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:
May. 21, 2019

Filed:

Dec. 02, 2015
Applicants:

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

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

Inventors:

Jun Shi, Carmel, IN (US);

Robert J. Shinavski, Mission Viejo, CA (US);

Assignees:

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

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B32B 18/00 (2006.01); F01D 11/00 (2006.01); C23C 16/04 (2006.01); F01D 5/02 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); F01D 5/30 (2006.01); B32B 15/14 (2006.01); C23C 16/32 (2006.01); B32B 9/04 (2006.01); C04B 37/02 (2006.01); B32B 5/26 (2006.01); B32B 3/30 (2006.01);
U.S. Cl.
CPC ...
F01D 5/284 (2013.01); B32B 3/30 (2013.01); B32B 5/26 (2013.01); B32B 9/041 (2013.01); B32B 15/14 (2013.01); B32B 18/00 (2013.01); C04B 37/025 (2013.01); C23C 16/045 (2013.01); C23C 16/325 (2013.01); F01D 5/02 (2013.01); F01D 5/147 (2013.01); F01D 5/282 (2013.01); F01D 5/3092 (2013.01); F01D 11/006 (2013.01); B32B 2255/02 (2013.01); B32B 2255/20 (2013.01); B32B 2262/105 (2013.01); B32B 2307/306 (2013.01); B32B 2603/00 (2013.01); C04B 2237/04 (2013.01); C04B 2237/06 (2013.01); C04B 2237/083 (2013.01); C04B 2237/365 (2013.01); C04B 2237/38 (2013.01); C04B 2237/40 (2013.01); C04B 2237/405 (2013.01); C04B 2237/592 (2013.01); C04B 2237/61 (2013.01); C04B 2237/708 (2013.01); F05D 2220/32 (2013.01); F05D 2230/314 (2013.01); F05D 2230/60 (2013.01); F05D 2240/30 (2013.01); F05D 2240/55 (2013.01); F05D 2300/10 (2013.01); F05D 2300/21 (2013.01); F05D 2300/222 (2013.01); F05D 2300/2261 (2013.01); F05D 2300/514 (2013.01); F05D 2300/6033 (2013.01); F05D 2300/614 (2013.01);
Abstract

An assembly for use in a gas turbine engine and method for making the same are described herein. The assembly comprising a CMC component, a metallic component spaced apart from the CMC component, and a spacer. The spacer having a first surface in contact with the CMC and a second surface opposite the first surface in contact with the metallic component, the spacer comprising a CMC substantially free of silicon metal with a porosity of between about 5 percent and about 40 percent by volume to chemically isolate the CMC component from the metallic component.


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