航空学报 > 1996, Vol. 17 Issue (3): 373-378

4种铝合金的应变疲劳力学特性的研究

丁传富1, 欧阳辉1, 罗安民2, 岳俊文2   

  1. 1. 北京航空材料研究所25室;2. 成都飞机设计所,成都,610041
  • 收稿日期:1994-08-08 修回日期:1995-03-13 出版日期:1996-06-25 发布日期:1996-06-25

A STUDY OF STRAIN FATIGUE MECHANICS BEHAVIOUR

Ding Chuanfu1, Ou Yanghui1, Luo Anmin2, Yue Junwen2   

  1. 1. Beijing Institute of Aeronautical Materials, Beijing,100095;2. Chengdu Aircraft Institute, Chengdu, 610041
  • Received:1994-08-08 Revised:1995-03-13 Online:1996-06-25 Published:1996-06-25

摘要: 分析了 4种铝合金在循环应变作用下的力学行为及材料在纵、横或高向的应变疲劳力学性能的差异。实验结果表明,不同的取样方向对铝合金的应变疲劳寿命的影响主要取决于材料的塑性。4种铝合金在纵、横或高向的循环应力-应变行为均表现为循环硬化。7475 T735 1合金较之其他 3种材料具有较好的应变疲劳特性

关键词: 铝合金, 试验, 力学性质, 应力-应变关系, 材料疲劳

Abstract: The mechanics behaviour of the four aluminum alloys under cyclic strain control as well as the discrepancies of strain fatigue behaviour between transvers,longitudinal and high direction are analysed in the paper. The test results is shown that influence of different direction on strain fatigue life of alluminum alloys mainly depend on plastic of materials. Behaviour of cyclic stress strain on four aluminum alloys all exhibit cyclic strain hardning in longitudinal, transvers and high orientation. 7475T7351 alloys show the larger strain fatigue properties as compared with other three aluminum alloys.

Key words: aluminum alloys tests, mechanical properties, stressst rain relationships, fa tigue (materials)

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