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. 21, 2025

Filed:

Dec. 15, 2022
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Etienne Plamondon, Candiac, CA;

Michel Bousquet, Longueuil, CA;

Kevin Nguyen, Montreal, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/10 (2006.01); F01C 1/22 (2006.01); F01C 11/00 (2006.01); F02C 3/14 (2006.01); F02C 6/12 (2006.01);
U.S. Cl.
CPC ...
F02K 3/10 (2013.01); F01C 1/22 (2013.01); F01C 11/008 (2013.01); F02C 3/14 (2013.01); F02C 6/12 (2013.01); F05D 2220/80 (2013.01);
Abstract

An aircraft power plant, has: a combustion engine having an outlet outputting combustion gases; a turbine downstream of the combustion engine; a detonation combustion tube fluidly connecting the combustion engine to the turbine; a member having an open position in which the outlet of the combustion engine is fluidly connected to the turbine and a closed position in which the combustion engine is fluidly disconnected from the turbine; a fuel injector fluidly connected to the detonation combustion tube; an igniter operatively connected to the detonation combustion tube; and a controller operatively connected to the fuel injector and to the igniter, the controller configured to, in response to receiving of a command: inject fuel into the detonation combustion tube via the fuel injector, and once the member is in the closed position, power the igniter to ignite a mixture of the combustion gases and the fuel into the detonation combustion tube.


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