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:
Jul. 21, 2026

Filed:

Oct. 26, 2023
Applicant:

Cornerstone Research Group, Inc., Miamisburg, OH (US);

Inventors:

Gray E. Fowler, Allen, TX (US);

James M. Davidson, Miamisburg, OH (US);

Garrett U. Yoder, Springboro, OH (US);

Assignee:

Cornerstone Research Group, Inc., Miamisburg, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C04B 35/83 (2006.01); B29C 70/00 (2006.01); B29C 70/02 (2006.01); B29C 70/36 (2006.01); C04B 35/71 (2006.01); B29K 77/00 (2006.01); B29K 105/08 (2006.01); B29K 301/00 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
C04B 35/83 (2013.01); B29C 70/003 (2021.05); B29C 70/021 (2013.01); B29C 70/36 (2013.01); C04B 35/71 (2013.01); B29C 2791/006 (2013.01); B29K 2077/00 (2013.01); B29K 2105/0845 (2013.01); B29K 2301/00 (2013.01); B29L 2031/3005 (2013.01); Y10T 428/30 (2015.01);
Abstract

Methods of making a carbon-carbon composite structure with internal microchannels include (i) assembling a dry carbon fiber composite preform with a sacrificial template woven or placed within to form a primary assembly; (ii) placing the primary assembly under a sealed enclosure; (iii) applying a vacuum to the sealed enclosure to evacuate air from the dry carbon fiber composite preform; (iv) infusing a polymer resin into the dry carbon fiber composite preform to generate a resin infused preform; (v) heating the resin infused preform under vacuum to cure the polymer resin in the resin infused preform to form a cured composite; (vi) demolding the cured composite; and (vii) heating the cured composite to an elevated temperature of at least 800° C. under a flow of an inert gas to decompose the sacrificial template to form the internal microchannels and carbonize the cured composite to form the carbon-carbon composite structure.


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