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.

Patent No.:

US 8740150 B1

PDF
Full Text
Expired
Date of Patent:
Jun. 03, 2014

Filed:

Aug. 18, 2009
Applicants:

Frank Werth, Stuhr, DE;

Andreas Poppe, Reessum, DE;

Hermann Benthien, Sottrum, DE;

Bernd Beschorner, Schwarme, DE;

Inventors:

Frank Werth, Stuhr, DE;

Andreas Poppe, Reessum, DE;

Hermann Benthien, Sottrum, DE;

Bernd Beschorner, Schwarme, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 1/26 (2006.01);
U.S. Cl.
CPC ...
Abstract

An aerofoil connection on a fuselage airframe comprising a plurality of double-jointed coupling members. In each case at least two z-coupling members extending substantially parallel to a vertical axis of the aircraft and in each case at least two xz-coupling members are arranged in the region of two longitudinal edges of a fuselage airframe recess wherein the xz-coupling members are configured in each case for a first maximum of a load in the event of a crash and of a load in normal flight operation parallel to a longitudinal axis of the aircraft, and for a second maximum of a load in the event of a crash and of a load in normal flight operation parallel to the vertical axis. The xz-coupling members are capable of absorbing force components parallel to the x-axis as well as force components which arise parallel to the z-axis.


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