US180748A - Improvement in rivets - Google Patents
Improvement in rivets Download PDFInfo
- Publication number
- US180748A US180748A US180748DA US180748A US 180748 A US180748 A US 180748A US 180748D A US180748D A US 180748DA US 180748 A US180748 A US 180748A
- Authority
- US
- United States
- Prior art keywords
- rivet
- rivets
- burr
- head
- headed
- 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
Links
- 239000000463 material Substances 0.000 description 7
- 239000007787 solid Substances 0.000 description 6
- 238000010276 construction Methods 0.000 description 2
- 239000004744 fabric Substances 0.000 description 1
- 239000010985 leather Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J15/00—Riveting
- B21J15/02—Riveting procedures
- B21J15/04—Riveting hollow rivets mechanically
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B19/00—Bolts without screw-thread; Pins, including deformable elements; Rivets
- F16B19/04—Rivets; Spigots or the like fastened by riveting
- F16B19/05—Bolts fastening by swaged-on collars
Definitions
- My invention relates to the construction of rivets, and is more especially applicable to securing together two or more pieces of leather, rubber, cloth, or other flexible material, and is designed to be used in combination with a burr or washer, upon which it is headed.
- the rivet In the application of solid or tubular rivets, in combination with burrs for securing together two or more pieces of soft yielding ma terial, as heretofore practiced, the rivet has been headed by striking a single blow upon its end; and it has been found that, in consequence of the yielding nature of the material through which the rivet passes, and the fact that the shank or body of the rivet has an equal area in-cross-section at all points in its length, the greater part of the force of the blow is absorbed in upsetting the body of the rivet below the burr, and, as a consequence, but very little if any head is formed above the burr, and the articles are very imperfectly secured together.
- Figure 1 of the drawings is a section through the center of one of my improved rivets and its burr, in position to be headed.
- Fig. 2 is a similar section, showing the parts as they appear after being headed.
- Fig. 3 is a similar section, illustrating the appearance of the ordinary solid rivet and burr after being headed in yielding material; and
- Fig. 4 represents, in section, a rivet having the whole length of its shank made hollow, and of even thickness, as it appears after having been headed upon a burr and inclosed in a yielding material.
- A, Fig. 1 represents my improved rivet, provided with a head, a, and having drilled in the center of its point the chamber b, which is concentric with, and 'parallel to, the periphery of the body of the rivet, and extends to a depth about equal to the length of rivet which protrudes through the material, as shown.
- B represents the ordinary burr, placed over the end of the rivet, and resting upon the upper surface of the material G.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Insertion Pins And Rivets (AREA)
Description
11!. any.
RIVE'IIS.
Patented Aug.8, 1876.
INVENTOR.
WlTNESSES.
UNITED STATES] PATENT OFFICE.
MELLEN BRAY, or NEWTON, MASSACHUSETTS.
IMPROVEMENT IN RIVETS.
Specification forming part of Letters Patent No. 180,748, dated August 8, 1876; application filed January 12, 1876.
To all whom it may concern Be it known that I, MELLEN BRAY, of Newton, in the county of Middlesex and State of Massachusetts, have invented a new and useful Improvement in Rivets, of which the following, taken in connection with the accompanyin g drawings, is a specification:
My invention relates to the construction of rivets, and is more especially applicable to securing together two or more pieces of leather, rubber, cloth, or other flexible material, and is designed to be used in combination with a burr or washer, upon which it is headed.
In the application of solid or tubular rivets, in combination with burrs for securing together two or more pieces of soft yielding ma terial, as heretofore practiced, the rivet has been headed by striking a single blow upon its end; and it has been found that, in consequence of the yielding nature of the material through which the rivet passes, and the fact that the shank or body of the rivet has an equal area in-cross-section at all points in its length, the greater part of the force of the blow is absorbed in upsetting the body of the rivet below the burr, and, as a consequence, but very little if any head is formed above the burr, and the articles are very imperfectly secured together.
To obviate this difficulty I take a solid rivet and drill a hole in the center of its point to a depth about equal to the length that the rivet is to protrude through the material to be secured before it is headed, thus reducing the amount of stock in the point of the rivet, and forming therein a chamber, the walls of which are substantially parallel to the exterior periphery of the shank of the rivets, while that portion of the rivet between the burr and the head of the rivet remains solid. v
By this construction I am enabled, at a single blow, to form a good firm head above the burr Without upsetting or enlarging the rivet between the head and the burr.
Figure 1 of the drawings is a section through the center of one of my improved rivets and its burr, in position to be headed. Fig. 2 is a similar section, showing the parts as they appear after being headed. Fig. 3 is a similar section, illustrating the appearance of the ordinary solid rivet and burr after being headed in yielding material; and Fig. 4 represents, in section, a rivet having the whole length of its shank made hollow, and of even thickness, as it appears after having been headed upon a burr and inclosed in a yielding material.
A, Fig. 1, represents my improved rivet, provided with a head, a, and having drilled in the center of its point the chamber b, which is concentric with, and 'parallel to, the periphery of the body of the rivet, and extends to a depth about equal to the length of rivet which protrudes through the material, as shown. B represents the ordinary burr, placed over the end of the rivet, and resting upon the upper surface of the material G.
It, now, a blow be struck upon the end of the rivet A by means of a hammer or springplunger, while the head a rests upon a suitable anvil, the tubular end thereof will be headed down over the burr B, as shown in Fig. 2, without affecting materially that portion of the body of the rivet between its head and the burr.
If a similar blow be struck on the end of the solid rivet D, or a tubular rivet, E, having the whole length of its shank made hollow and -of even thickness, to head them down upon the burrs c and d, the first and principal efl'ect of said blow is to upset or expand the body of the rivets near their heads, as shown in Figs. 3 and 4, and, as a consequence, but very little head -will be formed unless a second, or perhaps a third, blow is struck, which is impracticable to do in setting such rivets by automatic machinery, such as is usually used for the purpose.
I do not claim, broadly, a tubular rivet, for I am aware that rivets having their entire shanks made hollow, or in the form of a tube, have been used before; neither do I claim a rivet having its end countersunk to aid in heading, as I am aware that such rivets have been used; but they do not fully meet the requirements of the case.
What I claim as my invention, and desire Executed at Boston, Massachusetts, this to secure by Letters Patent of the United 26th day of November, 1875.
States, is-
As a new article of manufacture, a rivet MELLEN BRAY. having a portion of the length of its shank made tubular, and of nearly even thickness, Witnesses: and the remaining portion next its head made N. G. LOMBARD,
solid, as and for the purpose described. WM. P. EDWARDS.
Publications (1)
Publication Number | Publication Date |
---|---|
US180748A true US180748A (en) | 1876-08-08 |
Family
ID=2250154
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US180748D Expired - Lifetime US180748A (en) | Improvement in rivets |
Country Status (1)
Country | Link |
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US (1) | US180748A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2471359A (en) * | 1946-01-30 | 1949-05-24 | Stevens Nichols | Tire casing repair device |
US2511920A (en) * | 1950-06-20 | Method of riveting and assemblage | ||
US2619564A (en) * | 1948-03-12 | 1952-11-25 | Underwood Electric & Mfg Co In | Circuit breaker |
US4088053A (en) * | 1973-09-21 | 1978-05-09 | Lockheed Aircraft Corporation | Cavity rivet assembly |
-
0
- US US180748D patent/US180748A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2511920A (en) * | 1950-06-20 | Method of riveting and assemblage | ||
US2471359A (en) * | 1946-01-30 | 1949-05-24 | Stevens Nichols | Tire casing repair device |
US2619564A (en) * | 1948-03-12 | 1952-11-25 | Underwood Electric & Mfg Co In | Circuit breaker |
US4088053A (en) * | 1973-09-21 | 1978-05-09 | Lockheed Aircraft Corporation | Cavity rivet assembly |
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