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:
Feb. 21, 2017

Filed:

Nov. 26, 2012
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Werner Dyckrup, Visbek, DE;

Wilfried Ellmers, Achim, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/28 (2006.01); B64C 9/02 (2006.01); B64C 9/16 (2006.01); B64C 13/42 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
B64C 13/28 (2013.01); B64C 9/02 (2013.01); B64C 9/16 (2013.01); B64C 13/42 (2013.01); B64D 2045/001 (2013.01); Y02T 50/44 (2013.01);
Abstract

The invention concerns a device for a adjustable flap adjustably mounted on a main wing surface of an aeroplane wing, in particular, a landing flap, with at least one adjustment unit for purposes of adjustment of the adjustable flap, which has an actuator arranged, or that can be arranged, on the main wing surface, and has a kinematic adjustment mechanism running between the actuator and the adjustable flap, wherein the adjustable flap is mechanically coupled with the actuator via the kinematic adjustment mechanism. At least one damping unit for purposes of damping a dynamic loading effected by the adjustable flap on the adjustment unit, which can occur as a result of a critical malfunction event occurring in the region of the adjustable flap, is arranged, or can be arranged, between the main wing surface and the adjustable flap.


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