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飞机易损性模型简化方法研究 被引量:5

Research on the Simplification of Aircraft Vulnerability Models
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摘要 针对工程应用中飞机零部件数目庞大导致易损性计算耗时长的问题,提出了3种飞机模型简化方法:产品封装法、等效法和修正法。产品封装法主要用于飞机系统部件的简化,等效法主要用于飞机结构部件的模型简化,修正法则用于飞机全机模型的简化。经过简化后的飞机模型,部件数目在300以内。使用飞机易损性评估方法计算模型简化后的飞机易损性,其计算耗时大约是不简化的0.5%,可满足工程实际应用。 Three methods for the simplification of aircraft vulnerability models are proposed in this paper for resolving the problem that the vulnerability calculation of actual aircraft is time-consuming because of the large number of the parts on the aircraft. They are product packaging method, equivalent method and modified method. The simplification of the system components and the structure use the product packaging method and the equivalent method separately, the modified method is used for the simplification of the all aircraft models. The components number of the aircraft models which will be simplification is 300. The time for calculating the vulnerability of the simplification aircraft is only 0.5% of the actual aircraft, it meets the requirement for the engineering application.
出处 《机电一体化》 2011年第10期36-40,共5页 Mechatronics
基金 教育部博士点基金(No.200806991002)
关键词 易损性 飞机 模型 简化 vulnerability aircraft models simplification
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参考文献5

  • 1Robert E Ball.飞机作战生存力分析与设计基础[M].林光宇,宋笔锋.北京:航空工业出版社,1998.
  • 2BALL R E. The fundamentals of aircraft combat survivability analysis and design [ M ]. First edition. New York: American Institute of Aeronautics and Astronautics, 1985.
  • 3BALL R E. The fundamentals of aircraft combat survivability analysis and design [ M ]. Second edition. California: American Institute of Aeronautics and Astronautics, 2003.
  • 4裴扬,宋笔锋,韩庆.基于等效靶方法的飞机单击中易损性通用计算模型(英文)[J].Chinese Journal of Aeronautics,2006,19(3):183-189. 被引量:11
  • 5裴扬,宋笔锋,李占科.飞机易损性评估的基本方法研究[J].弹箭与制导学报,2004,24(2):70-74. 被引量:12

二级参考文献17

  • 1裴扬,宋笔锋,韩庆.基于有限元模型的飞机几何描述算法研究[J].西北工业大学学报,2004,22(5):567-571. 被引量:9
  • 2裴扬 宋笔锋 李占科.一种基于DMECA的飞机致命性部件辩识软件[J].机械科学与技术,2004,23:109-112.
  • 3MIL-HDBK-336-2,Survivability aircraft nonnuclear airframe[S].Washington DC:Dept of Defense,1983.
  • 4GJB/Z202-2001,飞机非核生存力通用指南[S].北京:国防科工委军标出版发行部出版,2002.
  • 5MIL-HDBK-336-1,Survivability aircraft nonnuclear general criteria[S].Washington DC:Dept of Defense,1988.
  • 6Ball R E.The fundamentals of aircraft combat survivability analysis and design[M].2nd ed.Reston:AIAA,2003.
  • 7宋笔锋 韩庆.飞机易损性指标计算的基本理论与方法(Ⅰ)[J].现代防御技术,1999,27(4):38-45.
  • 8Kiwan A R.An overview of High-Explosive (HE) blast damage mechanisms and vulnerability prediction methods[R].ARL-TR-1468,1997.
  • 9魏惠之,朱鹤松.米-24D武装直升机等效靶研究[R].GF85786,1992.
  • 10朱鹤松,高世泽.武装直升机易损性分析[R].GF85783,1992.

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