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. 11, 2016

Filed:

Feb. 25, 2014
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Peter Babilo, Mission Viejo, CA (US);

Randall Jay Moss, Thousand Oaks, CA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C09J 11/06 (2006.01); B32B 37/12 (2006.01); C08K 3/38 (2006.01); C09J 163/00 (2006.01); H05K 1/02 (2006.01); H05K 3/30 (2006.01); B32B 37/18 (2006.01); C09K 5/14 (2006.01);
U.S. Cl.
CPC ...
C09J 11/06 (2013.01); B32B 37/1284 (2013.01); B32B 37/18 (2013.01); C08K 3/38 (2013.01); C09J 163/00 (2013.01); C09K 5/14 (2013.01); H05K 1/0203 (2013.01); H05K 3/305 (2013.01); B32B 2037/1253 (2013.01); B32B 2457/00 (2013.01); H05K 2201/0133 (2013.01); H05K 2201/0209 (2013.01); H05K 2201/0239 (2013.01); H05K 2203/12 (2013.01); Y02P 70/613 (2015.11);
Abstract

Provided are methods of forming thermally conductive flexible bonds for use in electronic boards of unmanned spacecrafts and other types of aircraft. Also provided are methods of preparing adhesive materials to form these bonds including methods of preparing treated filler particles. In some aspects, an adhesive material includes filler particles having organofunctional groups, such as boron nitride particles treated in silane. These particles may be combined with a urethane modified epoxy to form the adhesive material. The weight ratio of the particles in the adhesive material may be about 40-60%. The adhesive material may be thermally cured using a temperature of less than 110° C. to prevent damage to bonded electronic components. The cured adhesive may have a thermal conductivity of at least about 2 W/m K measured in vacuum and may have a glass transition temperature if less than −40° C.


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