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:
Feb. 11, 2020

Filed:

Nov. 29, 2017
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Serge Dussault, Ste-Julie, CA;

Andre Julien, Ste-Julie, CA;

Michael Lanktree, La Prairie, CA;

Edwin Schulz, St-Bruno, CA;

Jean Thomassin, Ste-Julie, CA;

Nigel Davenport, Hillsburgh, CA;

Eugene Gekht, Brossard, CA;

Assignee:

Pratt & Whitney Canada Corp., Longueuil, Quebec, CA;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02B 55/08 (2006.01); F02B 53/12 (2006.01); F02B 53/02 (2006.01); F02B 19/12 (2006.01); F02B 53/10 (2006.01); F01C 21/18 (2006.01); F01C 21/10 (2006.01); F01C 21/06 (2006.01); F01C 1/22 (2006.01); F02B 19/10 (2006.01); F04C 29/00 (2006.01); F01C 21/08 (2006.01); F01C 20/24 (2006.01); F01C 20/10 (2006.01); F01C 20/06 (2006.01); F01C 11/00 (2006.01);
U.S. Cl.
CPC ...
F02B 55/08 (2013.01); F01C 1/22 (2013.01); F01C 21/06 (2013.01); F01C 21/106 (2013.01); F01C 21/18 (2013.01); F01C 21/183 (2013.01); F02B 19/108 (2013.01); F02B 19/12 (2013.01); F02B 53/02 (2013.01); F02B 53/10 (2013.01); F02B 53/12 (2013.01); F01C 11/006 (2013.01); F01C 20/06 (2013.01); F01C 20/10 (2013.01); F01C 20/24 (2013.01); F01C 21/08 (2013.01); F04C 29/0092 (2013.01); F04C 2240/80 (2013.01); Y02T 10/125 (2013.01); Y02T 10/17 (2013.01);
Abstract

A rotary engine including a rotor sealingly received within an internal cavity of an outer body to define a plurality of combustion chambers having a variable volume, a pilot subchamber located in a wall of the outer body, the pilot subchamber in fluid communication with the internal cavity via at least two spaced apart transfer holes defining a flow restriction between the pilot subchamber and the internal cavity, a pilot fuel injector in fluid communication with the pilot subchamber, an ignition element configured for igniting fuel in the pilot subchamber, and a main fuel injector extending through the stator body and communicating with the cavity at a location spaced apart from the pilot subchamber. A method of combusting fuel in a rotary engine is also discussed.


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