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.:
Date of Patent:
Jul. 02, 2024
Filed:
Jun. 27, 2022
Applicant:
Rtx Corporation, Farmington, CT (US);
Inventor:
David C. Jarmon, Hendersonville, NC (US);
Assignee:
RTX CORPORATION, Farmington, CT (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C04B 35/80 (2006.01); B28B 1/00 (2006.01); B28B 11/12 (2006.01); C04B 35/01 (2006.01); C04B 35/565 (2006.01); C04B 35/571 (2006.01); C04B 35/573 (2006.01); C04B 35/622 (2006.01); C04B 35/634 (2006.01); C04B 35/638 (2006.01); C04B 35/64 (2006.01); C04B 35/76 (2006.01); C04B 35/83 (2006.01); C04B 37/00 (2006.01); D03D 25/00 (2006.01); F01D 5/00 (2006.01); F01D 9/00 (2006.01); F01D 11/00 (2006.01); F01D 25/00 (2006.01); F01D 25/24 (2006.01); F01D 25/28 (2006.01); F01D 25/30 (2006.01); F02C 7/28 (2006.01); F02K 1/82 (2006.01); F23R 3/00 (2006.01); F23R 3/28 (2006.01); F23R 3/60 (2006.01);
U.S. Cl.
CPC ...
C04B 35/80 (2013.01); B28B 1/001 (2013.01); B28B 1/002 (2013.01); B28B 11/12 (2013.01); C04B 35/01 (2013.01); C04B 35/565 (2013.01); C04B 35/571 (2013.01); C04B 35/573 (2013.01); C04B 35/62227 (2013.01); C04B 35/634 (2013.01); C04B 35/638 (2013.01); C04B 35/64 (2013.01); C04B 35/76 (2013.01); C04B 35/83 (2013.01); C04B 37/001 (2013.01); D03D 25/005 (2013.01); F01D 5/00 (2013.01); F01D 9/00 (2013.01); F01D 11/00 (2013.01); F01D 25/00 (2013.01); F01D 25/005 (2013.01); F01D 25/243 (2013.01); F01D 25/246 (2013.01); F01D 25/28 (2013.01); F01D 25/30 (2013.01); F02C 7/28 (2013.01); F02K 1/822 (2013.01); F23R 3/002 (2013.01); F23R 3/007 (2013.01); F23R 3/283 (2013.01); F23R 3/60 (2013.01); C04B 2235/48 (2013.01); C04B 2235/5208 (2013.01); C04B 2235/5244 (2013.01); C04B 2235/5248 (2013.01); C04B 2235/5252 (2013.01); C04B 2235/5256 (2013.01); C04B 2235/612 (2013.01); C04B 2235/614 (2013.01); C04B 2235/616 (2013.01); C04B 2237/38 (2013.01); C04B 2237/385 (2013.01); C04B 2237/60 (2013.01); C04B 2237/61 (2013.01); C04B 2237/80 (2013.01); C04B 2237/84 (2013.01); F05D 2220/323 (2013.01); F05D 2230/10 (2013.01); F05D 2230/314 (2013.01); F05D 2240/91 (2013.01); F05D 2260/30 (2013.01); F05D 2260/31 (2013.01); F05D 2300/6033 (2013.01); F23M 2900/05004 (2013.01); Y02T 50/60 (2013.01);
Abstract
A gas turbine engine component includes a gas turbine engine component body formed of a ceramic matrix composite material having at least one fastener integrally formed with the gas turbine engine component body as a single-piece structure. The gas turbine engine component body initially comprises a rigidized preform structure formed from a polymer based material. The at least one fastener connects the gas turbine engine component body to an engine support structure.