The pressure reducing regulator which was the key point of turbo-pump gas-sealed decompressing experiment system was optimized by PSO(particle swarm optimization).Uniform design was used twice before the optimization for the sake of reducing computing quantity.The structure parameters of pressure reducing regulator were optimized to obtain steady outlet pressure meeting engineering requirement.The result indicates that the range of variables was compressed availably through twice of the uniform design.Compared with initial point
the swing of outlet pressure decreases obviously according with engineering design.
A multi cycle propulsion system for amphibious unmanned aerial vehicle with repeatable water exit
Cavitation modeling and start⁃up under⁃rated pressure simulation of liquid rocket engine
Predicting method of safety life of reusable liquid rocket engine turbopump
Failure mechanism and improvement of ball bearing in aliquid rocket engine turbopump
Fault diagnosis of liquid rocket engine based on comprehensive fuzzy clustering algorithm
Related Author
Jun TIAN
Yufan XIE
Fei LONG
Qin LIU
Yidan CHEN
Hongyu CHEN
Yazhou LIU
Shijie LIU
Related Institution
China Special Vehicle Research Institute,Aviation Industry Corporation of China,Limited
Airport Support Bureau,Air Force Logistics Department
Nanjing Puguo Technology Company,Limeted
National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
Laboratory of Science and Technology on Cryogenic Liquid Propulsion,Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation