NASA NTRS · 19720000173
Vortex servovalve for fluidic or electrical input
Abstract
Proportional-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.
Keep this discovery
Explore connections, maps & timelines
Honda, T. S.. 1972-01-01. Vortex servovalve for fluidic or electrical input. https://ntrs.nasa.gov/citations/19720000173
Cite the original work for its findings. Save a collection to share your selection of sources.