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:
Sep. 01, 2020

Filed:

Jul. 11, 2019
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventors:

Timothy Axford, Bristol, GB;

Tony Fong, Bristol, GB;

Stuart Alexander, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 23/06 (2006.01); B64C 3/18 (2006.01); B64C 3/54 (2006.01); B64C 3/56 (2006.01);
U.S. Cl.
CPC ...
B64C 23/072 (2017.05); B64C 3/185 (2013.01); B64C 3/546 (2013.01); B64C 3/56 (2013.01); B64C 3/54 (2013.01); Y02T 50/14 (2013.01); Y02T 50/164 (2013.01);
Abstract

An aircraft including a wing and a wing tip device is disclosed. The wing tip device is moveable between a flight configuration for use during flight and a ground configuration for use during ground-based operations. In the ground configuration the wing tip device is folded inwardly from the flight configuration such that the span of the aircraft is reduced. The wing tip device is connected to the wing along a hinge axis by spar beams of the wing tip device, one of the beams being mounted for pivoting about a fixed axis and the other beam being mounted on a spherical bearing to provide greater freedom of movement. Various actuator arrangements may be provided to pivot the wing tip device.


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