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. 24, 2015

Filed:

Sep. 24, 2013
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Matthew A. Moser, Marysville, WA (US);

Michael R. Finn, Kirkland, WA (US);

Mark J. Gardner, Snohomish, WA (US);

Mark S. Good, Seattle, WA (US);

Sarah A. Jones, Mill Creek, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/50 (2006.01); B64C 13/34 (2006.01); B64C 9/14 (2006.01); B64C 13/26 (2006.01);
U.S. Cl.
CPC ...
B64C 13/34 (2013.01); B64C 3/50 (2013.01); B64C 9/14 (2013.01); B64C 13/26 (2013.01);
Abstract

A variable camber system for an aircraft may include a variable camber trim unit (VCTU) positioned between an inboard device and an outboard device. The inboard device and the outboard device may be mounted to at least one of a leading edge and a trailing edge of a wing. The VCTU may include a speed sum gearbox having an inboard shaft coupled to the inboard device and an outboard shaft coupled to the outboard device. The VCTU may additionally include a VCTU electric motor engaged to the speed sum gearbox. The VCTU electric motor may be selectively operable in conjunction with the speed sum gearbox to rotate the outboard shaft independent of the inboard shaft in a manner causing the outboard device to be actuated independent of the inboard device.


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