US1548990A - Drag link - Google Patents

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Publication number
US1548990A
US1548990A US522376A US52237621A US1548990A US 1548990 A US1548990 A US 1548990A US 522376 A US522376 A US 522376A US 52237621 A US52237621 A US 52237621A US 1548990 A US1548990 A US 1548990A
Authority
US
United States
Prior art keywords
body member
link
socket
tubular
socket member
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
US522376A
Inventor
Harry B Garman
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.)
Steel Products Co
Original Assignee
Steel Products Co
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 Steel Products Co filed Critical Steel Products Co
Priority to US522376A priority Critical patent/US1548990A/en
Application granted granted Critical
Publication of US1548990A publication Critical patent/US1548990A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D7/00Steering linkage; Stub axles or their mountings
    • B62D7/20Links, e.g. track rods
    • 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
    • Y10T29/49917Overedge assembling of seated part by necking in cup or tube wall
    • 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
    • Y10T29/49925Inward deformation of aperture or hollow body wall
    • Y10T29/49927Hollow body is axially joined cup or tube
    • 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
    • Y10T29/49925Inward deformation of aperture or hollow body wall
    • Y10T29/49927Hollow body is axially joined cup or tube
    • Y10T29/49929Joined to rod
    • 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
    • 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
    • Y10T29/4994Radially expanding internal tube
    • 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
    • Y10T403/4991Both members deformed

Description

Aug. 11, 1925.
H. E. GARMAN DRAG LINK Filed Dec. 14, 1921 2 Sheets-Sheet l 2 Sheets-Sheet 2 H. B. GARMAN DRAG LINK Filed Dec. l4, 1921 Aug. 1l,` 1925.
Patented tug. 11, 1925.
HARRY B. GARMAN, OF DETROT, IVICI-IIGAN, ASSIGNOR TO THE STEEL PRGDUCTS COT/IPANY, OF CLEVELAND, OHIO, A CORPORATON OF O'HIO.
DRAG LINK.
Application filed December 14, 1921.
To all whom t may concern.'
Be it known that I, Hanni B. GARMAN, a citizen of the United States, resi t of Detroit, county of TvVa-yne, and State of Michigan, have invented new and useful Improvements in Drag Links, of which the following is a. specification, the principle of the invention being herein explained and the best mode in which I have contemplated applying that principle, so as to distinguish it from other inventions.
This invention relates to drag links for use as a part of the steering mechanism of automobiles and more particularly the connection of the enlarged end sockets to the central body portion of the link.
1t is the object of this invention to pron vide a link which can be cheaply constructed, is neat in appearance and is possessed of the necessary rigidity and strength. More speci ically, it is the object of this invention to provide a joint between Vthe end sockets and the central body portion of the link which permits quick assembly and interlocking of the parts in forming a permanent connection between them, and by means of which the parts are rigidly held against relative movement either longitudinally or circumferentia-ily.
rThe annexed drawings and the following description set forth in detail certain means embodying my invention, the disclosed means, however, constituting but a few of the various mechanical forms in which the principle of the invention may be employed.
1n said annexed drawings:
Fig. 1 is a broken plan view showing one end of the link in section.
Fig. 2 is a longitudinal section through an end socket before assembling.
Fig. 3 is a fragmentary longitudinal section of an end of the central portion of the link before assembling.
Fig. L1 is a section on line N,F-IV of Fig. 1.
Fig. 5 is a broken plan view partly in section showing a link with a solid body portion.
Fig. 6 is a broken plan view of the solid body portion before showing one end thereof in section.
Fig. 7 is a section on line VHVH of Fig. 5.
Serial No. 522,376.
Fig. 8 is a broken plan view of a link havingl a slightly modified form of joint, one end being` shown in section.
Fig. 9 is a longitudinal sec-ion through the end socket member of Fig. 8 before assembling.
Fig. 10 is a longitudinal section through the central body member of Fig. 8 before assembling.
in the modification shown. in Figs. 1 to 4 inclusive, the drag link consists of a central tubular body portion 1, and enlarged tubular end socket members 2. As shown in Fig. 2 the socket members 2 have a restricted neck portion 3 at one end, the internal ldia-meter of which is such as to fit snugly upon the central tubular body member 2. As shown in Fig. 3 the central body portion 1 is first formed with external ribs or shoulders d spaced somewhat from the ends thereof. In assembling the link-the neck portion 3 of a socket member 2 is slipped on the end of the body member 1 with the end thereof in engagement with the shoulder 4i. The outer end 5 of the tubular body member is then upset or expanded within the enlarged portion of the socket member 2 to fit against the shoulder 6 formed by the reduced neck portion 3. lindentations 7 are then formed in the neck portion 3 of the socket member and the tubular body member 1 effectually locking the members 1 and 2 against relative circumferential movement.
In the modification shown in Figs. 5, 6 and 'i' the cent-ral body portion 8 of the link is a solid bar. rFhe end socket members 9 are exactly the same as in Fig. 1. The neck portion 10 fits snugly upon the end of the body member 8 with its outer end in engagement with the shoulder 11 on the body inember, the outer end 12 of the body member is upset within the. socket member 9 against the shoulder 13 at the inner end of the neck portieri, and the neck portion 10 has indentations 14- projeeting into the solid body member 8.
In the modification shown in Figs. 8, 9 and 10 the tubular body member 15 has peripheral grooves 16 formed therein adjacent the ends thereof. An end socket member 17 has a reduced neck portion 18 adapted to fit snugly on the body member 15. rThe neck portion 18 is slipped on the end of the body member 15 and peripheral grooves 19 are formed therein, the internal ribs formed by the grooves 19 filling the grooves 16 of the body member. The inner end 2O of the body member 15 is then expanded or upset inside the socket member 17 against the shoulders Q1 at the inner end of the neck portion 1S.
hat l: claim is:
1. A drag` link comprising` a tubular body member; and a tubular end socket member, said socket member having a restricted tubular end portion fitting;` over said body member, the end of said body member being expanded to iit within the internal shoulder at the inner end of said restricted portion or' the socket member, said restricted portion of the socket member and the body member having additional interengaging shoulders.
2. A drag link comprising a body member, and a tubular end socket member, said socket member having` a restricted tubular end portion fitting over said body member, said body member having an upset shoulder adapted to engage the outer end of said restricted portion of the socket member, the inner end of said body member being upset Within the tubular member to iit against the shoulder at the inner end of said restricted portion of the socket member, the restricted portion of said socket member having' an indentation projecting into said body member.
Signed this 9th day of November, 1921.
HARRY B. GARA/IAN.
US522376A 1921-12-14 1921-12-14 Drag link Expired - Lifetime US1548990A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US522376A US1548990A (en) 1921-12-14 1921-12-14 Drag link

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US522376A US1548990A (en) 1921-12-14 1921-12-14 Drag link

Publications (1)

Publication Number Publication Date
US1548990A true US1548990A (en) 1925-08-11

Family

ID=24080619

Family Applications (1)

Application Number Title Priority Date Filing Date
US522376A Expired - Lifetime US1548990A (en) 1921-12-14 1921-12-14 Drag link

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Country Link
US (1) US1548990A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2584696A (en) * 1947-09-16 1952-02-05 Thompson Prod Inc Rod and tube assembly
US2589820A (en) * 1948-09-08 1952-03-18 Anton W Konchan Shock absorber link
US4010533A (en) * 1974-12-11 1977-03-08 Nadella Method of producing a transmission device
US4513488A (en) * 1982-02-08 1985-04-30 Grumman Aerospace Corporation Method of fabricating a torque joint
US4523872A (en) * 1981-08-12 1985-06-18 Grumman Aerospace Corporation Torsion resistant grooved joint
US4561799A (en) * 1982-02-08 1985-12-31 Grumman Aerospace Corp. Torque joint
US5623756A (en) * 1994-09-22 1997-04-29 Nsk Ltd. Method of manufacturing a shock absorbing type steering shaft
US5937496A (en) * 1996-07-09 1999-08-17 Nbg Technologies, Inc. Electromagnetic joint forming method for mobile unit frames
US20040055133A1 (en) * 2002-09-24 2004-03-25 Saha Pradip K. Low chamfer angled torque tube end fitting metal
US20040081509A1 (en) * 2002-10-15 2004-04-29 Hitachi Unisia Autimotive Ltd. Structure and method of coupling shaft member and cylindrical member
US20050051224A1 (en) * 2002-09-24 2005-03-10 The Boeing Company Low chamfer angled torque tube end fitting with elongated overflow groove
US20120080862A1 (en) * 2010-09-30 2012-04-05 Hendrickson Usa, L.L.C. Heavy-duty axle-to-beam connection
US11518190B2 (en) 2017-10-23 2022-12-06 Hendrickson United Kingdom Ltd Heavy-duty connections e.g. for axle/suspension systems

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2584696A (en) * 1947-09-16 1952-02-05 Thompson Prod Inc Rod and tube assembly
US2589820A (en) * 1948-09-08 1952-03-18 Anton W Konchan Shock absorber link
US4010533A (en) * 1974-12-11 1977-03-08 Nadella Method of producing a transmission device
US4523872A (en) * 1981-08-12 1985-06-18 Grumman Aerospace Corporation Torsion resistant grooved joint
US4513488A (en) * 1982-02-08 1985-04-30 Grumman Aerospace Corporation Method of fabricating a torque joint
US4561799A (en) * 1982-02-08 1985-12-31 Grumman Aerospace Corp. Torque joint
US5623756A (en) * 1994-09-22 1997-04-29 Nsk Ltd. Method of manufacturing a shock absorbing type steering shaft
US5937496A (en) * 1996-07-09 1999-08-17 Nbg Technologies, Inc. Electromagnetic joint forming method for mobile unit frames
US20040055133A1 (en) * 2002-09-24 2004-03-25 Saha Pradip K. Low chamfer angled torque tube end fitting metal
US20050051224A1 (en) * 2002-09-24 2005-03-10 The Boeing Company Low chamfer angled torque tube end fitting with elongated overflow groove
US6932118B2 (en) * 2002-09-24 2005-08-23 The Boeing Company Low chamfer angled torque tube end fitting metal
US7363945B2 (en) * 2002-09-24 2008-04-29 The Boeing Co. Low chamfer angled torque tube end fitting with elongated overflow groove
US20040081509A1 (en) * 2002-10-15 2004-04-29 Hitachi Unisia Autimotive Ltd. Structure and method of coupling shaft member and cylindrical member
US20120080862A1 (en) * 2010-09-30 2012-04-05 Hendrickson Usa, L.L.C. Heavy-duty axle-to-beam connection
US8454040B2 (en) * 2010-09-30 2013-06-04 Hendrickson Usa, L.L.C. Heavy-duty axle-to-beam connection
US11518190B2 (en) 2017-10-23 2022-12-06 Hendrickson United Kingdom Ltd Heavy-duty connections e.g. for axle/suspension systems

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