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:
Sep. 01, 2015

Filed:

Apr. 14, 2012
Applicants:

Brian R Spence, Solvang, CA (US);

Steven F White, Ventura, CA (US);

Peter Sorenson, Santa Barbara, CA (US);

Inventors:

Brian R Spence, Solvang, CA (US);

Steven F White, Ventura, CA (US);

Peter Sorenson, Santa Barbara, CA (US);

Assignee:
Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/22 (2006.01); B64G 1/44 (2006.01);
U.S. Cl.
CPC ...
B64G 1/222 (2013.01); B64G 1/443 (2013.01); B64G 1/44 (2013.01);
Abstract

A large area, deployable flexible blanket photovoltaic solar array architecture for high power applications is disclosed. The structure is a modularized and scalable solar array system that provides high power level scalability. The structure is comprised of repeating, similar modular deployable roll-out solar array wings mounted in an opposing manner and along the length of a rigid, strong and efficiently packaged deployable backbone structure. The deployable roll-out solar array building block modular 'winglet' elements can be comprised of either a rolled or z-folded flexible photovoltaic blanket configuration, and their structural deployment is motivated by the elastic strain energy of longitudinal roll-out booms. The backbone structure is comprised of a stiff deployable beam structure articulated that is deployed perpendicular with respect to the spacecraft sidewall and latched out. Deployment of the 'winglets' can be conducted once the articulated backbone structure has been deployed, is latched, and forms a rigid beam.


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