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Hub-mounted actuators for blade pitch collective controlBlade collective pitch control is provided for a rotor system by rotary actuators located between adjacent blades. Each actuator is connected to the leading edge of one adjacent blade and the trailing edge of the other adjacent blade.
Document ID
20080005894
Acquisition Source
Ames Research Center
Document Type
Other - Patent
Authors
Jeffery, Philip A. E.
Luecke, Greg R.
Date Acquired
August 24, 2013
Publication Date
November 26, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-644001
Patent Number: US-PATENT-4,555,219
Funding Number(s)
CONTRACT_GRANT: NAS2-11058
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,555,219
Patent Application
US-PATENT-APPL-SN-644001

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