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.

Patent No.:

US 9733027 B1

PDF
Full Text
Expired
Date of Patent:
Aug. 15, 2017

Filed:

Jan. 15, 2014
Applicant:

Minus K. Technology, Inc., Inglewood, CA (US);

Inventors:

David L. Platus, Santa Monica, CA (US);

Erik K Runge, Buellton, CA (US);

Assignee:

Other;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F28F 9/26 (2006.01); F16F 15/04 (2006.01); F28F 13/00 (2006.01); F25D 19/00 (2006.01); B64G 1/50 (2006.01); F28D 21/00 (2006.01); B64G 1/22 (2006.01);
U.S. Cl.
CPC ...
F28F 9/26 (2013.01); B64G 1/50 (2013.01); F16F 15/04 (2013.01); F25D 19/006 (2013.01); F28F 13/00 (2013.01); B64G 2001/228 (2013.01); F28D 2021/0021 (2013.01); F28F 2013/006 (2013.01); F28F 2255/02 (2013.01); F28F 2265/26 (2013.01); F28F 2265/30 (2013.01);
Abstract

Negative-stiffness-producing mechanisms can be incorporated with structural devices that are used on spacecraft that provide thermal coupling between a vibrating source and a vibration-sensitive object. Negative-stiffness-producing mechanisms can be associated with a flexible conductive link (FCL) or 'thermal strap' or 'cold strap' to reduce the positive stiffness of the FCL. The negative-stiffness-producing mechanisms can be loaded so as to create negative stiffness that will reduce or negate the natural positive stiffness inherent with the FCL. The FCL will still be able to provide maximum thermal conductance while achieving low or near-zero stiffness to maximize structural decoupling.


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Platus, David. (2017). Thermal straps for spacecraft (U.S. Patent No. 9733027). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9733027

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