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. 13, 2022

Filed:

Feb. 14, 2019
Applicant:

Jalapeno Holdings, Llc, Bellbrook, OH (US);

Inventors:

Richard D. Hreha, Dayton, OH (US);

Kristopher K. Aber, Dayton, OH (US);

Joel P. Brubaker, Dayton, OH (US);

Kristin M. Cable, Dayton, OH (US);

Michael D. Rauscher, Beavercreek, OH (US);

Assignee:

Systima Technologies, Inc., Mukilteo, WA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
C04B 35/83 (2006.01); C04B 35/64 (2006.01); C08J 5/04 (2006.01); C08G 73/02 (2006.01); C08G 73/06 (2006.01); C08G 73/00 (2006.01);
U.S. Cl.
CPC ...
C04B 35/83 (2013.01); C04B 35/64 (2013.01); C08J 5/042 (2013.01); C04B 2235/422 (2013.01); C04B 2235/5248 (2013.01); C04B 2235/658 (2013.01); C04B 2235/6562 (2013.01); C04B 2235/6565 (2013.01); C04B 2235/6567 (2013.01);
Abstract

Methods of producing a carbon matrix composite are provided which include preparing a carbon matrix composite precursor comprising at least one carbon-based reinforcement material and a cured thermoset polymer matrix comprising a chemical composition in accordance with Formula I where n and m are integers, at least one of Ror Rcomprises an aromatic moiety, and X is selected from the group consisting of CH, NH, O, S, SO, and combinations thereof. The methods further include heating the carbon matrix composite precursor in air to a first processing temperature of between 300° C. and 500° C. to form a carbon matrix composite intermediate, and heating the carbon matrix composite intermediate in nitrogen to a second processing temperature of between 900° C. to 1650° C. and holding at the second processing temperature for at least 1 hour in an inert gas environment to form the carbon matrix composite.


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