电脉冲除冰系统的除冰实验与数值模拟

李清英; 朱春玲; 白天

电脉冲除冰系统的除冰实验与数值模拟

南京航空航天大学航空宇航学院, 南京 210016

基金项目: 国家自然科学基金(10972106)

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出版历程
- 收稿日期: 2011-08-01
- 修回日期: 2011-12-21
- 刊出日期: 2012-02-28

De-icing experiment and numerical simulation of the electro-impulse de-icing system

College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

摘要

摘要: 搭建了电脉冲除冰实验台,完成了脉冲放电500V时的除冰实验,获得了三次除冰激励后的除冰效果.同时,为数值模拟除冰过程,求解了除冰动力即铝板在涡流场作用下的脉冲压力分布,建立了冰-铝板三维有限元分析模型,利用ANSYS单元生死技术瞬态非线性分析了冰层的失效单元,比较了Labeas冰层失效准则与第一强度理论分析冰层失效的效果.结果表明:加载除冰激励后,利用第一强度理论数值仿真去除冰层范围的结果更符合本次除冰实验.
- 电脉冲除冰系统 /
- 除冰实验 /
- 除冰激励 /
- 单元生死 /
- 冰层失效
Abstract: An electro-impulse de-icing system was developed to undertake the de-icing experiments.De-icing occurred when the circuit was trigged three times with the discharge voltage 500V.Meanwhile,the de-icing excitation exerting on the aluminum plate was numerically simulated in the eddy current field.A three dimensional finite model of ice and aluminum plate was introduced to analyze the ice failure in the nonlinear transient method by killing elements of the ANSYS FE(finite element) code.The ice failure criterion was checked by comparing the Labeas de-icing criterion with the first strength theory.It concludes that the latter is more suitable for simulating the de-icing process by loading the de-icing excitation in this test.
- electro-impulse de-icing system /
- de-icing test /
- de-icing excitation /
- kill elements /
- ice failure

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参考文献(15)

[1]	Thomas S K,Cassoni R P.Aircraft anti-icing and de-icing techniques and modeling[J].Journal of Aircraft,1996,3(5):841-854.
[2]	Zumwalt G W,Schrag R L,Bernhart W D,et al.Electro-impulse de-icing testing analysis and design.NASA CR-4175,1988.
[3]	裘燮纲,郭宪民.电脉冲除冰系统参数的合理选择[J].南京航空航天大学学报,1993,25(2):211-217. QIU Xiegang,GUO Xianmin.Parameter selection of electro-impulse de-icing systems[J].Journal of Nanjing University of Aeronautics and Astronautics,1993,25(2):211-217.(in Chinese)
[4]	李清英,白天,朱春玲.电脉冲除冰系统的电磁场分析[J].南京航空航天大学学报,2011,43(1):95-100. LI Qingying,BAI Tian,ZHU Chunling.Electromagnetic field analysis for electro-impulse de-icing system[J].Journal of Nanjing University of Aeronautics and Astronautics,2011,43(1):95-100.(in Chinese)
[5]	Scavuzzo R J,Chu M L,Kellackey C J.Impact ice stresses in rotating airfoils[J].Journal of Aircraft,1990,28(7):450-455.
[6]	Smith S O.Modeling and strain gauging of eddy current repulsion deicing systems.AIAA 93-0296,1993.
[7]	Labeas G N,Diamantakos I D,Sunnaric M M.Simulation of the electroimpulse de-icing process of aircraft wings[J].Journal of Aircraft,2006,43(6):1876-1885.
[8]	Xian X,Chu M L,Scavuzzo R J,et al.An experimental evaluation of the tensile strength of impact ice[J].Journal of Materials Science of Materials Science Letters,1989,8(10):1205-1208.
[9]	Reich A D.Ice property/structure variations across the glaze/rime transition.AIAA 92-0296,1992.
[10]	Cole D M.Reversed direct-stress testing of ice:initial experimental results and analysis[J].Cold Regions Science and Technology,1990,18(3):303-321.
[11]	Gupta V,Bergstrom J S.A progressive damage model for failure by shear faulting in polycrystalline ice under biaxial compression[J].International Journal of Plasticity,2002,18(4):507-530.
[12]	Arccher P,Gupta V.Measurement and control of ice adhesion to aluminum 6061 alloy[J].The Journal of the Mechanics and Physics of Solids,1998,46(10):1745-1771.
[13]	Kandagal S B,Venkatraman K.Piezo-actuated vibratory deicing of a flat plate.AIAA 2005-2115,2005.
[14]	Zhu Y,Palacios J L,Rose J L,et al.De-icing of multi-layer composite plates using ultrasonic guided waves.AIAA 2008-1862,2008.
[15]	李围.ANSYS土木工程应用实例[M].北京:中国水利水电出版社,2007.