期刊文献+

基于可靠性的飞机风挡抗鸟撞优化设计 被引量:1

Reliability-Based Optimization Design of Aircraft Windshield for Resisting Bird Impact
下载PDF
导出
摘要 传统的飞机风挡设计通常在确定的工况下进行,未能充分考虑实际鸟撞风挡过程中不确定性因素的影响,导致飞机鸟撞风挡的故障多发。综合考虑鸟撞飞机风挡过程中鸟体材料参数、质量、撞击速度等不确定因素的影响,以飞机风挡抗鸟撞的可靠度为约束,风挡质量为目标,基于双循环方法和近似技术建立了风挡抗鸟撞可靠性优化设计系统,利用一阶矩法进行可靠性分析,对某飞机风挡进行了基于可靠性的优化设计。实例分析证明所建风挡抗鸟撞可靠性优化设计系统可行有效。 Traditional methods for aircraft windshield design are carried out based on determinate work condition.The effect of uncertainty factors during the process of windihield impacted by bird are not fully considered,so this result in low reliability of windshield performance.The effects of uncertainty factors into as bird body material paraineters,mass and inpact velocity during the process of windshield impacted by bird are considered.Reliability-based optimization design of windshield for resisting bird impact is set up according to the reliability of aircraft windshield for resisting bird impact and the windshield quality based on the double loop strategy and the approximation technique.The reliatility analysis is carried out by using the first-order reliability method.The reliability-based optimization design of aircraft wind shield for resinting bird impact is made.It is proved that this optimization design is feasible.
机构地区 西北工业大学
出处 《航空制造技术》 北大核心 2012年第11期93-95,共3页 Aeronautical Manufacturing Technology
关键词 飞机风挡 鸟撞 可靠性设计优化 一阶矩法 近似技术 Aircraft windshield Bird impact Reliability-based optimization design First-order reliability method Approximation technique
  • 相关文献

参考文献11

  • 1Chen X G;Hasselman T K;Neill D J.Reliability based structural design optimization for practical applications,1997.
  • 2屈滋培.可靠性工程,2000.
  • 3王富生,岳珠峰,冯震宙,王新军.鸟撞飞机风挡动态响应数值模拟方法研究现状[J].飞机设计,2008,28(5):39-46. 被引量:11
  • 4李磊,虞跨海,毛坤,岳珠峰.多学科设计优化在飞机座舱透明件设计中的应用[J].机械设计,2010,27(11):69-72. 被引量:4
  • 5Turcotte J;Trepanier J Y;Tribes C.Integration and multidisciplinary design optimization of a simplified gas turbine model using perl and isight.AIAA 2004-4425.
  • 6Perez R E;Liu Hugh H T;Behdinan K.Evaluation of multidisciplinary optimization approaches for aircraft conceptual design.AIAA 2004-4537.
  • 7Du X P;Sudjianto A;Chen W.An integrated framework for optimizaion under uncertainty using inveerse reliability strategy,2004.
  • 8Du X;Chen W.Sequential optimization and reliability assessment for probabilistic design,2004(02).
  • 9李磊;李元生;于明.船用大功率柴油机涡轮增压器多学科设计优化,2011.
  • 10原薇.基于可靠性的多学科设计优化,2004.

二级参考文献42

共引文献52

同被引文献13

  • 1王文智,万小朋,郭葳.民机风挡结构抗鸟撞仿真分析与设计[J].西北工业大学学报,2009,27(4):481-485. 被引量:5
  • 2黄创盛,姚进,Chuang-sheng.飞机风挡玻璃弯曲成形回弹数值模拟[J].机械设计与制造,2010(12):183-185. 被引量:3
  • 3罗华,侯力,郭祚达,谭永健.锥面风挡玻璃弯曲成型控制方法[J].四川大学学报(工程科学版),2007,39(2):170-174. 被引量:2
  • 4Wang Fusheng,Yue Zhufeng. Numerical simulation of damage and failure in aircraft windshield structure against bird strike[J].Materials and Design,2010,(02):687-695.
  • 5Grimaldi A,Sollo A,Guida M,Marulo F. Parametric study of a SPH high velocity impact analysis-A birdstrike windshield application[J].Computers & Structures,2013.616-630.
  • 6Heimbs S. Computational methods for bird strike simulations:A review[J].Computers & Structures,2011,(23-24):2093-2112.
  • 7Hinke L,Pichler L,Pradlwarter H J,Mace B R Waters T P. Modeling of spatial variations in vibration analysis with application to an automotive windshield[J].Finite Elements in Analysis and Design,2011,(01):55-62.
  • 8Xu Jun,Li Yibing,Chen Xi,Yan Yuan Ge Dongyun Zhu Mengyi Liu Bohan. Characteristics of windshield cracking upon low-speed impact:Numerical simulation based on the extended finite element method[J].COMPUTATIONAL MATERIALS SCIENCE,2010,(03):582-588.
  • 9Timmel M,Kolling S,Osterrieder P,Du Bois P A. A finite element model for impact simulation with laminated glass[J].International Journal of Impact Engineering,2007,(08):1465-1478.
  • 10Daoudi J,Irving E,Ports N. Multivariable predictive control of a laminated windshield bending furnace[J].Control Engineering Practice,1996,(07):909-914.

引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部