A quantitative methodology on constant pressure valve (CPV) stability analysis was presented. Firstly
the main parameters affecting static property of CPV were got by static analysis. The root-locus plots of CPV were achieved through small deviation dynamic analysis. By defining the concept of critical inlet pressure
the quantitative results of five main structural parameters' effect on the CPV stability margin was got: the spring stiffness has a little effect on stability margin; the increase of spool diameter
damping coefficient
load
and decrease of constant pressure chamber volume could enlarge the stability margin. The analytical result has an excellent consistence with AMESim simulation result and engineering experience. Finally
two conclusions were presented for enhancing the stability margin of CPV: (1) for improving problem of CPV
the most effective method is to change the outlet area; (2) for CPV design problem
based on the inlet pressure requirement and the minimum load
the critical inlet pressure need be determined firstly
and then the spool area and constant pressure chamber volume are taken as main design parameters by dynamic analysis.
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Related Author
YANG Dong
LI Zhiping
QI Lei
刘超
苏三买
汪天兴
陈永琴
SHI Jing-cheng
Related Institution
西安电子科技大学 机电工程学院
西北工业大学 动力与能源学院
Science and Technology on Space Physics Laboratory, China Academy of Launch Vehicle Technology, China Aerospace Science and Technology Corporation
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Department of Engine Engrneering, Aviation Industry Corporation of China