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. 06, 2020

Filed:

Jul. 09, 2018
Applicant:

Advanced Ceramic Fibers, Llc, Idaho Falls, ID (US);

Inventor:

John E. Garnier, Idaho Falls, ID (US);

Assignee:

ADVANCED CERAMIC FIBERS, LLC., Idaho Falls, ID (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
C04B 35/80 (2006.01); C04B 35/573 (2006.01); C04B 35/591 (2006.01); C04B 37/00 (2006.01); C04B 35/628 (2006.01); C04B 35/571 (2006.01); C04B 38/00 (2006.01); C04B 35/589 (2006.01); C04B 111/00 (2006.01);
U.S. Cl.
CPC ...
C04B 35/806 (2013.01); C04B 35/571 (2013.01); C04B 35/573 (2013.01); C04B 35/589 (2013.01); C04B 35/591 (2013.01); C04B 35/62863 (2013.01); C04B 35/62865 (2013.01); C04B 35/62868 (2013.01); C04B 35/62897 (2013.01); C04B 37/005 (2013.01); C04B 38/00 (2013.01); C04B 2111/0081 (2013.01); C04B 2111/00362 (2013.01); C04B 2111/00431 (2013.01); C04B 2111/00793 (2013.01); C04B 2111/00801 (2013.01); C04B 2111/00862 (2013.01); C04B 2235/383 (2013.01); C04B 2235/386 (2013.01); C04B 2235/3865 (2013.01); C04B 2235/3882 (2013.01); C04B 2235/524 (2013.01); C04B 2235/526 (2013.01); C04B 2235/5244 (2013.01); C04B 2235/5248 (2013.01); C04B 2235/5264 (2013.01); C04B 2235/5292 (2013.01); C04B 2235/5296 (2013.01); C04B 2235/5436 (2013.01); C04B 2235/767 (2013.01); C04B 2235/80 (2013.01); C04B 2235/9607 (2013.01);
Abstract

Ceramic composite materials that are reinforced with carbide fibers can exhibit ultra-high temperature resistance. For example, such materials may exhibit very low creep at temperatures of up to 2700° F. (1480° C.). The present composites are specifically engineered to exhibit matched thermodynamically stable crystalline phases between the materials included within the composite. In other words, the reinforcing fibers, a debonding interface layer disposed over the reinforcing fibers, and the matrix material of the composite may all be of the same crystalline structural phase (all hexagonal), for increased compatibility and improved properties. Such composite materials may be used in numerous applications.


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