CA176217S - Tie rod end - Google Patents

Tie rod end

Info

Publication number
CA176217S
CA176217S CA176217F CA176217F CA176217S CA 176217 S CA176217 S CA 176217S CA 176217 F CA176217 F CA 176217F CA 176217 F CA176217 F CA 176217F CA 176217 S CA176217 S CA 176217S
Authority
CA
Canada
Prior art keywords
view
design
tie rod
rod end
plan
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.)
Active
Application number
CA176217F
Other versions
CA1011229A (en
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.)
Aircraft Gear Corp
Original Assignee
Aircraft Gear 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 Aircraft Gear Corp filed Critical Aircraft Gear Corp
Application granted granted Critical
Publication of CA176217S publication Critical patent/CA176217S/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The design consists of the features of shape and configuration as applied to a tie rod end as illustrated in solid lines in the drawings. The portions shown in stippled lines do not form part of the design. The environment shown in stippled lines in Fig. 7 does not form part of the design.Drawings of the design are included, in which:FIG. 1 is a left, front, and top perspective view of a tie rod end in accordance with the present design;FIG. 2 is a front plan view thereof; the rear view being identical;FIG. 3 is a top plan view thereof;FIG. 4 is a bottom plan view thereof;FIG. 5 is a left end view thereof;FIG. 6 is a right end view thereof; andFIG. 7 is a left, front, and top perspective view thereof, shown with its environment.
CA176217F 2017-02-02 2017-08-01 Tie rod end Active CA176217S (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/592,797 USD847036S1 (en) 2017-02-02 2017-02-02 Tie rod end

Publications (1)

Publication Number Publication Date
CA176217S true CA176217S (en) 2018-06-27

Family

ID=62750447

Family Applications (1)

Application Number Title Priority Date Filing Date
CA176217F Active CA176217S (en) 2017-02-02 2017-08-01 Tie rod end

Country Status (2)

Country Link
US (1) USD847036S1 (en)
CA (1) CA176217S (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD847696S1 (en) * 2017-02-02 2019-05-07 Aircraft Gear Corporation Tie rod connector
USD852684S1 (en) * 2017-02-18 2019-07-02 Aircraft Gear Corporation Shaft
USD967241S1 (en) * 2020-11-13 2022-10-18 Spartan Boss Ltd Bipod leg

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FR813920A (en) 1935-12-09 1937-06-11 G & J Weir Ltd Ball joint
US3103377A (en) 1958-08-25 1963-09-10 Moog Industries Inc Adjustable ball joint
GB891798A (en) 1959-07-20 1962-03-21 Eng Productions Clevedon Ltd Improvements in ball joints
GB992100A (en) 1964-03-03 1965-05-12 William Charles Wehner Swivel joint
US3325197A (en) 1964-06-12 1967-06-13 Moog Industries Inc Ball joint
US3418011A (en) 1966-05-31 1968-12-24 Moog Industries Inc Wear-compensating ball joints
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USD294219S (en) * 1985-04-17 1988-02-16 George Hamatani Bushing puller
US5116159A (en) 1990-08-23 1992-05-26 Dana Corporation Ball and socket joint assembly
US5287776A (en) * 1992-06-26 1994-02-22 Lisle Corporation Inner tie rod tool
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US5794341A (en) * 1995-12-28 1998-08-18 Aircraft Gear Corporation Method for assembling a constant velocity universal joint
US5839845A (en) 1996-02-02 1998-11-24 American Axle & Manufacturing Adjustable torque pivot joint
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CA121646S (en) * 2007-01-29 2008-04-10 A M A Cardan S R L Universal joint transmission
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US9324462B2 (en) * 2010-07-13 2016-04-26 Westinghouse Electric Company Llc Reactor head seismic support tie rod system
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JP6125186B2 (en) * 2012-10-12 2017-05-10 Ntn株式会社 Fixed constant velocity universal joint
KR101519753B1 (en) * 2013-12-18 2015-05-12 현대자동차주식회사 Support system for inner shaft of vehicle power train
USD749994S1 (en) * 2014-06-10 2016-02-23 TriMas Corporation Pty Ltd. Hitch pin
JP1555641S (en) * 2015-08-03 2016-08-08
USD823735S1 (en) * 2016-07-14 2018-07-24 Aircraft Gear Corporation Constant velocity joint

Also Published As

Publication number Publication date
USD847036S1 (en) 2019-04-30

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