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不同校准装置对引压管腔动态特性校准

李博 杨军 石玉松

李博, 杨军, 石玉松. 不同校准装置对引压管腔动态特性校准[J]. 航空动力学报, 2019, 34(12): 2559-2568. doi: 10.13224/j.cnki.jasp.2019.12.004
引用本文: 李博, 杨军, 石玉松. 不同校准装置对引压管腔动态特性校准[J]. 航空动力学报, 2019, 34(12): 2559-2568. doi: 10.13224/j.cnki.jasp.2019.12.004
LI Bo, YANG Jun, SHI Yusong. Calibration of dynamic characteristics of pressure tube cavity by different calibration devices[J]. Journal of Aerospace Power, 2019, 34(12): 2559-2568. doi: 10.13224/j.cnki.jasp.2019.12.004
Citation: LI Bo, YANG Jun, SHI Yusong. Calibration of dynamic characteristics of pressure tube cavity by different calibration devices[J]. Journal of Aerospace Power, 2019, 34(12): 2559-2568. doi: 10.13224/j.cnki.jasp.2019.12.004

不同校准装置对引压管腔动态特性校准

doi: 10.13224/j.cnki.jasp.2019.12.004
基金项目: 装备技术基础项目(JZX7J201802JL0022XX); 国家“十三五”技术基础项目(JSJL2015205B015)

Calibration of dynamic characteristics of pressure tube cavity by different calibration devices

  • 摘要: 为了探索引压管腔在动态压力校准中各校准方法的一致性与数据准确性,确立了以简单直管形式引压管腔开展动态特性校准的研究。采用理论和仿真的手段分析并建立了引压管腔模型,理论模型和仿真结果一致性极高。利用3种正弦压力校准装置对同一引压管腔进行了动态校准组合试验,结果表明:3种校准方法所得的动态特性与理论分析趋势一致,对于引压管腔基频的校准各试验之间偏差小于0.55%,但与基频理论值最大偏差为-3.17%。该研究将会为未来引压管腔结构设计和动态特性的补偿修正提供了一定参考依据。

     

  • [1] 李继超,王偲臣,林峰,等.一种容腔效应标定技术及其在高频响动态探针中的应用[J].航空动力学报,2011,26(12):2749-2756. LI Jichao,WANG Sichen,LIN Feng,et al.A technique to calibrate cavity effect in unsteady pressure probes with high frequency response[J].Journal of Aerospace Power,2011,26(12):2749-2756.(in Chinese)
    [2] PERSICO G,GAETANI P,GUARDONE A.Design and analysis of new concept fast-response pressure probes[J].Measurement Scienceand Technology,2005,16(9):1741-1750.
    [3] KANG J S,YANG S S.Fast-response total pressure probe for turbomachinery application[J].Journal of Mechanical Science and Technology,2010,24(2):569-574.
    [4] 郭勇,王效葵,王洪伟.高频压力探针动态性能的补偿方法[J].航空动力学报,2005,20(2):273-277. GUO Yong,WANG Xiaokui,WANG Hongwei.Improvement on dynamic characteristics of high response pressure probe[J].Journal of Aerospace Power,2005,20(2):273-277.(in Chinese)
    [5] 江勇.一种爆膜式动压测量校准系统[J].航空动力学报,1996,11(3):320-322. JIANG Yong.A broken film calibration system of dynamic pressure measurement[J].Journal of Aerospace Power,1996,11(3):320-322.(in Chinese)
    [6] 包家立.带引压管和容腔的压力传感器现场动态标定的探讨[J].仪器仪表学报,1990,11(1):65-71. BAO Jiali.A discussion of the dynamic calibration on the spot for pressure transducer with impulse tube and chamber[J].Chinese Journal of Scientific Instrument,1990,11(1):65-71.(in Chinese)
    [7] 任先贞,殷帅,裴东兴,等.膛压测试系统耗散型传压管道动态响应方法[J].探测与控制学报,2017,39(2):108-112. REN Xianzheng,YIN Shuai,PEI Dongxing,et al.Dissipation type dynamic response method of chamber pipeline pressure test system[J].Journal of Detection and Control,2017,39(2):108-112.(in Chinese)
    [8] 吕永志.压力测试取样管路系统动态特性分析及畸变信号的修正[D].太原:中北大学,2017. L Yongzhi.Analysis of dynamic characteristics of pressure sampling pipeline system and correction of distortion signal[D].Taituan:North University of China,2017.(in Chinese)
    [9] BROUCKAERT J F.Fast response aerodynamic probes for measurements in turbomachines[J].Proceedings of the Institution of Mechanical Engineers:Part A Journal of Power and Energy,2007,221(6):811-813.
    [10] 柳兆荣,陈金娥,黄东群.压力传感器频率响应的分析[J].力学学报,1980,16(4):363-372. LIU Zhaorong,CHEN Jine,HUANG Dongqun.An analysis of frequency responese of pressure transducer[J].Acta Mechanica Sinica,1980,16(4):363-372.(in Chinese)
    [11] MILLER E L,DUDENHOEFER J E.On the dynamic response of pressure transmission lines in the research of helium-charged free piston Stirling engines[R].Washington,DC,USA:the 24th Intersociety Energy Conversion Engineering Conference 1989.
    [12] WHITMORE S A,PETERSEN B J,SCOTT D D.A dynamic response model for pressure sensors in continuum and high knudsen number flows with large temperature[R].AIAA 96-0563,1996.
    [13] 徐有恒,黄东群.一种测试压力传感器容腔动态特性的简易方法[J].上海力学,1981(4):50-58. XU Youheng,HUANG Dongqun.A simple method for determining the dynamic characteristics of pressure transducer terminated at a chamber[J].Shanghai Mechanics,1981(4):50-58.(in Chinese)
    [14] 王维,唐磊,王棋.压力测试管道管腔效应研究[R].北京:第13届全国压力计量与测试技术学术交流会,2012.
    [15] 朱明武.动压测量[M].北京:国防工业出版社,1983.
    [16] 苏尔皇.管道动态分析及液流数值计算方法[M].哈尔滨:哈尔滨工业大学出版社,1985.
    [17] 周毅,顾明.并联管道耗散模型的理论研究[J].振动与冲击,2004,23(3):79-82. ZHOU Yi,GU Ming.Research on theoretical representation of dissipative model of parallel tube-manifold systems[J].Journal of Vibration and Shock,2004,23(3):79-82.(in Chinese)
    [18] 蔡亦钢.流体传输管道动力学[M].杭州:浙江大学出版社,1990.
    [19] 张东青,王烨.压力传感器动态测量方法的研究[J].传感器与微系统,2007,26(6):23-25. ZHANG Dongqing,WANG Ye.Research on dynamic measurement medthod for pressure transducer[J].Transducer and Microsystem Technologies,2007,26(6):23-25.(in Chinese)
    [20] PRYOR R W.Multiphysics modeling using COMSOL:a first principles approach[M].Burlington,MA,USA:Jones and Bartlett Publishers Incorporation,2011.
    [21] 王维新,谢壮宁.测压传压管路系统动态特性的试验分析[J].西北大学学报(自然科学版),2005,35(4):392-396. WANG Weixin XIE Zhuangning.Experimental investigation on the dynamic characteristics of tubing systems for fluctuating wind pressure measurements[J].Journal of Northwest University(Natural Science Edition),2005,35(4):392-396.(in Chinese)
    [22] YANG Jun,WANG Yufang,LI Cheng.Dynamic modeling of pressure pipelines and signal reconstruction[R].Beijing:the 1st International Conference on Instrumentation,Measurement,Computer,Communication and Control,2011.
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出版历程
  • 收稿日期:  2019-05-31
  • 刊出日期:  2019-12-28

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