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:
Mar. 09, 2021

Filed:

Dec. 16, 2015
Applicants:

Rolls-royce North American Technologies, Inc., Indianapolis, IN (US);

Rolls-royce High Temperature Composites Inc., Cypress, CA (US);

Inventors:

Ted J. Freeman, Danville, IN (US);

Wayne S. Steffier, Huntington Beach, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/60 (2006.01); F01D 25/28 (2006.01); F23R 3/00 (2006.01); F01D 11/08 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F23R 3/60 (2013.01); F01D 11/08 (2013.01); F01D 25/246 (2013.01); F01D 25/28 (2013.01); F23R 3/002 (2013.01); F23R 3/007 (2013.01); F05D 2260/30 (2013.01); F23R 2900/00017 (2013.01);
Abstract

A combustor of a gas turbine engine and a turbine shroud for a turbine of a gas turbine engine are disclosed. The combustor is configured to ignite a mixture of compressed air and fuel in a combustion chamber included therein. The turbine shroud is configured to direct products of the combustion reaction toward a plurality of rotatable turbine blades of the turbine to cause the plurality of turbine blades to rotate.


Find Patent Forward Citations

Loading…