Dynamic Model for a Dome-Loaded Pressure Regulator

Author:

Nabi A.1,Wacholder E.1,Dayan J.2

Affiliation:

1. Rafael–Israel Armament Development Authority, P.O. Box 2250, Haifa, 31021, Israel

2. Technion–Israel Institute of Technology, Mechanical Engineering Faculty, Haifa, 32000, Israel

Abstract

A generalized physical model describing dynamic behavior of a fast-acting, dome-loaded, gas pressure regulator was developed. The regulator is designed to respond quickly to command changes, and to operate over a wide range of flow rates and pressures. The analytical lumped-parameter model developed consists of a set of nonlinear, first-order, ordinary differential equations with respect to time, accounting for mass and energy conservation at regulator outlet, command dome and internal feedback compartments. It also accounts for the equation-of-motion for the poppet and the control piston-assembly. The numerical solution, based on a Runge–Kutta method, is amenable to an extensive parametric study of regulator performance, and serves as a useful analytical tool for designing new pressure regulators. Several tests were performed on a fast-acting regulator to verify the physical model. Good agreement between predictions and measurements was obtained. The effect of several parameters, geometrical and operational, on regulator performance was studied. [S0022-0434(00)00402-0]

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Reference9 articles.

1. Tsai, D. H., and Cassidy, E. C., 1961, “Dynamic Behavior of Simple Pneumatic Pressure Reducer,” ASME J. Basic Eng., 83, p. 253253.

2. Dustin, M. O., 1971, “Analog Computer Study of Design Parameter Effects on the Stability of a Direct-Acting Gas Pressure Regulator,” NASA TN D-6267.

3. Anisimikin, Yu. S., Kvasov, V. M., Kravchenko, Yu., Suslin, E. I., Shorin, V. P., and Chibizov, V. V., 1976, “Stability Analysis of Gas Pressure Regulator Operating Under High-Temperature Conditions Over a Wide Flow Rate Range,” Sov. Aeronaut., 19, No. 1, p. 9494.

4. Sverbilov, Y. Ya , and Anisimikin, Yu. S., 1981, “Evaluation of Multi-Purpose Gas Pressure Regulator Stability,” Sov. Aeronaut. 24, No. 3, p. 6262.

5. Andersen, B. W., 1967, The Analysis and Design of Pneumatic Systems, Wiley, New York.

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