
US4736494A (en) * 1984-07-06 1988-04-12 Minu S.P.A. Magnetic button for articles of clothing, leather goods, and the like
US5690459A (en) * 1996-05-29 1997-11-25 Textron Inc. Plate and riveted stud assembly
WO2001030516A1 (en) * 1999-10-26 2001-05-03 Toyota Jidosha Kabushiki Kaisha Rivet, riveted joint structure, riveting apparatus, and riveting method
USD669442S1 (en) * 2009-05-15 2012-10-23 Bowen Iii Frank Randolph Set of magnets
US20130315690A1 (en) * 2012-05-25 2013-11-28 Sungwoo Hitech Co., Ltd. Self-piercing rivet
US20160061245A1 (en) * 2014-04-24 2016-03-03 Teijin Limited Fiber Reinforced Resin Joined Body, Intermediate Body, and Fastening Rod
US11105353B2 (en) * 2018-04-10 2021-08-31 C.R.F. Societa Consortile Per Azioni Connection system for connecting two or more overlapping layers of material, and related joint and connection method

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2542144A (en) * 1945-01-01 1951-02-20 Shellmar Products Corp Blind rivet
US2594840A (en) * 1946-04-29 1952-04-29 Grigsby Allison Company Inc Riveted joint
US2781144A (en) * 1950-04-11 1957-02-12 Grigsby Allison Company Inc Riveting apparatus
US2642242A (en) * 1950-10-24 1953-06-16 Diamond Expansion Bolt Co Drive ring
US2753624A (en) * 1952-02-06 1956-07-10 English Electric Co Ltd Method of assembling two components by a fastener
US3154841A (en) * 1961-04-17 1964-11-03 Coro Inc Of Rhode Island Method of manufacture of article of jewelry
DE1540644B1 (en) * 1963-02-22 1971-08-12 Aerpat Ag Connection part for electrical lines that can be inserted and locked in a hole in a strip or plate
US3240100A (en) * 1963-05-09 1966-03-15 Standard Screw Drive pin
US4012884A (en) * 1971-09-21 1977-03-22 Kaynar Mfg. Co., Inc. Prestressed connection and fastener therefor
US3827004A (en) * 1972-05-10 1974-07-30 Du Pont Circuit board pin
US3980367A (en) * 1975-03-19 1976-09-14 Sealectro Corporation Electrical connector for joining conductors attached to printed circuit boards
US4736494A (en) * 1984-07-06 1988-04-12 Minu S.P.A. Magnetic button for articles of clothing, leather goods, and the like
US5690459A (en) * 1996-05-29 1997-11-25 Textron Inc. Plate and riveted stud assembly
WO2001030516A1 (en) * 1999-10-26 2001-05-03 Toyota Jidosha Kabushiki Kaisha Rivet, riveted joint structure, riveting apparatus, and riveting method
US6988862B1 (en) 1999-10-26 2006-01-24 Toyota Jidosha Kabushiki Kaisha Rivet, riveted joint structure riveting apparatus, and riveting method
USD669442S1 (en) * 2009-05-15 2012-10-23 Bowen Iii Frank Randolph Set of magnets
US20130315690A1 (en) * 2012-05-25 2013-11-28 Sungwoo Hitech Co., Ltd. Self-piercing rivet
US8851814B2 (en) * 2012-05-25 2014-10-07 Sungwoo Hitech Co., Ltd. Self-piercing rivet
US20160061245A1 (en) * 2014-04-24 2016-03-03 Teijin Limited Fiber Reinforced Resin Joined Body, Intermediate Body, and Fastening Rod
US9556891B2 (en) * 2014-04-24 2017-01-31 Teijin Limited Fiber reinforced resin joined body, intermediate body, and fastening rod
US11105353B2 (en) * 2018-04-10 2021-08-31 C.R.F. Societa Consortile Per Azioni Connection system for connecting two or more overlapping layers of material, and related joint and connection method

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