航空学报 > 2003, Vol. 24 Issue (4): 336-338

7075铝合金板材残余应力深度梯度的评估

王秋成1, 柯映林1, 章巧芳2   

  1. 1. 浙江大学机械与能源学院, 浙江杭州 310027;2. 浙江工业大学机械工程系, 浙江杭州 310014
  • 收稿日期:2002-08-22 修回日期:2002-12-31 出版日期:2003-08-25 发布日期:2003-08-25

Evaluation of Residual Stress Depth Profiling in 7075 Aluminum Alloy Plates

WANG Qiu-cheng1, KE Ying-lin1, ZHANG Qiao-fang2   

  1. 1. College of Mechanical and Energy Engineering; Zhejiang University; Hangzhou 310027; China;2. Department of Mechanical Engineering; Zhejiang University of Technology; Hangzhou 310014; China
  • Received:2002-08-22 Revised:2002-12-31 Online:2003-08-25 Published:2003-08-25

摘要: 提高航空结构件残余应力的测试精度, 意味着可提高其安全可靠性, 减轻重量及降低成本, 然而现有的残余应力测试方法( 如钻孔法、X 射线法等) 只能测定构件外表面与浅表层的残余应力。为此, 引进一种被称为裂纹柔度法的残余应力测试新技术, 对7075 铝合金板材在T73, T7351, T7352 与T7353 状态下的内部残余应力进行了专门研究与评估。有关研究结果表明, 这种残余应力测试新技术不仅能测定7075 铝合金板材的全厚度残余应力分布及其应力梯度, 而且比逐层钻孔法与X 射线衍射法具有更好的敏感性和精确度。

关键词: 铝合金, 内部残余应力, 应力梯度, 裂纹柔度法, 评估, 测量

Abstract: The abilit y to accurately evaluate residual stresses will lead to stronger, lighter, longer2lasting and cheapercomponents in aircr aft industry. However, t he common residual stress measurement methods ( e. g . hole drillingmethod and X-ray diffraction met hod) are only useful to measur e the surface or subsurface r esidual stresses. Witht his in mind, the current research program is to introduce t he crack compliance method to characterize interior r esidual stresses in rolled 7075 aluminum plates procured in T73, T7351, T7352 and T7353 temper designations. Experimental results revealed that this newly proposed met hod can be used to evaluate through-thickness r esidual stresses of7075 aluminum plates. It further showed that measured subsurface stresses are mor e sensitive and accurate thant hose obtained by the incr emental hole dr illing method or X-ray diffraction method.

Key words: aluminum alloy, interior residual stress, stress gradient, crack compliance method, evaluation, measurement

中图分类号: