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Pivoting output unit control systems activated by jacksAn invention to be used for controlling aircraft flaps is described. It is applicable to control systems with two coaxial output units which pivot simultaneously with respect to two fixed units and which are activated by two opposed, straight coaxial jacks.
Document ID
19790001895
Acquisition Source
Legacy CDMS
Document Type
Other - Other
Authors
Belliere, P. (NASA Headquarters Washington, DC United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1978
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-75581
Report Number: NASA-TM-75581
Accession Number
79N10066
Funding Number(s)
CONTRACT_GRANT: NASW-3199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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