AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20240017842A1
SERIAL NO

17866081

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An aircraft system is provided that includes a first propulsor rotor, a first transmission, a second propulsor rotor, a second transmission and an intermittent combustion engine. The first propulsor rotor is rotatable about a first propulsor axis. The first transmission is coupled to the first propulsor rotor. The second propulsor rotor is rotatable about a second propulsor axis. The second transmission is coupled to the second propulsor rotor. The intermittent combustion engine is configured to drive rotation of the first propulsor rotor through the first transmission. The intermittent combustion engine is configured to drive rotation of the second propulsor rotor through the second transmission.

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Patent Owner(s)

Patent OwnerAddress
PRATT & WHITNEY CANADAQUEBEC CAN QUEBEC

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Freer, Richard Saint-Basile-Le-Grand, CA 64 87

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