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:
Nov. 12, 2024

Filed:

Sep. 13, 2023
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventor:

Richard Freer, Saint-Basile-le-Grand, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 5/06 (2006.01); B64D 27/08 (2006.01); B64D 27/20 (2006.01); B64D 27/24 (2006.01); B64D 33/08 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64D 27/08 (2013.01); B64D 27/20 (2013.01); B64D 33/08 (2013.01); F02C 5/06 (2013.01); B64D 27/026 (2024.01);
Abstract

An aircraft propulsion system for an aircraft having a nacelle that includes a pylon structure is provided. The system includes compressor and turbine sections, an IC engine, a fan, and an IC engine cooling system. The compressor section is powered by a first electric motor. The turbine section is configured to power a first electric generator configured to produce electrical power. The first fan is rotationally driven by a second electric motor. The fan has a hub and a plurality of fan blades extending radially outward from the hub. The hub is disposed in the pylon interior region and the fan blades are configured to extend outside of the pylon structure. The fan is positioned downstream of the compressor section. The IC engine cooling system has a heat exchanger and a pump configured to provide coolant communication between the IC engine and the heat exchanger.


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