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:
Jan. 04, 2022

Filed:

Aug. 03, 2016
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Anthony Jones, San Diego, CA (US);

Andre Julien, Ste-Julie, CA;

David Menheere, Norval, CA;

Jean Thomassin, Ste-Julie, CA;

Richard Ullyott, St-Bruno, CA;

Daniel Van Den Hende, Mississauga, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 33/10 (2006.01); B64D 41/00 (2006.01); B64D 33/08 (2006.01); B64F 5/20 (2017.01); B64D 15/06 (2006.01); F01P 3/20 (2006.01); F01P 7/16 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
B64D 33/10 (2013.01); B64D 15/06 (2013.01); B64D 33/08 (2013.01); B64D 41/00 (2013.01); B64F 5/20 (2017.01); F01P 3/20 (2013.01); F01P 7/16 (2013.01); B64D 2033/0213 (2013.01); B64D 2033/0233 (2013.01); F01P 2025/08 (2013.01); F01P 2050/20 (2013.01); F01P 2060/18 (2013.01); F05D 2220/50 (2013.01); F05D 2260/213 (2013.01); Y02P 70/50 (2015.11); Y02T 50/60 (2013.01);
Abstract

An aircraft heating assembly including an internal combustion engine having a liquid coolant system distinct from any fuel and lubricating system of the engine and including cooling passages in the internal combustion engine for circulating a liquid coolant from a coolant inlet to a coolant outlet, a coolant circulation path outside of the internal combustion engine and in fluid communication with the coolant inlet and the coolant outlet, and a heating element in heat exchange relationship with a portion of the aircraft to be heated. The coolant circulation path extends through a heat exchanger configured to remove a portion of a waste heat from the liquid coolant. The heating element is in heat exchange relationship with the coolant circulation path to receive another portion of the waste heat therefrom. A method of heating a portion of an aircraft is also discussed.


Find Patent Forward Citations

Loading…