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. 08, 2020

Filed:

Feb. 19, 2018
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Luc Dionne, Candiac, CA;

Bruno Villeneuve, Boucherville, CA;

Jean Thomassin, Sainte-Julie, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 35/02 (2006.01); B64C 1/06 (2006.01); B64C 25/34 (2006.01); B64D 27/08 (2006.01); B64D 33/08 (2006.01); F01P 3/18 (2006.01); F01P 7/02 (2006.01); F01P 11/10 (2006.01); F02B 37/00 (2006.01); F02B 41/10 (2006.01); F02B 53/00 (2006.01); B64D 33/10 (2006.01); B64D 33/02 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 35/02 (2013.01); B64C 1/068 (2013.01); B64C 25/34 (2013.01); B64D 27/08 (2013.01); B64D 33/08 (2013.01); B64D 33/10 (2013.01); F01P 3/18 (2013.01); F01P 7/023 (2013.01); F01P 11/10 (2013.01); F02B 37/004 (2013.01); F02B 41/10 (2013.01); F02B 53/00 (2013.01); B64D 2027/026 (2013.01); B64D 2033/024 (2013.01); F02B 2053/005 (2013.01);
Abstract

An assembly for an aircraft having a propeller, including a wheel well for a retracted landing gear, first and second cooling ducts; and an engine assembly having an engine shaft configured for driving engagement with the propeller, the engine assembly including a coolant circulation system for circulation of a liquid coolant, a lubricant circulation system for circulation of a lubricant, a first heat exchanger in fluid communication with at least the coolant circulation system, and a second heat exchanger in fluid communication with at least the lubricant circulation system. Each heat exchanger is positioned and configured for receiving a cooling airflow from the respective cooling duct. The wheel well is located between the heat exchangers. A method of cooling a lubricant and a liquid coolant of an engine assembly is also discussed.


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