飞机蒙皮典型搭接结构附加弯矩分析
详细信息    查看全文 | 推荐本文 |
  • 英文篇名:SECONDARY BENDING ANALYSIS OF AIRPLANE TYPICAL SINGLE-SHEAR LAP JOINT
  • 作者:杨静 ; 姜兴长 ; 王慧梅
  • 英文作者:YANG Jing;JIANG XingChang;WANG HuiMei;AVIC Aircraft XifeiCommercial Aircraft Co.Ltd.;
  • 关键词:搭接结构 ; 附加弯矩 ; 一维平板壳模型 ; 模型验证
  • 英文关键词:Single-shear lap joint;;The secondary bending;;The flat shells method;;Method validation
  • 中文刊名:JXQD
  • 英文刊名:Journal of Mechanical Strength
  • 机构:中航西飞民用飞机有限责任公司;
  • 出版日期:2019-04-08
  • 出版单位:机械强度
  • 年:2019
  • 期:v.41;No.202
  • 语种:中文;
  • 页:JXQD201902021
  • 页数:4
  • CN:02
  • ISSN:41-1134/TH
  • 分类号:138-141
摘要
蒙皮典型搭接结构是飞机进行疲劳设计的重要结构件之一,其附加弯矩分析一直受到工程上的广泛关注。采用一维平板壳单元,通过合理的模型建立,飞机机身蒙皮典型搭接结构进行分析,计算得到搭接结构各疲劳细节点所应附加弯矩。同时还一维平板壳模型进行了验证,证实其计算的有效性。所得附加弯矩计算结果飞机机身蒙皮典型搭接结构疲劳设计具有直接参考价值。
        As an important structural component of a plane in its fatigue design,typical single-shear lap joint usually requires the analysis of its secondary bending. With the flat shells, by rational modelestablishing and analysis, the papergot the secondary bending of all fatigue detail points. At the same time, the paper validated the flat shells method. The calculation results and conclusionspresented in the paper are of reference value for the fatigue design of airplane's typical single-shear lap jointstructures.
引文
[1] CCAR-25-R4.中国民用航空规章(第25部). 运输类飞机适航规章[S]. 北京:中国民用航空局,2011:56-58.CCAR-25-R4. China civil aviation regulation(Part25). Airworthiness standards: transport category airplanes[S]. Beijing: Civil Aviation Administration of China, 2011:56-58 (In Chinese).
    [2] JSchijve, GCampoli, AMonaco. Fatigue of structures and secondary bending in structural elements[J].International Journal of Fatigue. 2009: 1111-1123.
    [3] 郑晓玲.民机结构耐久性与损伤容限设计手册:疲劳设计与分析[M].北京:航空工业出版社,2003:227-233.ZHENG XiaoLing. Handbook of civil airplane structure durability and damage tolerance design: Fatigue design and analysis[M]. Beijing: Aviation Industry Press,2003:227-233 (In Chinese).
    [4] Schijve J. Fatigue of structures and materials[D]. The Netherlands: Springer, 2001:5-6.
    [5] Schijve J. Riveted lap joints with a staggered thickness in the overlap of the joint[J]. Faculty of Aerospace Engineering, 2006:08-09.
    [6] Schijve J. Some elementary calculations on secondary bending in simple lap joints[M]. Amsterdam:National Aerospace Laboratory, 1972:11-13.
    [7] Müller RPG. An experimental and analytical investigation on the fatigue behavior of fuselage riveted lap joints[D]. Delft: Delft University of Technology,1995:123-125.
    [8] IC Whittaker, M Miller, UG Goranson. Durability and Damage Tolerance Evaluations of Jet Transport Structures[C]. The 5th International Conference on Structural Safety and Reliability(ICOSSAR),San Francisco, 1989, California: National Aerospace Laboratory, 1989:33-35.
    [9] 黄玮, 孙秦. 整体壁板结构纵向连接接头的优化设计[J]. 机械强度,2009,31(5):781-786.HUANG Wei, SUN Qin. Research and optimization design of a riveted longitudinal lap joint in integral panel structure[J]. Journal of Mechanical Strength, 2009,31(5):781-786 (In Chinese).

© 2004-2018 中国地质图书馆版权所有 京ICP备05064691号 京公网安备11010802017129号

地址:北京市海淀区学院路29号 邮编:100083

电话:办公室:(+86 10)66554848;文献借阅、咨询服务、科技查新:66554700