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. 07, 2020

Filed:

Mar. 07, 2016
Applicants:

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

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

Inventors:

Tara G. Schetzel, Indianapolis, IN (US);

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

David J. Thomas, Brownsburg, IN (US);

Assignees:

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

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 5/28 (2006.01); B23P 15/04 (2006.01); F01D 5/22 (2006.01); F01D 5/18 (2006.01); F01D 5/20 (2006.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); B23P 15/04 (2013.01); F01D 5/187 (2013.01); F01D 5/20 (2013.01); F01D 5/225 (2013.01); F01D 5/284 (2013.01); F05D 2220/32 (2013.01); F05D 2230/237 (2013.01); F05D 2250/241 (2013.01); F05D 2260/2214 (2013.01); F05D 2260/231 (2013.01); F05D 2300/6033 (2013.01);
Abstract

An airfoil assembly for use in a gas turbine engine is disclosed. The airfoil assembly includes a root, a tip shroud, and an airfoil located between the root and tip shroud. The airfoil includes a spar, a heat shield arranged around the spar, and a plurality of describe rigid load supports extending between the spar and the heat shield to transfer loads between the heat shield and the spar.


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