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:
Apr. 26, 2022

Filed:

Aug. 20, 2019
Applicants:

Rolls-royce Corporation, Indianapolis, IN (US);

Rolls-royce Plc, London, GB;

Inventors:

Daniel K. Vetters, Indianapolis, IN (US);

Michael J. Whittle, London, GB;

Assignees:

Rolls-Royce Corporation, Indianapolis, IN (US);

Rolls-Royce plc;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 5/28 (2006.01); F01D 5/14 (2006.01); F01D 11/00 (2006.01); F01D 11/02 (2006.01);
U.S. Cl.
CPC ...
F01D 5/18 (2013.01); F01D 5/147 (2013.01); F01D 5/282 (2013.01); F01D 5/284 (2013.01); F01D 11/001 (2013.01); F01D 11/025 (2013.01); F05D 2220/323 (2013.01); F05D 2240/12 (2013.01); F05D 2240/301 (2013.01); F05D 2240/55 (2013.01); F05D 2300/6033 (2013.01);
Abstract

An airfoil assembly for a gas turbine engine includes a vane, a support strut, and an inner carrier. The vane is adapted to interact with hot gases flowing around the airfoil assembly during use of the airfoil assembly. The support strut is located in an interior cavity formed in the vane and configured to receive force loads applied to the ceramic matrix composite vane by the hot gases. The inner carrier is coupled with the support strut and adapted to block the hot gases from flowing radially inward toward an axis of the gas turbine engine.


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