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:
Apr. 09, 2019

Filed:

Aug. 03, 2016
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Andre Julien, Ste-Julie, CA;

Jean Thomassin, Ste-Julie, CA;

Maxime Courtois, Longueuil, CA;

Bruno Villeneuve, Boucherville, CA;

Serge Dussault, Ste-Julie, CA;

Richard Ullyott, St-Bruno, CA;

Serge LaFortune, Mascouche, CA;

Luc Dionne, Candiac, CA;

Anthony Jones, San Diego, CA (US);

Behzad Hagshenas, San Diego, CA (US);

David Menheere, Norval, CA;

Assignee:

PRATT & WHITNEY CANADA CORP., Longueuil, QC, CA;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/38 (2006.01); F01P 5/02 (2006.01); F02B 53/02 (2006.01); F01C 21/18 (2006.01); F02C 7/14 (2006.01); B64D 41/00 (2006.01); F01C 1/22 (2006.01); F02K 5/00 (2006.01); F02C 5/00 (2006.01); F02C 7/18 (2006.01); F02B 63/04 (2006.01); F02B 63/06 (2006.01); F02B 67/04 (2006.01); F01N 3/05 (2006.01); F01P 11/10 (2006.01); F02K 1/82 (2006.01); F02B 53/00 (2006.01);
U.S. Cl.
CPC ...
F02K 1/386 (2013.01); B64D 41/00 (2013.01); F01C 1/22 (2013.01); F01C 21/18 (2013.01); F01N 3/05 (2013.01); F01P 5/02 (2013.01); F01P 11/10 (2013.01); F02B 53/02 (2013.01); F02B 63/04 (2013.01); F02B 63/06 (2013.01); F02B 67/04 (2013.01); F02C 5/00 (2013.01); F02C 7/14 (2013.01); F02C 7/18 (2013.01); F02K 1/82 (2013.01); F02K 5/00 (2013.01); B64D 2041/002 (2013.01); F02B 2053/005 (2013.01); F05D 2220/50 (2013.01); F05D 2260/213 (2013.01); F05D 2300/173 (2013.01); F05D 2300/43 (2013.01); F05D 2300/603 (2013.01); Y02T 10/17 (2013.01); Y02T 50/53 (2013.01); Y02T 50/672 (2013.01); Y02T 50/676 (2013.01);
Abstract

An engine assembly for an aircraft, including an internal combustion engine having a liquid coolant system in fluid communication with a heat exchanger, an exhaust duct in fluid communication with air passages of the heat exchanger, a fan in fluid communication with the exhaust duct for driving a cooling air flow through the air passages of the heat exchanger and into the exhaust duct, and an intermediate duct in fluid communication with an exhaust of the engine and having an outlet positioned within the exhaust duct downstream of the fan and upstream of the outlet of the exhaust duct. The outlet of the intermediate duct is spaced inwardly from a peripheral wall of the exhaust duct. The engine assembly may be configured as an auxiliary power unit. A method of discharging air and exhaust gases in an auxiliary power unit having an internal combustion engine is also discussed.


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