The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jan. 24, 2023

Filed:

Jun. 04, 2020
Applicant:

Schaublin SA, Delemont, CH;

Inventors:

David Coombe, Somerset, GB;

Maxime Merg, Manspach, FR;

Assignee:

Schaublin SA, Delémont, CH;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16C 17/10 (2006.01); F16C 33/24 (2006.01); F16C 41/00 (2006.01);
U.S. Cl.
CPC ...
F16C 17/107 (2013.01); F16C 33/24 (2013.01); F16C 41/002 (2013.01); F16C 2326/43 (2013.01);
Abstract

A bushing for aircraft landing gear includes a cylindrical wall having an interior surface defining a bore extending between a first and second axial end thereof and a cylindrical recess extending into the interior surface. The bushing includes a cylindrical self-lubricating liner which is substantially flush with the interior surface is disposed in the recess. The cylindrical wall includes a flange that has an annular recess that receives an annular self-lubricating liner that has a planar axial bearing surface. The planar axial bearing surface is coplanar with an inboard axial surface of the flange. The bushing has an electrically conductive path that conducts electrical current and that extends around the cylindrical self-lubricating liner and the annular self-lubricating liner and through the cylindrical wall and the flange.


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