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:
Oct. 24, 2017

Filed:

Jul. 23, 2015
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Jean Thomassin, Ste Julie, CA;

Sebastien Bolduc, St-Bruno, CA;

Bruno Villeneuve, Boucherville, CA;

Stephane Berube, St-Philippe, CA;

Mike Fontaine, Boucherville, CA;

David Gagnon-Martin, Longueuil, CA;

Andre Julien, Ste-Julie, CA;

Mark Cunningham, Montreal, CA;

Serge Lafortune, Mascouche, CA;

Pierre-Yves Legare, Chambly, CA;

Assignee:

PRATT & WHITNEY CANADA CORP., Longueuil, Quebec, unknown;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02B 29/04 (2006.01); F01C 1/22 (2006.01); F01C 11/00 (2006.01); F02B 33/34 (2006.01); F02B 41/10 (2006.01); F02B 61/04 (2006.01); F01D 13/00 (2006.01); F02K 5/00 (2006.01); F02C 6/12 (2006.01); F02B 53/00 (2006.01);
U.S. Cl.
CPC ...
F02B 29/0493 (2013.01); F01C 1/22 (2013.01); F01C 11/002 (2013.01); F01C 11/008 (2013.01); F01D 13/003 (2013.01); F02B 29/0412 (2013.01); F02B 29/0418 (2013.01); F02B 33/34 (2013.01); F02B 41/10 (2013.01); F02B 53/00 (2013.01); F02B 61/04 (2013.01); F02C 6/12 (2013.01); F02K 5/00 (2013.01); F02B 2053/005 (2013.01); F05D 2220/40 (2013.01); Y02T 10/146 (2013.01); Y02T 10/163 (2013.01); Y02T 10/17 (2013.01);
Abstract

A compound engine assembly including an air conduit having an inlet in fluid communication with ambient air around the compound engine assembly, a compressor having an inlet in fluid communication with the air conduit, an engine core including at least one rotary internal combustion engine and having an inlet in fluid communication with an outlet of the compressor, a turbine section having an inlet in fluid communication with an outlet of the engine core and configured to compound power with the engine core; and at least one heat exchanger in fluid communication with the air conduit, each heat exchanger configured to circulate a fluid of the engine assembly in heat exchange relationship with an airflow from the air conduit circulating therethrough. A method of supplying air to a compound engine assembly is also discussed.


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