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:
Apr. 11, 2017

Filed:

Mar. 12, 2013
Applicants:

Brian R Spence, Solvang, CA (US);

Stephen F White, Ventura, CA (US);

Mark V Douglas, Santa Barbara, CA (US);

Kevin B Schmid, Santa Barbara, CA (US);

Ron S Takeda, Santa Barbara, CA (US);

Inventors:

Brian R Spence, Solvang, CA (US);

Stephen F White, Ventura, CA (US);

Mark V Douglas, Santa Barbara, CA (US);

Kevin B Schmid, Santa Barbara, CA (US);

Ron S Takeda, Santa Barbara, CA (US);

Assignee:
Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
H01L 31/044 (2014.01); H02S 30/20 (2014.01); H01L 31/041 (2014.01);
U.S. Cl.
CPC ...
H01L 31/045 (2013.01); H01L 31/041 (2014.12); Y02E 10/50 (2013.01);
Abstract

A modular, lightweight, high-survivable, photovoltaic flexible blanket assembly for a space solar array is disclosed. The modular blanket is an accordion foldable or rollable flexible photovoltaic solar panel blanket assembly comprising a plurality of common photovoltaic modules spaced in an orthogonal pattern. Each module is mechanically attached with multiple low profile fasteners on their backside to an open weave mesh tensioned backplane structure. The backplane forms a tensioned dimensionally stable planar surface in the deployed configuration onto which the modules are suspended. Each module is common and comprised of a rectangular substrate that includes solar cell assemblies, circuitry, exposed electrical contacts for integration of blanket-level harnessing, and frontside and rearside shielding and coatings as required for the mission application. The blanket assembly may be dispersed with an open pattern of compliant and formable material on the backside to provide insulation against the vigorous vibration of the launch environment.


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