航空学报 > 1986, Vol. 7 Issue (6): 531-538

飞机损伤容限和耐久性设计技术的发展

李克唐   

  1. 成都飞机公司发展部
  • 收稿日期:1986-02-20 修回日期:1900-01-01 出版日期:1986-12-25 发布日期:1986-12-25

DEVELOPMENT OF DAMAGE TOLERANCE AND DURABILITY DESIGN TECHNOLOGY

Li Ketang   

  1. Development Department, Chengdu Aircraft Company
  • Received:1986-02-20 Revised:1900-01-01 Online:1986-12-25 Published:1986-12-25

摘要:

本文评介并讨论了以下问题:两类经验教训;设计思想的发展——五种模式;损伤容限和耐久性设计技术的特征;飞机设计应用实例;需要进一步研究的若干问题。

Abstract:

In this paper, The following problems are reviewed and discussed: Two kinds of experiences and lessons; Development of design conceptionr Characteristics of damage tolerance and durability design technology; practical examples in aircraft design; Some problems to be further studied.