Research and development of a vortex valve for flow modulation of a 16-percent aluminized 5500 deg F propellant gas
Vortex valve for hot gas flow modulation in secondary injection thrust vector control system
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Vortex valve for hot gas flow modulation in secondary injection thrust vector control system
Performance of vortex valve controlled secondary injection thrust vector system for solid propellant rocket motor control
Roentgen video densitometer study of mitral valve closure during fibrilation, discussing atrial contraction role on ventricular function in normal and failing heart
Initiating combustion of altitude control rocket engines in a precombustion chamber of ductile material reduces high pressure surges generated by hypergolic propellants. Two-step bipropellant valve concepts control initial propellant flow into precombustion chamber and subsequent full flow into main chamber.
Performance tests on modified manual gas valve
Environmental tests of manual globe valves for high pressure helium storage tanks
Design and performance of liquid oxygen tank vent and relief valve
Electronic position indicator for latching solenoid valves in SNAP 8 ground test facility
Relief valve to permit slow and fast bleeding rates at difference pressure levels
Dynamic performance analysis of fast-response fuel control valve for air breathing engine research
Fluidic vortex valve warm gas flow control for rocket application
Fluidic vortex valve to modulate solid propellant generated hot gas flow
Thin ring valve for the inlets and exhausts of reciprocating compressors, and possibly for the inlets of internal combustion engines, encircles the cylinder and operates on the Bernoulli principle.
Microminiature slide action valve requires power only during actuation and can be used as an on-off or single inlet to alternately selected outlets.
Valve is insensitive to fluctuating sense pressure. It remains in full-open position until the supply pressure is removed.
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.
Inducing losses in the vortex chamber of vortex valves and vortex amplifiers resolves the problem of unstable operation caused by a sufficiently large positive feedback. Induced losses also reduce pressure gain and throttling range of vortex pressure amplifier.