电脉冲除冰系统的结构力学性能分析

李广超; 何江; 林贵平

doi:10.13700/j.bh.1001-5965.2015.0609

电脉冲除冰系统的结构力学性能分析

doi: 10.13700/j.bh.1001-5965.2015.0609

1.
北京航空航天大学航空科学与工程学院, 北京 100083
2. 中国空间技术研究院, 北京 100081

基金项目: 航空科学基金（2013ZC51030）

详细信息

作者简介:
李广超,男,博士,副研究员。主要研究方向:流动控制、飞机除防冰。Tel.:010-82339235,E-mail:liguangchao@buaa.edu.cn

通讯作者:
李广超,Tel.:010-82339235,E-mail:liguangchao@buaa.edu.cn

中图分类号: V244.1⁺5
计量
- 文章访问数: 888
- HTML全文浏览量: 87
- PDF下载量: 356
- 被引次数: 0
出版历程
- 收稿日期: 2015-09-17
- 网络出版日期: 2016-10-20

Performance analysis on structural dynamics of EIDI system

1.
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
2. China Academy of Space Technology, Beijing 100081, China

Funds: Aeronautical Science Foundation of China (2013ZC51030)

摘要

摘要: 电脉冲除冰（EIDI）作为一种电动-机械式除冰系统，具有广阔的应用前景。本文采用线圈和金属平板组成的电脉冲系统作为EIDI结构动力学模型的研究对象，基于有限元分析软件MSC/NASTRAN，建立了一套针对典型平板-线圈结构的EIDI系统结构动力学仿真模型，研究了模型的固有特性（模态与频率）与时域响应分析，并开展了仿真模型的实验验证。研究了基于模型的EIDI系统结构动力学特性，重点关注最大应变和位移在空间的分布规律，并讨论了电容、电压等放电参数的影响。研究表明，电脉冲作用下，平板最大位移分布特性近似“马鞍型”，提升电容和电压可以增大脉冲力峰值和结构变形量，同时减小固定位置处的应变。
- 飞机防冰除冰 /
- 电脉冲除冰(EIDI) /
- 有限元分析 /
- 模态分析 /
- 应力-应变
Abstract: As an electromechanical de-icing system, electro-impulse de-icing (EIDI) technology has broad application prospect. In the present paper, structural dynamics characteristics of a simplified EIDI system consisting of coil and metal plate were numerically and experimentally studied. A finite element simulation model of an EIDI system was constructed, and the structural dynamics was analyzed by FEM software MSC/NASTRAN. The inherent characteristics (modal and frequency) as well as the transient response of the model were analyzed. The simulation was then validated by the experimental measurement. The structure dynamics characteristics of an EIDI model were studied. The maximum strain and displacement of the skin surface characteristic locations were evaluated with different capacitance, voltage and clearance between the skin and the coils. It is found that under the electro-impulse, the maximum displacement of the metal plate presents a saddle-like distribution. Increasing the capacitance and voltage will increase the impulse peak value and the structural deformation, and meanwhile, the strain of fixed location will be decreased.
- aircraft anti-icing and de-icing /
- electro-impulse de-icing (EIDI) /
- finite element analysis /
- modal analysis /
- stress-strain

HTML全文

参考文献(15)

[1]	钟长生,洪冠新.飞机翼面结冰对飞行特性影响的研究[J].航空科学技术,2004(3):32-34.ZHONG C S,HONG G X.Review about effects of lifting surface icing on aircraft flight characteristics[J].Aeronautical Science & Technology,2004(3):32-34(in Chinese).
[2]	LYNCH F T,KHODADOUST A.Effects of ice accretions on aircraft aerodynamics[J].Progress in Aerospace Sciences,2001,37(8):669-767.
[3]	KHATKHATE A A,SCAVUZZO R J,CHU M L.A finite element study of the EIDI system[C]//Proceedings of the 26th AIAA Aerospace Sciences Meeting.Reston:AIAA,1988:1-8.
[4]	THOMAS S K,CASSONI R P,MACARTHUR C D.Aircraft anti-icing and de-icing techniques and modeling[J].Journal of Aircraft,1996,33(5):841-854.
[5]	周莉,徐浩军,龚胜科.飞机结冰特性及防除冰技术研究[J].中国安全科学学报,2010,20(6):105-110.ZHOU L,XU H J,GONG S K.Research of aircraft icing characteristics and anti-icing and de-icing technology[J].China Safety Science Journal,2010,20(6):105-110(in Chinese).
[6]	BERNHART W D,GIEN P H.A structural dynamics investigation related to EIDI applications:AIAA-1986-0550[R].Reston:AIAA,1986.
[7]	ZUMWALT G W.Analysis and tests for design of an electro-impulse de-icing system:NASA/CR-1987-174919[R].Washington,D.C.:NASA,1987.
[8]	GIEN P H.Free vibration and transient analysis of a semi-cylinder subjected to electro-impulse de-icing forces[M].Wichita,Kansas:Wichita State University,1985:19-37.
[9]	SCAVUZZO R J,CHU M L.Finite element studies of the electro impulse de-icing system[J].Journal of Aircraft,1990,27(9):757-763.
[10]	LABEAS G N,DIAMANTAKOS I D,SUNARIC M M.Simulation of the electroimpulse de-icing process of aircraft wings[J].Journal of Aircraft,2006,43(6):1876-1885.
[11]	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[J].航空动力学报,2012,27(2):350-356.LI Q Y,ZHU C L,BAI T.De-icing experiment and numerical simulation of the electro-impulse de-icing system[J].Journal of Aerospace Power,2012,27(2):350-356(in Chinese).
[12]	李清英,朱春玲,白天.电脉冲除冰系统激励简化与影响因素[J].航空学报,2012,25(8):1384-1393.LI Q Y,ZHU C L,BAI T.Simplification of de-icing excitation and influential factors of the electro-impulse de-icing system[J].Acta Aeronautica et Astronautica Sinica,2012,25(8):1384-1393(in Chinese).
[13]	张文杰,董文俊,王斌团.电脉冲除冰仿真冰层松脱准则研究[J].计算机工程与应用,2012,48(3):232-233.ZHANG W J,DONG W J,WANG B T.Study on de-icing criterion of electro-impulse de-icing simulation[J].Computer Engineering and Applications,2012,48(3):232-233(in Chinese).
[14]	李广超,何江,林贵平.电脉冲除冰(EIDI)系统电动力学模型分析[J].航空动力学报,2011,26(1):54-59.LI G C,HE J,LIN G P.Research of electrodynamics in electro-impulse de-icing (EIDI) system[J].Journal of Aerospace Power,2011,26(1):54-59(in Chinese).
[15]	李广超,何江,林贵平.电脉冲除冰(EIDI)技术研究[J].航空动力学报,2011,26(8):1718-1735.LI G C,HE J,LIN G P.Electro-impulse de-icing(EIDI) technology study[J].Journal of Aerospace Power,2011,26(8):1718-1735(in Chinese).