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. 03, 2019

Filed:

Jun. 08, 2016
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventors:

Kaspar Von-Wilmowsky, Donauworth, DE;

Christian Reichensperger, Asbach Baeumenheim, DE;

Andreas Rack, Burghausen, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/06 (2006.01); B64C 1/00 (2006.01); B64C 25/10 (2006.01); B64C 25/20 (2006.01); B64C 25/34 (2006.01); B64C 27/00 (2006.01); B64C 27/04 (2006.01); B64C 25/32 (2006.01); F16B 5/01 (2006.01); F16B 9/00 (2006.01); F16B 11/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/069 (2013.01); B64C 1/00 (2013.01); B64C 1/064 (2013.01); B64C 25/10 (2013.01); B64C 25/20 (2013.01); B64C 25/34 (2013.01); B64C 27/00 (2013.01); B64C 27/04 (2013.01); B64C 2001/0054 (2013.01); B64C 2025/325 (2013.01); F16B 5/01 (2013.01); F16B 9/00 (2013.01); F16B 11/006 (2013.01);
Abstract

An aircraft structural component that is adapted for absorbing and transmitting forces in an aircraft, the aircraft structural component comprising at least one panel element and at least one reinforcing structure. The at least one reinforcing structure is rigidly attached to the at least one panel element such that at least one cavity is defined between the at least one panel element and the at least one reinforcing structure, the at least one cavity being adapted for distributing forces that are absorbed by the aircraft structural component in operation.


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