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SPACE PATENTS BY
Aerospace Assignees
Aerospace Inventors
Time Lines

Flexible self-erecting substructures for sensor networks

Invented by: Jayson T. Durham
Lakeside, CA

Joshua Blanchi
San Diego, CA

Originally Assigned to: The United States of America as represented by Secretary of the Navy
Washington, DC
[Now assigned to . . .]

Issued:2012-06-19
Filed:2008-07-02
Application No:12167075
Examined by:Swiatek; Rob

A composite flexible and aerodynamic load bearing wing structure suitable for compact unmanned vehicles, is described. Flexible printed circuitry and micro fuel cells can be incorporated as, or part of, the flexible aerodynamic structure. Accordingly, the overall system configuration can be optimized with respect to weight, space and size requirements. The flexible aerodynamic structure for the unmanned vehicle may be configured with a flexible dielectric substrate having an electrical contact on at least one surface of the substrate, and a flexible printed circuit disposed upon the substrate. The printed circuit can flex with the substrate and the substrate, with the printed circuit, to form a load lifting aerodynamic wing configuration when unfolded from a folded position.

[pdf] U.S. Pat. No. 8,201,773

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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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