Full Text:
<1093>
Summary: 
<468>
CLC number:
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
Crosschecked: 2022-10-21
Cited: 0
Clicked: 3103
Three-dimensional flow field mathematical model inside the pilot stage of the deflector jet servo valve
| ||||||||||||||
Shuang-lu LI, Yao-bao YIN, Jiang-yang YUAN, Sheng-rong GUO. Three-dimensional flow field mathematical model inside the pilot stage of the deflector jet servo valve[J]. Journal of Zhejiang University Science A, 2022, 23(10): 795-806.
@article{title="Three-dimensional flow field mathematical model inside the pilot stage of the deflector jet servo valve",
author="Shuang-lu LI, Yao-bao YIN, Jiang-yang YUAN, Sheng-rong GUO",
journal="Journal of Zhejiang University Science A",
volume="23",
number="10",
pages="795-806",
year="2022",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A2200030"
}
%0 Journal Article
%T Three-dimensional flow field mathematical model inside the pilot stage of the deflector jet servo valve
%A Shuang-lu LI
%A Yao-bao YIN
%A Jiang-yang YUAN
%A Sheng-rong GUO
%J Journal of Zhejiang University SCIENCE A
%V 23
%N 10
%P 795-806
%@ 1673-565X
%D 2022
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A2200030
TY - JOUR
T1 - Three-dimensional flow field mathematical model inside the pilot stage of the deflector jet servo valve
A1 - Shuang-lu LI
A1 - Yao-bao YIN
A1 - Jiang-yang YUAN
A1 - Sheng-rong GUO
J0 - Journal of Zhejiang University Science A
VL - 23
IS - 10
SP - 795
EP - 806
%@ 1673-565X
Y1 - 2022
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.A2200030
Abstract: A new flow field mathematical model is proposed to describe accurately the flow field structure and calculate the static characteristics of the pilot stage in a deflector jet servo valve (DJSV). The flow field is divided into five regions, a 3D turbulent jet is adopted to describe the free jet region, and a velocity distribution expression of the jet is proposed. The jet entrainment model is put forward in the pressure recovery region to describe the coupling relationship between the pressure in the receiving chamber and the jet flow. The static characteristics, including pressure-flow characteristics, pressure characteristics, and flow characteristics of the pilot stage are obtained. The flow field structure and the static characteristics are verified by finite element analysis (FEA) and experiment, respectively, and the mathematical model results are in good agreement with the experimental and simulation results.
[1]KarunanidhiS, SingaperumalM, 2010. Mathematical modelling and experimental characterization of a high dynamic servo valve integrated with piezoelectric actuator. Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 224(4):419-435.
[2]LiYS, 2016. Mathematical modelling and characteristics of the pilot valve applied to a jet-pipe/deflector-jet servovalve. Sensors and Actuators A: Physical, 245:150-159.
[3]LiuXQ, JiH, MinW, et al., 2020. Erosion behavior and influence of solid particles in hydraulic spool valve without notches. Engineering Failure Analysis, 108:104262.
[4]LiuYS, DongJ, WuS, et al., 2019. Theoretical research on the dynamic characteristics of electrohydraulic servo valve (EHSV) in deep sea environment. Ocean Engineering, 192:105957.
[5]MarstersGF, 1981. Spanwise velocity distributions in jets from rectangular slots. AIAA Journal, 19(2):148-152.
[6]SahaBK, LiSJ, LvXB, 2020a. Analysis of pressure characteristics under laminar and turbulent flow states inside the pilot stage of a deflection flapper servo-valve: mathematical modeling with CFD study and experimental validation. Chinese Journal of Aeronautics, 33(3):1107-1118.
[7]SahaBK, PengJH, LiSJ, 2020b. Numerical and experimental investigations of cavitation phenomena inside the pilot stage of the deflector jet servo-valve. IEEE Access, 8:64238-64249.
[8]SangiahDK, PlummerAR, BowenCR, et al., 2013. A novel piezohydraulic aerospace servovalve. Part 1: design and modelling. Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 227(4):371-389.
[9]SforzaPM, SteigerMH, TrentacosteN, 1966. Studies on three-dimensional viscous jets. AIAA Journal, 4(5):800-806.
[10]SquireHB, TrouncerJ, 1944. Round Jets in a General Stream. Aeronautical Research Council, Reports and Memoranda No. 1974, London, UK.
[11]StefanskiF, MinorowiczB, PerssonJ, et al., 2017. Non-linear control of a hydraulic piezo-valve using a generalised Prandtl–Ishlinskii hysteresis model. Mechanical Systems and Signal Processing, 82:412-431.
[12]TamburranoP, PlummerAR, DistasoE, et al., 2018. A review of electro-hydraulic servovalve research and development. International Journal of Fluid Power, 20(1):53-98.
[13]TamburranoP, PlummerAR, de PalmaP, et al., 2020. A novel servovalve pilot stage actuated by a piezo-electric ring bender: a numerical and experimental analysis. Energies, 13(3):671.
[14]YanH, RenYK, YaoL, et al., 2019. Analysis of the internal characteristics of a deflector jet servo valve. Chinese Journal of Mechanical Engineering, 32(2):31.
[15]YinYB, YuanJY, GuoSR, 2017. Numerical study of solid particle erosion in hydraulic spool valves. Wear, 392-393:174-189.
[16]YinYB, LiSL, ZhangXW, et al., 2019. Steady-state flow force calculation of the first stage in a deflector jet servo valve. IEEE 8th International Conference on Fluid Power and Mechatronics, p.452-458.
[17]ZhengFX, LiS, DingC, et al., 2021. Theoretical and experimental research on the cartridge two-dimensional (2D) electro-hydraulic servo valve. Advances in Mechanical Engineering, 13(2):168781402199653.
[18]ZhuMZ, ZhaoSD, DongP, et al., 2018. Design and analysis of a novel double-servo direct drive rotary valve with high frequency. Journal of Mechanical Science and Technology, 32(9):4313-4323.
ORCID: 
Open peer comments: Debate/Discuss/Question/Opinion
<1>