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Compensating linkage for main rotor controlA compensating linkage for the rotor control system on rotary wing aircraft is described. The main rotor and transmission are isolated from the airframe structure by clastic suspension. The compensating linkage prevents unwanted signal inputs to the rotor control system caused by relative motion of the airframe structure and the main rotor and transmission.
Document ID
19810010561
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Jeffery, P. A. E. (United Aircraft Corp. Stratford, Conn., United States)
Huber, R. F. (United Aircraft Corp. Stratford, Conn., United States)
Date Acquired
September 4, 2013
Publication Date
January 20, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Number: US-PATENT-4,245,956
Patent Application Number: US-PATENT-APPL-SN-969755
Patent Number: NASA-CASE-LAR-11797-1
Accession Number
81N19087
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,245,956|NASA-CASE-LAR-11797-1
Patent Application
US-PATENT-APPL-SN-969755

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