Analysis and optimization of the pilot stage of jet pipe servo valve

被引:9
作者
Zhang, Ying [1 ]
机构
[1] Xian Technol Univ, Sch Optoeletron Engn, Xian 710021, Peoples R China
关键词
Jet pipe servo valve; Pilot stage; Finite volume method (FVM); Jet amplifier; FLOW; CAVITATION; SIMULATION;
D O I
10.1016/j.aej.2021.04.087
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Based on the principle of two-phase hydrodynamics and the mechanism of cavitation generation, this paper uses the finite volume method (FVM) in computational fluid dynamics (CFD) to analyse the features of fluid flow in jet amplifier, i.e., the pilot stage of jet pipe servo valve, and designs a lab bench to experimentally prove the accuracy of this numerical method. On this basis, the author discussed how four structural parameters influence the amplification efficiency of the jet amplifier. The amplification efficiency of the jet pipe servo valve can be maximized by setting the distance between nozzle and receiving holes of 0.1 mm, the diameter of receiving holes of 0.2 mm, the inclination angle of 22.5 degrees, and the spacing between the two receiving holes of 0 mm (if possible). The research methods and results provide a solid basis for the design and performance prediction of the jet pipe servo valve. (C) 2021 THE AUTHOR. Published by Elsevier BV on behalf of Faculty of Engineering, Alexandria University.
引用
收藏
页码:41 / 50
页数:10
相关论文
共 25 条
[1]  
Aldeek ZA, 2020, Int J Sustain Dev Plan, V15, P547, DOI [10.18280/ijsdp.150415, DOI 10.18280/IJSDP.150415]
[2]   Green architecture and sustainability in the complex transformation of the built urban environment in Jordan [J].
Aldeek Z.A.O. .
International Journal of Design and Nature and Ecodynamics, 2020, 15 (01) :113-120
[3]   Experimental Investigation of the Interaction of Fluid Transients with an In-Line Air Pocket [J].
Alexander, Jane M. ;
Lee, Pedro J. ;
Davidson, Mark ;
Li, Zhao ;
Murch, Ross ;
Duan, Huan-Feng ;
Meniconi, Silvia ;
Brunone, Bruno .
JOURNAL OF HYDRAULIC ENGINEERING, 2020, 146 (03)
[4]   Cavitation in Hydraulic Turbines [J].
Ayli, Ece .
INTERNATIONAL JOURNAL OF HEAT AND TECHNOLOGY, 2019, 37 (01) :334-344
[5]   Multidisciplinary design optimization of aircraft wing using commercial software integration [J].
Benaouali, Abdelkader ;
Kachel, Stanislaw .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 92 :766-776
[6]   A dual lane piezoelectric ring bender actuated nozzle-flapper servo valve for aero engine fuel metering [J].
Bertin, Michael ;
Plummer, Andrew ;
Bowen, Chris ;
Johnston, Nigel ;
Griffiths, Mike ;
Bickley, Dan .
SMART MATERIALS AND STRUCTURES, 2019, 28 (11)
[7]   3D flow simulation of a circular leading edge hydrofoil and assessment of cavitation erosion by the statistical evaluation of void collapses and cavitation structures [J].
Blume, Martin ;
Skoda, Romuald .
WEAR, 2019, 428 :457-469
[8]  
Chaabane R., 2020, MATH MODELL ENG PROB, V7, P421
[9]   Model Construction and Performance Degradation Characteristics of a Deflector Jet Pressure Servo Valve under the Condition of Oil Contamination [J].
Chu, Yuanbo ;
Yuan, Zhaohui ;
He, Xuegong ;
Dong, Zhichao .
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2021, 2021
[10]   Side Gust Effects on the Performance of a Supersonic Inlet with Bleed [J].
Halwas, Hussein K. ;
Aggarwal, Suresh .
JOURNAL OF AIRCRAFT, 2019, 56 (06) :2357-2370