Hybrid aircraft and landing launch/recovery system

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 11697508
APP PUB NO 20210047052A1
SERIAL NO

16995534

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A hybrid aircraft system uses a combination of direct propeller driven gas engine and electric motor power to provide vertical thrust and control for hover of the aircraft. Furthermore, a portable launch/recovery system is configured for use with an aircraft such as a Vertical Takeoff and Landing (VTOL) Unmanned Air Vehicle (UAV). The system is configured to enable ships with limited available deck space to become UAV-compatible.

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Patent Owner(s)

Patent OwnerAddress
LEIGH AEROSYSTEMS CORPORATION1232 KEYSTONE WAY VISTA CA 92081

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Harris, Gordon L Carlsbad, US 11 103
Harris, Stephen L Carlsbad, US 22 233

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