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:
Mar. 04, 2025

Filed:

Feb. 08, 2024
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Yusuf Syed, Oakville, CA;

Thomas Trevor Ricci, Kirkland, CA;

James Jarvo, Long Sault, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/58 (2006.01); B64C 11/38 (2006.01); F01D 15/10 (2006.01); F01D 15/12 (2006.01); F01D 25/18 (2006.01); F02C 7/32 (2006.01);
U.S. Cl.
CPC ...
F02C 9/58 (2013.01); B64C 11/385 (2013.01); F01D 15/10 (2013.01); F01D 15/12 (2013.01); F01D 25/18 (2013.01); F02C 7/32 (2013.01);
Abstract

A method of and system for operating a hybrid electric propulsion system for an aircraft in a start sequence is provided. The hybrid electric propulsion system includes a thermal engine, an electric motor, a gearbox, an electric power storage unit, and a propulsion unit having a propeller having propeller blades. The method includes: driving the propeller from a static state to a target rotational speed within a predetermined range of speeds using the electric motor; transitioning the propeller blades from a feathered mode to an unfeathered mode while the propeller is being driven at the target rotational speed solely by the electric motor; starting the thermal engine; and transitioning the driving of the propeller using the electric motor to driving the propeller using the thermal engine.


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