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:
Jun. 06, 2023

Filed:

Oct. 16, 2020
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Charles Cormier, Sainte-Julie, CA;

Daniel Coutu, Longueuil, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/22 (2006.01); F01D 7/00 (2006.01); F02C 9/58 (2006.01); F02K 1/66 (2006.01);
U.S. Cl.
CPC ...
F02C 9/22 (2013.01); F01D 7/00 (2013.01); F02C 9/58 (2013.01); F02K 1/66 (2013.01); F05D 2220/323 (2013.01); F05D 2240/12 (2013.01); F05D 2270/051 (2013.01); F05D 2270/304 (2013.01);
Abstract

A method and a system for providing in-flight reverse thrust for an aircraft are provided. The aircraft comprises an engine having a rotor, a compressor mechanically coupled to the rotor, and a variable geometry mechanism provided upstream of the compressor and configured to modulate an amount of compression work performed by the compressor. The method comprises operating the rotor with the variable geometry mechanism in a first position, receiving a request to increase reverse thrust for the rotor, in response to the request, adjusting the variable geometry mechanism from the first position towards a second position, the variable geometry mechanism having a greater opening angle in the second position than in the first position, and operating the rotor with the variable geometry mechanism in the second position for causing an increase in the amount of compression work performed by the compressor and an increase in reverse thrust for the rotor.


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