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US Patent 8382030 Variable cycle VTOL powerplant

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Is a
Patent
Patent
1

Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
1
Patent Number
83820301
Patent Inventor Names
Patrick A. Kosheleff1
Date of Patent
February 26, 2013
1
Patent Application Number
128073111
Date Filed
September 2, 2010
1
Patent Citations Received
‌
US Patent 11859542 Dual power lift system
2
Patent Primary Examiner
‌
Tien Dinh
1
Patent abstract

A VTOL aircraft powerplant choosing between a low-power, turbofan mode during cruise flight and a high-power, lift fan mode during vertical flight. Turbofan mode is a gas turbine engine's shaft power driving a remote front fan. Its fan flow goes to thrust for cruising flight. During VTOL, front fan output enters a boost compressor. It produces the compressed air for a combustion chamber which feeds a large lift-fan turbine. That is the implementation of lift-fan mode. The boost compressor has more stages than the front fan and is a big added load. The gas turbine engine is supercharged to turn that added load: Part of the boost compressor output is taken during VTOL. This is a new version of the supercharging. During cruise flight, a low pressure turbine stage is bypassed to match the lesser load. That completes the apparatus for a variable-cycle VTOL engine.

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