Research on the Inlet Pressure Accurate Control Method of the Nozzle for the Single-Jet Nozzle Tester of Aero Engine

被引:0
|
作者
Wang, Yemu [1 ]
Wang, Jie [1 ]
机构
[1] Shenyang Univ Technol, Mech Engn Inst, Shenyang, Peoples R China
来源
关键词
Closed loop pressure control; PID control; Nozzle; Proportional relief valve; Fixed throttle hole;
D O I
10.4028/www.scientific.net/AMR.468-471.980
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper introduces the closed loop pressure computer control system which is suitable for the environment of kerosene medium. The system can satisfy the technical requirements of the pressure regulation in the test of the single -jet nozzle of aero engine, the pressure can be accurately controlled and its control precision is within +/- 0.01 MPa. It indicates the principle and composition of the hydraulic system and computer measurement and control system. The paper introduces the design method and treatment process of the key technology, which includes the use of a proportional relief valve and a fixed throttle hole in hydraulic system, the use of PID control in closed loop control system, the use of high precision sensor and measurement method by grade in measuring system and the use of 24V precision steady voltage source. In the same time it indicates the actual application of the closed loop pressure control system.
引用
收藏
页码:980 / 983
页数:4
相关论文
共 50 条
  • [21] Research on test method of high pressure water descaling nozzle performance
    Shi, XJ
    Zhou, DF
    Si, JS
    Shao, JP
    ISTM/2005: 6th International Symposium on Test and Measurement, Vols 1-9, Conference Proceedings, 2005, : 4330 - 4333
  • [22] Analysis of Low-Pressure Turbine Nozzle Guide Vane Failure in an Aero Gas Turbine Engine: A Computational Approach
    D. Arul Kumaresan
    R. K. Mishra
    Journal of Failure Analysis and Prevention, 2019, 19 : 504 - 510
  • [23] Analysis of Low-Pressure Turbine Nozzle Guide Vane Failure in an Aero Gas Turbine Engine: A Computational Approach
    Kumaresan, D. Arul
    Mishra, R. K.
    JOURNAL OF FAILURE ANALYSIS AND PREVENTION, 2019, 19 (02) : 504 - 510
  • [24] Research on Quality Control Method of Hydrogen Nozzle Based on Machine Learning
    Zhang, Ze
    Zhao, Hongjie
    Zhang, Suyan
    Bi, Kai
    Yang, Bing
    2024 5TH INTERNATIONAL CONFERENCE ON COMPUTER ENGINEERING AND APPLICATION, ICCEA 2024, 2024, : 1408 - 1411
  • [25] Control law of passive fluid thrust vector nozzle based on thermal jet of micro turbojet engine
    Gong D.
    Gu Y.
    Zhou Y.
    Shi N.
    Gu, Yunsong (yunsonggu@nuaa.edu.cn), 1600, Chinese Society of Astronautics (41):
  • [26] Optimization of aero-engine nozzle control schedule under the maximum dry thrust condition based on installation performance
    Xie, Y.-P., 1600, Beijing University of Aeronautics and Astronautics (BUAA) (29):
  • [27] COMPUTATION OF LIQUID FUEL ATOMIZATION AND MIXING BY MEANS OF THE SPH METHOD: APPLICATION TO A JET ENGINE FUEL NOZZLE
    Dauch, T.
    Braun, S.
    Wieth, L.
    Chaussonnet, G.
    Keller, M.
    Koch, R.
    Bauer, H. -J.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 4A, 2016,
  • [28] Ultrahigh Pressure Nozzle Speed Optimization Research Based on the Characteristics of Water Jet Cutting Sound
    Zhang Jun
    Chen Dengqian
    Zhao Dean
    Li Xuefeng
    Zhao Mingyang
    2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 8076 - 8081
  • [29] High pressure water jet cutting sound feature extraction and nozzle traverse speed control
    Zhao, D. (dazhao@mail.ujs.edu.cn), 1600, Chinese Mechanical Engineering Society (49):
  • [30] Single Neuron PID Control of a Turbofan Engine with Inlet Pressure Distortion
    Wang, Bin
    Wang, Xi
    Liu, Yue
    MATERIALS PROCESSING AND MANUFACTURING III, PTS 1-4, 2013, 753-755 : 1534 - 1538