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. 14, 2021

Filed:

Dec. 05, 2018
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventors:

Francesco Gambioli, Bristol, GB;

Henry Edwards, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F16F 15/00 (2006.01); B64C 13/16 (2006.01); B64C 17/00 (2006.01); B64C 17/04 (2006.01); B64C 21/00 (2006.01); G05D 1/00 (2006.01); B64C 5/08 (2006.01); B64C 5/10 (2006.01); B64C 13/00 (2006.01); F15D 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 21/00 (2013.01); B64C 5/08 (2013.01); B64C 5/10 (2013.01); B64C 13/00 (2013.01); B64C 13/16 (2013.01); B64C 17/00 (2013.01); B64C 17/04 (2013.01); F15D 1/007 (2013.01); F16F 15/00 (2013.01); G05D 1/0066 (2013.01); B64C 2230/00 (2013.01);
Abstract

An aircraft is disclosed having a structure at least part of which is capable of generating aerodynamic lift. A body having a mass is movably mounted to a portion of the structure by an active support. The active support includes an actuator to move the body relative to the portion of the structure, and a controller for controlling movement of the actuator in response to a dynamic input. The active support provides a range of movement for the body in at least one degree of freedom. The actuator moves the body across the entire range of movement in that one degree of freedom in a time period of less than 3 seconds. The actuator moves the body sufficiently rapidly to generate an inertial force that is equal to or greater than any aerodynamic force generated by the body during that movement of the body. The active support may be used to reduce loads on the aircraft structure.


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