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:
Dec. 21, 2021

Filed:

Sep. 29, 2016
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventors:

Thomas Wilson, Bristol, GB;

Martin Herring, Bristol, GB;

John Pattinson, Bristol, GB;

Jonathan Cooper, Bristol, GB;

Andrea Castrichini, Bristol, GB;

Rafic Ajaj, Southampton, GB;

Hitul Dhoru, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/38 (2006.01); B64C 3/54 (2006.01); B64C 23/06 (2006.01); B64C 3/56 (2006.01); B64C 13/16 (2006.01);
U.S. Cl.
CPC ...
B64C 3/546 (2013.01); B64C 3/56 (2013.01); B64C 13/16 (2013.01); B64C 23/065 (2013.01); B64C 23/072 (2017.05); Y02T 50/10 (2013.01);
Abstract

An aircraft is disclosed having a wing, the wing having a fixed wing with a wing tip device moveably mounted about a hinge at the tip thereof. The wing tip device is operable between a flight configuration, and a load alleviating configuration for load alleviation during flight. The aircraft includes a restraining assembly operable between a restraining mode in which the wing tip device is held in the flight configuration using a restraining force such as by a brake, and a releasing mode in which the restraining force on the wing tip device is released, such that the wing tip device may adopt the load alleviating configuration.


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