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:
Aug. 16, 2022

Filed:

Jan. 24, 2020
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Michael J. Whittle, London, GB;

Keith Sadler, London, GB;

Matthew D. Thomason, London, GB;

Andrew Holt, London, GB;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/28 (2006.01); F01D 11/08 (2006.01); F01D 25/24 (2006.01); F01D 25/12 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 5/284 (2013.01); F01D 5/282 (2013.01); F01D 11/08 (2013.01); F01D 25/12 (2013.01); F01D 25/246 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2240/11 (2013.01); F05D 2240/12 (2013.01); F05D 2240/55 (2013.01); F05D 2240/81 (2013.01); F05D 2260/20 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A gas turbine engine includes a shroud ring, a vane ring, and a secondary flow assembly. The shroud ring extends around an associated turbine wheel and includes a carrier segment and a blade track segment comprising ceramic matrix composite materials. The blade track segment and the carrier segment defining a shroud cavity radially therebetween. The vane ring includes a heat shield comprising ceramic matrix composite materials that forms an outer platform, an inner platform, and an airfoil defining a heat shield cavity radially through the heat shield. The secondary flow assembly includes a recirculating flow circuit having a discharge tube and a vane pressurizing tube; and the secondary flow assembly is configured to cool the blade track segment. The flow circuit is further configured to pressurize the heat shield cavity thereby providing a seal against the gases from the primary gas path entering the heat shield cavity.


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