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:
Oct. 15, 2019

Filed:

Aug. 02, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Jian Dong, Irvine, CA (US);

Naveed Moayyed Hussain, Palos Verdes Penninsula, CA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/54 (2006.01); B64G 1/56 (2006.01); E04B 1/92 (2006.01); E04C 2/284 (2006.01); E04C 2/34 (2006.01); E04C 2/36 (2006.01); E04C 2/52 (2006.01); B32B 5/02 (2006.01); B32B 7/12 (2006.01); B32B 9/00 (2006.01); B32B 15/02 (2006.01); B32B 27/06 (2006.01); B32B 27/12 (2006.01); B32B 27/32 (2006.01); B32B 1/08 (2006.01); B32B 3/08 (2006.01); B32B 3/12 (2006.01); B64C 1/06 (2006.01); B64C 1/12 (2006.01); B64C 1/40 (2006.01);
U.S. Cl.
CPC ...
B64G 1/54 (2013.01); B32B 1/08 (2013.01); B32B 3/08 (2013.01); B32B 3/12 (2013.01); B32B 5/02 (2013.01); B32B 7/12 (2013.01); B32B 9/007 (2013.01); B32B 15/02 (2013.01); B32B 27/065 (2013.01); B32B 27/12 (2013.01); B32B 27/32 (2013.01); B64C 1/066 (2013.01); B64C 1/12 (2013.01); B64C 1/406 (2013.01); B64G 1/56 (2013.01); E04B 1/92 (2013.01); E04C 2/284 (2013.01); E04C 2/3405 (2013.01); E04C 2/365 (2013.01); E04C 2/521 (2013.01); E04C 2/526 (2013.01); B32B 2250/05 (2013.01); B32B 2250/40 (2013.01); B32B 2262/0253 (2013.01); B32B 2262/0269 (2013.01); B32B 2262/105 (2013.01); B32B 2262/106 (2013.01); B32B 2262/14 (2013.01); B32B 2266/0278 (2013.01); B32B 2307/202 (2013.01); B32B 2307/212 (2013.01); B32B 2307/304 (2013.01); B32B 2307/558 (2013.01); B32B 2307/56 (2013.01); B32B 2307/71 (2013.01); B32B 2307/7246 (2013.01); B32B 2571/02 (2013.01); B32B 2605/00 (2013.01); B32B 2605/18 (2013.01); B64D 2221/00 (2013.01); E04B 2001/925 (2013.01); E04C 2002/345 (2013.01);
Abstract

A multi-functional composite structure has a modular design that can be altered depending on an extreme environment in which the structure will be exposed such as hazardous radiation, micro-meteoroid and orbital debris impacts, extreme temperature changes, etc. The material combinations employed in the multi-functional composite structure provide a supporting structure with low weight and maximum protection from radiation, debris impacts and temperature variations.


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