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. 25, 2021

Filed:

Dec. 27, 2018
Applicants:

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

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

Inventors:

Behram Kapadia, McCordsville, IN (US);

Jack Moody, Indianapolis, IN (US);

Ryan C. Humes, Indianapolis, IN (US);

Brandon R. Snyder, Greenwood, IN (US);

Assignees:

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

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/18 (2006.01); F02C 9/18 (2006.01); F01D 25/12 (2006.01); F02K 3/06 (2006.01); F01D 19/02 (2006.01);
U.S. Cl.
CPC ...
F01D 11/18 (2013.01); F01D 25/12 (2013.01); F02C 9/18 (2013.01); F02K 3/06 (2013.01); F01D 19/02 (2013.01); F05D 2220/323 (2013.01); F05D 2220/3212 (2013.01); F05D 2240/11 (2013.01); F05D 2260/606 (2013.01); F05D 2270/42 (2013.01);
Abstract

The present disclosure relates to a gas turbine engine including a turbine wheel mounted for rotation about a central axis and a turbine shroud ring mounted radially outward from the turbine wheel. The turbine wheel includes a plurality of blades that are spaced apart radially from the turbine shroud ring to establish a blade tip clearance gap. The gas turbine engine further includes a blade tip clearance control system that passively controls the size of the clearance gap based on engine operation.


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