Development of high speed flueric logic circuitry for a novel pneumatic stepping motor
High speed fluidic logic circuitry for pneumatic stepping motor
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High speed fluidic logic circuitry for pneumatic stepping motor
Steady state and dynamic performance of proportional fluidic diverter valve
Fluid power-transmitting gas bearing was designed that is essentially frictionless, stable, and highly efficient. The two basic components of this design are the base assembly and the upper plate. System could be a fluidic control system, a momentum exchange or reaction jet device.
Fluidics concept applied to miniaturized all-fluid high temperature sensing probes for use in hypervelocity wind tunnels
Advanced aerospace engineering research on fluid transmission lines, fluidic elements, hydraulic and pneumatic stepping motors, and fluid jet amplifier dynamics
Fluidic analog to pulse frequency converter for pneumatic reactor control drum actuator system
Design and performance of pneumatic-input fluidic servovalve
Fluidic control of high hydraulic pressure by means of hydrodynamic vortex phenomenon
X-15 flight test data on fluidic temperature sensor for measuring total temperature of hypersonic aircraft
Fluidic breadboard version of rocket engine sequence control, describing pneumatic logic package and general limitations
Actuator exerts linear force that is controllable and reproducible to microinch tolerance. It is constructed for extremely accurate control of a valve but can also be used as a variable venturi meter, micropositioner, microthruster, and in fluidics and reaction-control systems.
Simple fluidic vibration damper for installation at each pivotal mounting between gimbals isolates inertial measuring units from external vibration and other disruptive forces. Installation between each of the three gimbal axes can dampen vibration and shock in any direction while permitting free rotation of the gimbals.
Fluidic vortex valves used as fluid control elements in hydraulic servoactuator control system
Fluidic type temperature sensor for total temperature measurement for hypersonic aircraft in atmosphere
Fluidic secondary injection thrust vector control systems for solid propellant and hydrogen-oxygen rocket engines
Fluidic vortex valve to modulate solid propellant generated hot gas flow
Flapper valve using a bimorph piezoelectric ceramic bender converts an electrical input into a pneumatic output signal capable of operating fluidic logic elements in a decoder and display system.
System for monitoring of fluidic pressures in cranial cavity uses a miniaturized pressure sensing transducer, combined with suitable amplification means, a meter with scale calibrated in terms of pressures between minus 100 and plus 900 millimeters of water, and a miniaturized chart recorder covering similar range of pressures.