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. 29, 2023

Filed:

May. 22, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Jonathan Ortiz, Torrance, CA (US);

Matthew P. Forcier, South Windsor, CT (US);

William K. Ackermann, East Hartford, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F01D 9/06 (2006.01); F02C 7/18 (2006.01); F01D 17/02 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F01D 9/065 (2013.01); F01D 17/02 (2013.01); F02C 7/18 (2013.01); F05D 2220/32 (2013.01); F05D 2260/20 (2013.01); F05D 2270/30 (2013.01);
Abstract

A bleed air cooling system for a gas turbine engine includes one or more bleed ports located at one or more axial locations of the gas turbine engine to divert a bleed airflow from a gas turbine engine flowpath, a bleed outlet located at a cooling location of the gas turbine engine and a bleed duct in fluid communication with the bleed port and the configured to convey the bleed airflow from the bleed port to the bleed outlet. One or more safety sensors are configured to sense operational characteristics of the gas turbine engine, and a controller is operably connected to the one or more safety sensors and configured to evaluate the sensed operational characteristics for anomalies in operation of the bleed air cooling system.


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