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:
Mar. 24, 2020

Filed:

Jun. 21, 2017
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventors:

Robert Ian Thompson, Bristol, GB;

Geoffrey Richard Williams, Bristol, GB;

Nicholas Livings, Bristol, GB;

Kevin Nicholls, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/56 (2006.01); B64C 3/40 (2006.01); B64C 3/58 (2006.01);
U.S. Cl.
CPC ...
B64C 3/56 (2013.01); B64C 3/40 (2013.01); B64C 3/58 (2013.01); Y02T 50/14 (2013.01);
Abstract

A method of configuring a wing tip device () on an aircraft (), including: undertaking ground-based operations at an airport with the wing tip device () in a ground configuration, in which the span of the aircraft is within an airport compatibility limit, moving the wing tip device () to a take-off configuration in which the wing tip device () is moved away from the ground configuration such that the span of the aircraft is increased and such that the wing tip device () has a first lift coefficient; taking-off with the wing tip device () in the take-off configuration; moving the wing tip device from the take-off configuration to a flight configuration, in which the wing tip device has a second lift coefficient, the second lift coefficient being lower than the first lift coefficient. The lift coefficient may be changed by adjusting the sweep of the wing tip device ().


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