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US Patent 9120583 Space solar array architecture for ultra-high power applications

Patent 9120583 was granted and assigned to Deployable Space Systems, Inc. on September, 2015 by the United States Patent and Trademark Office.

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Patent
Patent

Patent attributes

Current Assignee
‌
Deployable Space Systems, Inc.
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
9120583
Date of Patent
September 1, 2015
Patent Application Number
13447166
Date Filed
April 14, 2012
Patent Citations Received
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US Patent 12091198 Deployment device
1
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US Patent 12003210 Solar array attachment
2
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US Patent 12021162 Ultralight photovoltaic power generation tiles
3
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US Patent 12028016 Z-fold flexible blanket solar array
4
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US Patent 11670955 Integrated power module devices, systems, and methods
5
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US Patent 11772826 Actively controlled spacecraft deployment mechanism
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US Patent 11863120 Solar arrays and related vehicles and assemblies
6
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US Patent 11912440 Partially flexible solar array structure
7
...
Patent Primary Examiner
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Philip J Bonzell
Patent 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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