Volume 37 Issue 3
Mar.  2022
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2022  >  37(3): 449-456
XIAO Chunhua, WANG Hongwei, QIAO Baoying, XIE Xiaohui, ZHAO Dan. Hybrid ice detection system based on light intensity reflection and piezoelectric vibration[J]. Journal of Aerospace Power, 2022, 37(3): 449-456. doi: 10.13224/j.cnki.jasp.20200470
Citation: XIAO Chunhua, WANG Hongwei, QIAO Baoying, XIE Xiaohui, ZHAO Dan. Hybrid ice detection system based on light intensity reflection and piezoelectric vibration[J]. Journal of Aerospace Power, 2022, 37(3): 449-456. doi: 10.13224/j.cnki.jasp.20200470
shu

Hybrid ice detection system based on light intensity reflection and piezoelectric vibration

doi: 10.13224/j.cnki.jasp.20200470
  • 1.

    Low Speed Aerodynamics Institute，China Aerodynamics Research and Development Center，Mianyang Sichuan 621000，China

  • 2.

    Sichuan Aerospace Measurement and Test Research Institute，Sichuan Academy of Aerospace Technology，China Aerospace Science and Technology Corporation，Chengdu 610100，China

  • Received Date: 2020-11-04
  • Publish Date: 2022-03-28
    Abstract
  • There are some problems such as single-point measurement，inaccurate measurement and mismatching positions for current ice detection system of airplane.The optic fiber ice detection sensor was developed by the light intensity reflection method.And the flat film ice detection sensor was manufactured by the piezoelectric vibration method.These two were embedded into a NACA0012 airfoil.Thus a hybrid ice detection system suitable for airfoil surface and multi-point distributed measurement was developed，which was tested in cold storage and icing wind tunnel.It showed that，the hybrid ice detection system of multi-point distribution measurement can not only have the advantages of optic fiber ice detection and flat film ice detection，but also achieve ice detection on airfoil surface.The response time was less than 0.5 s and the measurement range of ice thickness was from 0.2 mm to 3 mm.The reliability of hybrid ice detection system was better than that of ice detection rod of single-point measurement，proving it is a novel and prospective ice detection technology.

     

    • FullText(HTML)
  • loading
    • References(20)
  • [1]
    KIND R J,POTAPCZUK M G,FEO A,et al.Experimental and computational simulation of in-flight icing phenomena[J].Progress in Aerospace Sciences,1998,34（5/6）:275-345.
    [2]
    BRAGG M B,BROEREN A P,BLUMENTHAL L A.Iced-airfoil aerodynamics[J].Progress in Aerospace Science,2005,41（5）:323-362.
    [3]
    肖春华,桂业伟,易贤,等.结冰翼型表面明冰的压力分布和应力计算[J].航空动力学报,2009,24（7）:1457-1463.
    [4]
    肖春华，于昆龙，陈辅政，等.结冰环境下结冰/除冰过程的气动参数测量实验技术[J].航空动力学报,2018,33（12）:2817-2826.
    [5]
    US Department of Transportation Federal Aviation Administration.Aircraft ice protection[R].FAA AC20-73A,2006.
    [6]
    张杰,周磊,张洪,等.飞机结冰探测技术[J].仪器仪表学报,2006,27（12）:1582-1583.
    [7]
    王华,王以伦,张滨华.基于磁致伸缩原理的结冰传感器设计理论[J].电工技术学报,2003,18（6）:77-80.
    [8]
    王华,张滨华,王以伦,等.结冰传感器的温度补偿[J].传感器技术,2002,21（10）:31-33.
    [9]
    SAE Society of Automotive Engineers.Aircraft inflight ice detectors and icing rate measuring instruments[R].AIR 4367A:1-22,2012.
    [10]
    朱程香,孙志国,付斌,等.探头式结冰探测器安装位置分析[J].航空动力学报,2011,26（12）:2676-2683.
    [11]
    李盼,朱家乐.FAR25第129号修正案对结冰探测系统的影响研究[J].飞机设计,2018,38（1）:76-80.
    [12]
    张龙浩.光纤阵列式结冰探测系统的研究[D].武汉：华中科技大学,2013.
    [13]
    IKIADES A A,ARMSTRONG D J,HARE G G,et al.Fiber optic sensor technology for air conformal ice detection[J].Industrial and Highway Sensors Technology,2004,5272:357-368.
    [14]
    IKIADES A A,ARMSTRONG D J,HOWARD G.Optical diffusion and polarization characteristics of ice accreting in dynamic conditions using a backscattering fiber optic technique[J].Sensors and Actuators,2007,140（1）:43-50.
    [15]
    ZHAO Z Q.Modulation function of the reflective optical fiber sensor for peculiar and diffuse reflection[J].Optical Engineering,1994,33（9）:2986-2991.
    [16]
    李薇,侯睿,程立.基于忆阻桥效应的光纤式双光路结冰探测方法[J].传感技术学报,2017,30（2）:206-210.
    [17]
    PIMPEC M L.Ultrasonic technology:a solution for in-flight and on-ground ice detection[R].Melbourne,Australia:21st Congress of International Council of the Aeronautical Sciences,1992.
    [18]
    ROY S,IZAD A,RUSSELL G D,et al.Smart ice detection systems based on resonant piezoelectric transducers[J].Sensors and Actuators A,1998,69（3）:243-250.
    [19]
    叶林.基于压电器件的冰传感器[J].仪表技术与传感器,2001（9）:6-7.
    [20]
    张洪,邢科新,张杰,等.平膜压电谐振式结冰传感器信号检测方法[J].仪表技术与传感器,2006（4）:6-11.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF(1397.0KB)
    XML

    Article Metrics

    Article views (622) PDF downloads(108) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return