NASA NTRS ยท 19850011105
The development of a microprocessor-controlled linearly-actuated valve assembly
Abstract
The development of a proportional fluid control valve assembly is presented. This electromechanical system is needed for space applications to replace the current proportional flow controllers. The flow is controlled by a microprocessor system that monitors the control parameters of upstream pressure and requested volumetric flow rate. The microprocessor achieves the proper valve stem displacement by means of a digital linear actuator. A linear displacement sensor is used to measure the valve stem position. This displacement is monitored by the microprocessor system as a feedback signal to close the control loop. With an upstream pressure between 15 and 47 psig, the developed system operates between 779 standard CU cm/sec (SCCS) and 1543 SCCS.
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Wall, R. H.. 1984-05-01. The development of a microprocessor-controlled linearly-actuated valve assembly. https://ntrs.nasa.gov/citations/19850011105
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