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:
Mar. 15, 2022

Filed:

Dec. 27, 2019
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventors:

Gaetan Dussart, Bristol, GB;

Ciaran O'Rourke, Bristol, GB;

Thomas Wilson, Bristol, GB;

Mudassir Lone, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/38 (2006.01); B64C 3/42 (2006.01); B64C 3/54 (2006.01); B64C 3/56 (2006.01); B64C 23/06 (2006.01);
U.S. Cl.
CPC ...
B64C 13/38 (2013.01); B64C 3/42 (2013.01); B64C 3/546 (2013.01); B64C 3/56 (2013.01); B64C 23/072 (2017.05);
Abstract

An actuator assembly for moving an aircraft wing tip device is disclosed. The wing tip device is rotatable about a hinge axis relative to a fixed wing of the aircraft. The hinge axis is orientated non-parallel to a line-of-flight direction of the aircraft. The actuator assembly includes a primary shaft having an axis of rotation orientated substantially parallel to the line-of-flight direction, a motor to cause rotation of the primary shaft, and a secondary shaft orientated substantially parallel to the hinge axis. The secondary shaft is couplable to the primary shaft and is arranged to rotate the wing tip device in response to the rotation of the primary shaft.


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