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Vortex servovalve for fluidic or electrical inputProportional-pressure control servovalve consisting of fluid amplifier bellows-driven jet-pipe and two vortex valves operating in push-pull, with a pair of bellows for pressure feedback is tolerant to comtaminant particles and meets minimum standby flow requirements for applications such as rocket thruster nozzles.
Document ID
19720000173
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Honda, T. S. (GE)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Machinery
Report/Patent Number
ARC-10155
Accession Number
72B10173
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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