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SPACE PATENTS BY
Aerospace Assignees
Aerospace Inventors
Time Lines

Structural component with rib and cross member element

Invented by: Philipp Westphal
Fuhlendorf, DE

Wolf-Dietrich Dolzinski
Ganderkesee, DE

Thorsten Roming
Himmelpforten, DE

Thorsten Schroeer
Buxtehude, DE

Dieter Kohlgrueber
Stuttgart, DE

Marius Luetzenburger
Boeblingen, DE Applicant: Name City State Country Type Westphal

Originally Assigned to: Airbus Operations GmbH
Hamburg, DE DLR-Deutsches Zentrum fuer Luft- und Raumfahrt e.V.
[Now assigned to . . .]

Issued:2013-05-14
Filed:2009-12-15
Application No:12638423
Examined by:Dinh; Tien

The present invention provides a fuselage structure for an aircraft or spacecraft with an outer skin. The fuselage structure comprises a rib element for stiffening the outer skin and ad cross member element. Here the rib element is bent in the shape of an arc to correspond to an inner contour of the outer skin. The cross member element connects two arc sections of the rib element transversely to each other. The cross member element has a higher strength than the rib element. From another point of view the invention provides an aircraft with such a fuselage structure.

[pdf] U.S. Pat. No. 8,439,307

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This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.

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