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:
Sep. 27, 2022

Filed:

Jun. 28, 2018
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Kevin M. Wittke, Milford, CT (US);

Bertrand J. Howard, Shelton, CT (US);

Assignee:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/59 (2006.01); B64C 11/06 (2006.01); B64C 27/78 (2006.01); F16C 19/54 (2006.01); F16C 19/52 (2006.01); F16C 39/02 (2006.01);
U.S. Cl.
CPC ...
B64C 27/59 (2013.01); B64C 11/06 (2013.01); B64C 27/78 (2013.01); F16C 19/52 (2013.01); F16C 19/54 (2013.01); F16C 39/02 (2013.01); F16C 2326/43 (2013.01);
Abstract

An aircraft rotor system includes a rotating pitch change shaft which rotates about an axis, a translating element disposed within the rotating pitch change shaft and movable along the axis and a pitch change bearing assembly which transfers movement of the translating element to the pitch change shaft. The pitch change bearing assembly includes a primary bearing and a secondary bearing coupled to the rotating pitch change shaft via the translating element when the primary bearing is in a first mode. A thrust shoulder is coupled to the translating element. The thrust shoulder is movable into engagement with the secondary bearing in response to failure of the primary bearing such that in a second mode, movement of the translating element is primarily transferred to the pitch change shaft via the secondary bearing.


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