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:
Nov. 26, 2024

Filed:

May. 22, 2020
Applicant:

Moog Inc., East Aurora, NY (US);

Inventor:

Christopher A. Moore, Yorba Linda, CA (US);

Assignee:

Moog Inc., East Aurora, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/32 (2006.01); B29D 99/00 (2010.01); F16C 3/02 (2006.01);
U.S. Cl.
CPC ...
B64C 13/32 (2013.01); B29D 99/0025 (2013.01); F16C 3/023 (2013.01); F16C 2208/02 (2013.01); F16C 2226/40 (2013.01); F16C 2226/62 (2013.01); F16C 2229/00 (2013.01); F16C 2326/43 (2013.01);
Abstract

Presented are a method and apparatus for an aircraft flight surface actuation system including a motor having an output shaft. A gearbox is coupled with the output shaft, whereby a first driving force output via the motor is converted to a second driving force. A torque shaft assembly is driveably coupled with the gearbox. The torque shaft assembly includes a first tube, a second tube located at least partially through the first tube and located coaxial therewith, wherein the first tube comprises an axial preload operable to mitigate lateral deflection, and wherein the first tube comprises a torsional preload operable to mitigate torsional deflection. In addition, the aircraft flight surface actuation system includes an eccentric cam mechanism driveably coupled with the torque shaft assembly, and a flight surface coupled with the eccentric cam mechanism.


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