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:
Mar. 08, 2022

Filed:

Oct. 28, 2019
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Roderick M. Townes, London, GB;

Andrew T. Holt, London, GB;

Michael J. Whittle, London, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/18 (2006.01); F01D 5/28 (2006.01); B33Y 10/00 (2015.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 5/188 (2013.01); F01D 5/284 (2013.01); B33Y 10/00 (2014.12); F05D 2230/31 (2013.01); F05D 2230/60 (2013.01); F05D 2240/126 (2013.01); F05D 2260/201 (2013.01); F05D 2260/22141 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A turbine vane assembly adapted for use with a gas turbine engine includes an airfoil and a spar. The airfoil is formed to define a cavity that extends into the airfoil. The spar is located in the cavity to define a cooling passage that extends around the spar between the spar and the airfoil. The turbine vane assembly includes cooling features to aid heat transfer of the turbine vane assembly during operation in the gas turbine engine.


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