• CN:11-2187/TH
  • ISSN:0577-6686

›› 1996, Vol. 32 ›› Issue (1): 103-109.

• 论文 • 上一篇    

ZM1镁合金的滚轧形变强化及机理

冯忠信;何家文;张建中;陈新增;魏振昌;田广东   

  1. 西安交通大学;宁波高等专科学校;华兴航空机轮公司
  • 发布日期:1996-01-01

SURFACE PLASTIC DEFORMATION STRENGTHENING BEHAVIOURS AND ITS MECHANISM OF MAGNESIUM ALLOY OF ZM1

Feng Zhongxin;He Jiawen;Zhang Jianzhong;Chen Xinzeng;Wei Zhenchang;Tian Guanglai   

  1. Xi'an Jiaotong University Ningbo College Huaxing Aircraft Wheel Corporation
  • Published:1996-01-01

摘要: 研究了ZM1铸造镁合金的表面滚压强化特性。结果表明,密排六方结构的ZM1镁合金的表面滚压强化效果相当显著,缺口疲劳极限提高达157%~212%,并大大超过未滚压的光滑疲劳极限。高的缺口疲劳强度可为构件提供充裕的强度裕度,缺口疲劳极限大于光滑疲劳极限可为构件的等强度设计提供可能性。滚压时该镁合金通过滑移和孪生两种方式进行塑性变形,伴随着位错密度的显著增高和引入高的残余压应力。缺口疲劳极限大幅度地提高主要归因于残余压应力有效地延缓疲劳裂纹的扩展以及显著地降低疲劳缺口敏感性的作用。此即表面形变残余压应力强化的观点。

关键词: 残余应力, 镁合金, 疲劳强度, 塑性形变

Abstract: The surface plastic deformation strengthening behaviours of magnesium alloy of ZM1 are studied. The results show that there is an excellent surface plastic deformation strengthening effect for magnesium alloy of ZM1 with hexagonal close-packed structure, the increments of the notch fatigue limit is about 157%~212% after surface rolling and is greatly above the smooth fatigue limit of non-rolling. The high notch fatigue strength can provide extra ample strength for parts, and notch fatigue limit that exceeded the smooth fatigue limit can also provide a possibility for equel strength design of parts. During surface rolling, the plastic deformation can be carried out in the surface layer of specimens by way of both slip and twin, with increasing the dislocation density and the introducing the high residual compressive stresses. The improvement of notch fatigue limit is mainly attributed to the high residual compressive stresses. Based on this, a new strengthening viewpoint of residual stress is proposed, which the residual compressive stresses play a dominant role in the fatigue strength for surface plastic deformation parts.

Key words: Fatigue strength, Magnesium alloy, Plastic deformation, Residual stress