VARIABLE PITCH FAN ACTUATOR

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20200024981A1
SERIAL NO

16188373

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A gas turbine engine including a core having in serial flow order a compressor, a combustor, and a turbine—the compressor, combustor, and turbine together defining a core air flowpath. The gas turbine engine additionally includes a fan section mechanically coupled to the core, the fan section including a plurality of fan blades, and each of the plurality fan blades defining a pitch axis. An actuation device is operable with the plurality fan blades for rotating the plurality fan blades about their respective pitch axes, the actuation device including an actuator located outward of the core air flowpath to, e.g., simplify the gas turbine engine.

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  • Owner owned or assignment not recorded

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Miller, Brandon Wayne Liberty Township, US 119 178
Niergarth, Daniel Alan Cincinnati, US 52 60
Zatorski, Darek Tomasz Fort Wright, US 62 99

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