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:
Nov. 20, 2018

Filed:

May. 12, 2015
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Oliver Seack, Hamburg, DE;

Tamas Havar, Bruckmuehl, DE;

Mirko Missbach, Bremen, DE;

Thomas Franke, Bremen, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 3/26 (2006.01); B64C 3/18 (2006.01); B32B 37/12 (2006.01); B64C 9/02 (2006.01);
U.S. Cl.
CPC ...
B64C 3/26 (2013.01); B32B 37/12 (2013.01); B64C 3/185 (2013.01); B64C 9/02 (2013.01); B32B 2305/72 (2013.01); B32B 2605/18 (2013.01); Y02T 50/44 (2013.01); Y10T 156/10 (2015.01);
Abstract

A flow body for an aircraft with a leading edge and a trailing edge includes a first spar, a second spar, and an external skin that spans from the leading edge to the trailing edge and on both sides rests on the spars. At least one of the first spar and the second spar includes a web and two spaced-apart flanges that enclose the web, on which flanges the skin that spans the respective spar is arranged. At least one of the first spar and the second spar includes at least one load introduction fin that forms an integral component with the web and extends outwards by way of one of the flanges and the skin that rests on the spars.


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