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老龄飞行器机体结构的损伤性分析 被引量:1

Structure Damage Analysis of an Aging Aircraft
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摘要 对服役状态下飞行器机体结构损伤进行了分析,并给出了开展机体结构损伤分析的一个总体思路。介绍了对老龄化机体结构所进行的修理、遭受的腐蚀损伤和广布疲劳损伤情况,探讨了这些情况对机体结构所造成的影响。最后通过具体实例分析了腐蚀及广布疲劳损伤对结构危险性的影响。 Damage analysis ing aircraft damage analysis tigue damages in an aircraft safety was studied. Finally, tigue damages on structural of the structure of a serving aircraft was carried out, and an overall methodology for ag- was presented. The relevant situations of repairs, corrosion damages and widespread fastructure were described, and the effect of the three situations on aged aircraft structure a numerical example was given to investigate the effect of corrosion and widespread fa-tigue damages on structural on structural risk.
出处 《机械科学与技术》 CSCD 北大核心 2009年第2期273-275,280,共4页 Mechanical Science and Technology for Aerospace Engineering
关键词 老龄飞行器 损伤分析 腐蚀 广布疲劳 危险性 aging aircraft damage analysis corrosion widespread fatigue damage structural risk
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参考文献5

  • 1陈跃良.腐蚀对现役飞机结构剩余强度的影响[D].西安:西北工业大学,2004.
  • 2Miedlar P C, Berens A P. USAF Damage Tolerant Design Handbook: Guidelines for the Analysis and Design of Damage Tolerant Aircraft Structures [ D ]. AFRL-VA-WP-TR- 2003-3002,2002
  • 3Brooks C L, Honeycutt K, Prost-Domasky S. Case studies for corrosion/fatigue life assessments [ A]. Fourth Joint NASA/FAA/ DoD Conference on Aging Aircraft[ C], St. Louis, Missouri, May 2000
  • 4Swift T. Unarrested fast fracture of metal aircraft structures [ A ]. Proceedings of the International Workshop on Structural Integ. rity of Aging Aircraft[ C], Atlanta Technology Publications, 1992
  • 5Alford R E, Bell R P, Cochran J B. C-141 WS 405 risk assessment [ A]. Proceedings of the 1991 USAF Structural Integrity Program Conference[ C], San Antonio, Texas. 1992

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