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. 15, 2022

Filed:

Mar. 27, 2019
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Kevin Ng, Ancaster, CA;

Johnny Vinski, Châteauguay, CA;

Adam Logan, Toronto, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F02C 9/42 (2006.01); B64D 13/06 (2006.01); F02C 6/02 (2006.01); B64D 35/08 (2006.01); F02C 6/04 (2006.01); F02C 9/52 (2006.01);
U.S. Cl.
CPC ...
F02C 6/02 (2013.01); B64D 35/08 (2013.01); F02C 6/04 (2013.01); F02C 9/18 (2013.01); F02C 9/42 (2013.01); F02C 9/52 (2013.01); F05D 2220/329 (2013.01); F05D 2270/093 (2013.01); F05D 2270/13 (2013.01);
Abstract

A method of operating a multi-engine aircraft having two or more gas turbine engines includes operating a first engine in a powered mode to provide motive power to the aircraft, and, in flight, operating a second engine in either a powered mode to provide motive power to the aircraft or in a standby mode to provide substantially no motive power to the aircraft. When operating the second engine in the powered mode, pressurized air is bled from a first bleed location of a compressor of the second engine. When operating the second engine in the standby mode, pressurized air is bled from a second bleed location of the compressor of the second engine and supplying the pressurized air to a bleed air system of the second engine. The second bleed location is downstream of the first bleed location within the compressor of the second engine.


Find Patent Forward Citations

Loading…