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:
Dec. 28, 2021

Filed:

Apr. 10, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventor:

JinQuan Xu, East Greenwich, RI (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 17/14 (2006.01); F01D 25/12 (2006.01); F02C 7/18 (2006.01); F01D 17/10 (2006.01); F02C 7/14 (2006.01); F02C 9/18 (2006.01); B64D 33/02 (2006.01); F01D 11/00 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F01D 17/145 (2013.01); F01D 11/003 (2013.01); F01D 17/105 (2013.01); F01D 25/12 (2013.01); F02C 3/04 (2013.01); F02C 7/14 (2013.01); F02C 7/18 (2013.01); F02C 9/18 (2013.01); B64D 2033/024 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2260/213 (2013.01); F05D 2300/514 (2013.01); Y02T 50/60 (2013.01);
Abstract

A cooling system for a gas turbine engine comprises a passage capable of receiving cooling air, a compartment radially adjacent thereto and axially aligned therewith, an opening therebetween, a valve within the opening, and a heat exchanger received in the compartment. The valve is moveable between a maximum open position and a minimum open position for increasing or decreasing airflow from the passage into the compartment. At the valve minimum open position, a leakage path is provided between the passage and the compartment, whereby cooling air is capable of passing from the passage to the compartment and toward the heat exchanger at all valve positions. A gas turbine engine is also disclosed.


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