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. 10, 2019

Filed:

Jul. 17, 2017
Applicant:

Raytheon Company, Waltham, MA (US);

Inventors:

Tracy M. Fiedler, El Segundo, CA (US);

Kurt S. Ketola, El Segundo, CA (US);

Andrew Truxel, Hermosa Beach, CA (US);

Assignee:

Raytheon Company, Waltham, MA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F16L 59/02 (2006.01); B64G 1/58 (2006.01); B33Y 80/00 (2015.01); B64G 1/50 (2006.01); F16L 59/08 (2006.01); F16L 59/12 (2006.01); B33Y 10/00 (2015.01); B22F 3/105 (2006.01); B22F 7/06 (2006.01); F16L 59/16 (2006.01);
U.S. Cl.
CPC ...
F16L 59/029 (2013.01); B33Y 80/00 (2014.12); B64G 1/50 (2013.01); B64G 1/58 (2013.01); B22F 3/1055 (2013.01); B22F 7/06 (2013.01); B33Y 10/00 (2014.12); F16L 59/08 (2013.01); F16L 59/12 (2013.01); F16L 59/161 (2013.01);
Abstract

A three-dimensional multi-shell insulation configured to conform to the shape of a spacecraft component to be insulated. The insulation may have a plurality of nested shell layers that are displaceable relative to each other for providing natural separation between the shell layers when the insulation is used in low-pressure and/or low-gravity space-related applications. To establish the spacing between shell layers, an edge clamp may be operatively coupled to an edge portion on at least one side of each shell layer. The shell layers may have sufficient flexibility and/or may be sufficiently displaceable relative to each other to allow the insulation to be installed or removed from the spacecraft component. One or more restraints may be provided in the space between the shell layers for restricting the relative lateral and/or transverse movement between shell layers for preventing contact. Additive manufacturing may be employed to fabricate the insulation and integrate features.


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