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:
Jul. 30, 2019

Filed:

Jul. 19, 2016
Applicants:

Airbus Defence and Space Gmbh, Taufkirchen, DE;

Airbus Group Limited, London, GB;

Inventors:

Andreas Wildschek, Riemerling, DE;

Stefan Storm, Unterschleißhein, DE;

Stephen Rolston, Bristol, GB;

Martin Herring, Bristol, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/38 (2006.01); B64C 3/42 (2006.01); B64C 3/56 (2006.01); B64C 13/40 (2006.01); B64C 39/00 (2006.01); B64C 39/10 (2006.01);
U.S. Cl.
CPC ...
B64C 3/38 (2013.01); B64C 3/42 (2013.01); B64C 3/56 (2013.01); B64C 13/40 (2013.01); B64C 39/00 (2013.01); B64C 2039/105 (2013.01);
Abstract

A coupling device for supporting a first wing section against a second wing section of an aircraft, and configured for passive flight load alleviation includes a housing including a chamber including a first portion and a second portion and filled with a fluid, a piston device movably arranged in the chamber and separating the first portion from the second portion in a fluid tight manner, a first fluid pathway connecting the first portion to the second portion, a first pressure relief valve arranged in the first fluid pathway and blocking the first fluid pathway, if the pressure in the second portion is smaller than a first relief pressure and opening the first fluid pathway, if the pressure in the second portion is greater than the first relief pressure. In addition, the coupling device can be used to actuate the second wing section against the first wing section.


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