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:
Dec. 13, 2022

Filed:

Dec. 05, 2018
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Jean Thomassin, Sainte-Julie, CA;

David Meisels, Montreal, CA;

Richard Ullyott, St-Bruno, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01P 11/10 (2006.01); B64C 9/38 (2006.01); B64D 33/10 (2006.01); B64C 21/04 (2006.01); B64C 21/06 (2006.01); B64D 27/10 (2006.01); F01P 3/20 (2006.01); F01P 5/10 (2006.01); B64C 21/08 (2006.01);
U.S. Cl.
CPC ...
F01P 11/10 (2013.01); B64C 9/38 (2013.01); B64C 21/04 (2013.01); B64C 21/06 (2013.01); B64C 21/08 (2013.01); B64D 27/10 (2013.01); B64D 33/10 (2013.01); F01P 3/20 (2013.01); F01P 5/10 (2013.01); B64C 2230/04 (2013.01); B64C 2230/22 (2013.01); Y02T 50/10 (2013.01); Y02T 50/30 (2013.01); Y02T 50/40 (2013.01);
Abstract

A method of providing active flow control for an aircraft includes cooling a liquid coolant in a heat exchanger by circulating a cooling airflow through the heat exchanger, and providing fluid communication between the cooling airflow and a boundary layer flow of at least one flight control surface of the aircraft. The cooling airflow affects the boundary layer flow of the flight control surface(s) to provide active flow control. A method of cooling an engine core of an engine assembly includes circulating a cooling fluid through the engine core, and cooling the cooling fluid with a cooling airflow used to provide active flow control to a flight control surface of the aircraft. An active flow control system for an aircraft is also discussed.


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