航空学报 > 1991, Vol. 12 Issue (10): 511-513

冷挤压孔板残余应力场分析

蒋金龙, 赵名泮   

  1. 飞机结构强度研究所
  • 收稿日期:1989-11-16 修回日期:1990-02-07 出版日期:1991-10-25 发布日期:1991-10-25

ANALYSIS OF RESIDUAL STRESS FIELD AT COLD-WORKED FASTENER HOLE

Jiang Jinlong, Zhao Mingban   

  1. Aircraft Structural Strength Research Institute
  • Received:1989-11-16 Revised:1990-02-07 Online:1991-10-25 Published:1991-10-25

摘要: <正> 1.冷挤压孔板残余应力场 如图1所示,设理想弹塑性材料厚壁圆筒内半径为R_1,外半径为R_2,受内压P作用,卸载后,形成塑性半径ρ,此时,圆筒残余应力场为

关键词: 残余应力, 厚壁筒, 塑性半径, 几何修正

Abstract: Based on ideally elastoplastic thick-walled cylinder solution, the residual stress field at cold-worked fastener hole of finite wide plate is obtained through geometric modification. The examples show that the calculations based on geometric modification agree with experiments very well in comparison with the solution based on thick -wall cylinder.

Key words: residual stress, thick-walled cylinder, plastic radius, geometric modifica-tion