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:
Oct. 27, 2015

Filed:

Jul. 06, 2012
Applicants:

Simon Topping, Bristol, GB;

Christopher Payne, Clevedon, GB;

Llifon Williams, Bristol, GB;

Martin Mayneord, Bristol, GB;

David Belfourd, Bristol, GB;

Xavier Hue, Bremen, DE;

Inventors:

Simon Topping, Bristol, GB;

Christopher Payne, Clevedon, GB;

Llifon Williams, Bristol, GB;

Martin Mayneord, Bristol, GB;

David Belfourd, Bristol, GB;

Xavier Hue, Bremen, DE;

Assignees:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/34 (2006.01); B64C 9/02 (2006.01); B64C 9/22 (2006.01);
U.S. Cl.
CPC ...
B64C 13/34 (2013.01); B64C 9/22 (2013.01); B64C 9/02 (2013.01);
Abstract

An aircraft wing has a main wing element with a spar and a leading edge rib supported by the spar, a high lift device movably mounted to the main wing element, and an actuation mechanism with a drive shaft and a gear train. The gear train has a drive cog carried by the drive shaft, an actuator cog coupled to the high lift device, and one or more intermediate cogs mounted to the rib and coupled in series with the drive cog and the actuator cog so as to transmit torque from the drive cog to the actuator cog which moves the high lift device between a retracted position and an extended position in which the high lift device increases the camber of the wing. Sizes of the cogs in the gear train are selected so that the drive shaft rotates at a higher rate than the high lift device.


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