STATIC AND DYNAMIC PERFORMANCE OF PILOT OPERATED HYDRAULIC RELIEF VALVES | ||||
International Conference on Aerospace Sciences and Aviation Technology | ||||
Article 12, Volume 4, ASAT CONFLENCE 14-16 May 1991 , CAIRO, May 1991, Page 135-143 PDF (1.75 MB) | ||||
Document Type: Original Article | ||||
DOI: 10.21608/asat.1991.25672 | ||||
View on SCiNiTO | ||||
Authors | ||||
M. G. RABIE1; S. A. KASSEM2; S. A. EL SAYED3; M. A. AZIZ3; O. G. EL BAYED4 | ||||
1Assoc.Prof.,Aeronautical Dept.,Military Technical College.,Cairo. | ||||
2Prof., Dept.of Mech.Design and Prod., Eng.Faculty,Cairo Univ. | ||||
3Assoc.Prof., Dept of Mech.Design and Prod.,Eng. Faculty, Zagazig Univ. | ||||
4Assistant, Eng. Faculty, Zagazig Univ. | ||||
Abstract | ||||
An investigation of the performance of pilot operated hydraulic relief valves has been carried out. The valve behavior is described by means of a nonlinear mathematical model, considering the nonlinear variation of the restriction areas, the nonlinear flow-pressure relations and the flow forces. The theoretical treatment is carried out by treating the developed mathematical model using a digital simulation program. The model is validated in the steady state by comparing simulation and experimental results. The transient behavior of the valve is investigated theoretically. The effect of the dimensions of the damping orifices and volume of oil filling the inlet line is predicted. The simulation program is used to predict the optimum dimensions of the damping orifices, which introduced an observable improvement in the transient response. | ||||
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