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:
Aug. 25, 2015

Filed:

May. 09, 2013
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventor:

Walter Oefner, Otterfing, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B32B 5/12 (2006.01); B32B 1/04 (2006.01); B29D 99/00 (2010.01); B64C 1/06 (2006.01); B29C 69/00 (2006.01); B29L 31/30 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B32B 1/04 (2013.01); B29C 69/001 (2013.01); B29D 99/0014 (2013.01); B64C 1/064 (2013.01); B29L 2031/3076 (2013.01); B29L 2031/3088 (2013.01); B64C 2001/0072 (2013.01); Y02T 50/433 (2013.01); Y10T 428/2419 (2015.01);
Abstract

A skin-stiffener transition assembly () with a skin () and two L-shaped fiber-reinforced fabric preforms () for a flange and a composite gusset filler () integrated between said skin () and said two L-shaped fiber-reinforced fabric preforms (). The skin () comprises two separate skin layers () and the flange comprises a flange layer (), each of said skin layers () and said flange layer () being provided with cut outs () along one side. Said skin layers () and the flange layer () are attached to the composite gusset filler () with at least one of its cut-outs () to one side of the essentially polygonal cross section of the composite gusset filler () and with at least one of its adjacent cut-outs () to another side of the essentially polygonal cross section of the composite gusset filler (). The present invention relates as well to a method of manufacture of said skin-stiffener transition assembly () and to applications of said skin-stiffener transition assembly ().


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