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:

Sep. 04, 2019
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventor:

Daniel Coutu, Longueuil, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/42 (2006.01); F01D 9/04 (2006.01); F01D 17/06 (2006.01); F01D 17/16 (2006.01); F02C 9/54 (2006.01);
U.S. Cl.
CPC ...
F02C 9/42 (2013.01); F01D 9/041 (2013.01); F01D 17/06 (2013.01); F01D 17/16 (2013.01); F02C 9/54 (2013.01); F05D 2220/323 (2013.01); F05D 2270/071 (2013.01); F05D 2270/304 (2013.01);
Abstract

A method of operating a multi-engine aircraft includes operating a first engine of the aircraft to provide motive power; and operating a second engine of the aircraft in a standby mode to provide substantially no motive power, a rotor of the second engine having an idle rotational speed in the standby mode, and in the standby mode, sequentially executing cycles, a given cycle of the cycles including: opening a set of variable guide vanes upstream a compressor section of the second engine, spiking a rate of a fuel flow to a combustor of the second engine, the spiking and the opening timed to increase a rotational speed of the rotor of the second engine to an upper threshold above the idle rotational speed of the rotor, and in response to the rotational speed reaching the upper threshold, at least substantially closing the set of variable guide vanes.


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