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. 24, 2021

Filed:

Nov. 08, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Peter M. Munsell, Granby, CT (US);

Philip S. Stripinis, Rocky Hill, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/08 (2006.01); F01D 11/06 (2006.01); F01D 25/12 (2006.01); F01D 11/04 (2006.01); F02C 9/18 (2006.01); F02C 7/28 (2006.01); F02C 7/06 (2006.01);
U.S. Cl.
CPC ...
F02C 6/08 (2013.01); F01D 11/04 (2013.01); F01D 11/06 (2013.01); F01D 25/125 (2013.01); F02C 9/18 (2013.01); F02C 7/06 (2013.01); F02C 7/28 (2013.01); F05D 2260/601 (2013.01); Y02T 50/60 (2013.01); Y10T 29/49323 (2015.01);
Abstract

A gas turbine engine includes a fan, a compressor section, and a turbine section configured to drive the compressor section and the fan. A buffer system is configured to communicate a buffer supply air to a portion of the gas turbine engine. The buffer system includes a first bleed air supply having a first pressure, a second bleed air supply having a second pressure that is greater than the first pressure, and an ejector that selectively augments the first bleed air supply to prepare the buffer supply air for communication to the portion of the gas turbine engine. A method and a buffer system are also disclosed.


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