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:
Jun. 30, 2020

Filed:

Jul. 21, 2016
Applicant:

California Institute of Technology, Pasadena, CA (US);

Inventors:

Sergio Pellegrino, Pasadena, CA (US);

Harry A. Atwater, South Pasadena, CA (US);

Seyed Ali Hajimiri, La Canada, CA (US);

Manan Arya, Pasadena, CA (US);

Christophe Leclerc, Pasadena, CA (US);

Nicolas Lee, Pasadena, CA (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/42 (2006.01); H02J 50/20 (2016.01); H02J 3/38 (2006.01); H01L 31/042 (2014.01); H02S 10/40 (2014.01); H02S 30/20 (2014.01); B64G 1/10 (2006.01); B64G 1/22 (2006.01); B64G 1/44 (2006.01); B64G 1/66 (2006.01); B65B 63/04 (2006.01); B64G 1/36 (2006.01); B64G 1/28 (2006.01);
U.S. Cl.
CPC ...
B64G 1/428 (2013.01); B64G 1/1085 (2013.01); B64G 1/222 (2013.01); B64G 1/443 (2013.01); B64G 1/66 (2013.01); B65B 63/04 (2013.01); H01L 31/042 (2013.01); H02J 3/383 (2013.01); H02J 50/20 (2016.02); H02S 10/40 (2014.12); H02S 30/20 (2014.12); B64G 1/288 (2013.01); B64G 1/36 (2013.01); Y02E 10/563 (2013.01);
Abstract

A space-based solar power station, a power generating satellite module and/or a method for collecting solar radiation and transmitting power generated using electrical current produced therefrom, and/or compactible structures and deployment mechanisms used to form and deploy such satellite modules and power generation tiles associated therewith are provided. Each satellite module and/or power generation tile may be formed of a compactable structure and deployment mechanism capable of reducing the payload area required to deliver the satellite module to an orbital formation within the space-based solar power station and reliably deploy it once in orbit.


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