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. 10, 2019

Filed:

Apr. 02, 2015
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventors:

Christopher Lynas, Bristol, GB;

Robert Thompson, Bristol, GB;

Llifon Williams, Bristol, GB;

John Hobday, Bristol, GB;

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

An aircraft wing () has a wing tip device () joined thereto. The root () of the wing tip device () is joined to the tip of the wing () at a first connection (). An external strut () extends between the wing () and the wing tip device (), the strut () being joined to the wing () at a second connection (). The second connection () is inboard of the first connection, such that loadings on the wing tip device () generated during use, are transferred, via the strut (), to a location on the wing () that is inboard of where the root () of the wing tip device () is joined to the tip of the wing.


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