论文

表面滚压对LZ50车轴钢疲劳短裂纹行为的影响

  • 杨冰
展开
  • 西南交通大学牵引动力国家重点实验室, 成都 610031
杨冰, 男, 1979年生, 副研究员, 博士

收稿日期: 2012-04-01

  修回日期: 2012-05-26

  网络出版日期: 2012-08-11

基金资助

国家自然科学基金项目 50575189和50821063, 中央高校基本科研业务费专项资金项目 SWJTU11CX075, 西南交通大学牵引动力国家重点实验室开放基金项目 2011TPL_T02资助

INFLUENCE OF SURFACE ROLLING ON SHORT FATIGUE CRACK BEHAVIOR FOR LZ50 AXLE STEEL

  • YANG Bing
Expand
  • 西南交通大学牵引动力国家重点实验室, 成都 610031

Received date: 2012-04-01

  Revised date: 2012-05-26

  Online published: 2012-08-11

Supported by

Supported by National Natural Science Foundation of China (Nos.50575189 and 50821063), Fundamental Research Funds for the Central Universities (No.SWJTU11CX075), and Opening Project of State Key Laboratory of Traction Power, Southwest Jiaotong University (No.2011TPL T02)

摘要

完成了6根表面经滚压处理的漏斗形圆棒试样疲劳短裂纹复型实验, 结果表明其短裂纹行为表现出明显的微观结构短裂纹(MSC)和物理短裂纹(PSC) 2阶段特征. 在MSC阶段, 由于不同微观结构障碍的阻碍, 主导短裂纹出现2次较明显的扩展减速, 进入PSC阶段后, 随着主导短裂纹尺度的增长, 该现象不再显著. 与表面未经滚压的试样相比, 在给定主导短裂纹尺度条件下, 滚压试样的裂纹扩展速率低得多, 这种差异在MSC阶段可达1个数量级. 滚压试样平均疲劳寿命达到未滚压试样的6.4倍. 表面滚压处理有效抑制了微裂纹的形核与合并, 改善了局部微观结构条件, 并推迟了MSC与PSC过渡阶段的到来,提高了材料的抗疲劳性能. 对主导短裂纹尺度、疲劳寿命分数和有效短裂纹密度3种特征参量进行分析, 确定了其良好假设分布和统计演化规律.

本文引用格式

杨冰 . 表面滚压对LZ50车轴钢疲劳短裂纹行为的影响[J]. 金属学报, 2012 , 48(8) : 922 -928 . DOI: 10.3724/SP.J.1037.2012.00169

Abstract

Crack initiation, coalescence and propagation normally occupy more than 70% the fatigue life of most engineering structure in the whole fatigue damage process. Investigation on the influence of final machining methods, such as surface rolling, on short fatigue crack behavior for LZ50 axle is beneficial to the manufacture and maintenance of corresponding railway axles. After rolling, the surface hardness increased from 201.68 HV0.1 to 222.90 HV0.1. Much higher residual compressive stress was also engendered in surface and sub–surface by this machining method. Totally six smooth hourglass shaped specimens with surface rolling were tested by a replica technique. The characteristic two–stages behavior, that is, the micro–structural short crack (MSC) stage and the physical short crack (PSC) stage, during crack initiation and propagation was revealed. In MSC stage, the growth rate of dominant short crack for all specimens decelerated twice clearly due to different microstructural barriers. This behavior was related to the restraint of ferrite grain boundary firstly and then to the constraint of pearlite banded structure. While in PSC stage, the decelerating trend was no longer obvious with the increasing dominant crack size. With a given dominant crack size, the crack growth rates of surface rolled specimens were much slower than those of specimens without surface rolling. This difference could reach 1 order of magnitude in MSC stage. Meanwhile, the average fatigue life of the former was about 5.4 times longer than that of the latter. The effective short fatigue crack density of surface rolled specimens increased in MSC stage, then attained the peak value at the turning point between MSC stage and PSC stage, and finally decreased in PSC stage. At the same time, surface rolled specimens owned much less crack density than specimens without surface rolling during the whole fatigue process. Surface rolling can restrain the nucleation and connection of micro–cracks, improve the local microstructure conditions, push back the transition point between MSC and PSC stages, and thus improve the anti–fatigue performance of material. Finally, the reasonable assumed distributions for three kinds of characteristic parameters, i.e., dominant short crack size, fatigue life fraction and effective short crack density, were determined. In general, the dispersion of above data was high in initial stage and relatively low in later stage during crack initiation and propagation process.

参考文献

[1] Liu E Z, Zheng Z, Tong J, Ning L K, Guan X R. Acta Metall Sin, 2010; 46: 708

(刘恩泽, 郑 志, 佟健, 宁礼奎, 管秀荣. 金属学报, 2010; 46: 708)

[2] Hu Y H, Zhang Z, Zhong Q P, Han B C. J Mech Strength, 2009; 31: 979

(胡燕慧, 张 峥, 钟群鹏, 韩邦成. 机械强度, 2009; 31: 979)

[3] Suresh S, translated by Wang Z G. Fatigue of Materials. 2nd Ed, Beijing: National Defense Industry Press, 1999: 387

(Suresh S著, 王中光译. 材料的疲劳. 第二版, 北京: 国防工业出版社, 1999: 387)

[4] Pearson S. Eng Fract Mech, 1975; 7: 235

[5] Maluf O, Milan M T, Spinelli D. J Mater Eng Perform, 2004; 13: 195

[6] Ueji R, Tsuji N, Minamino Y. Acta Mater, 2002; 50: 4177

[7] Mara N A, Sergueeva A V, Mara T D. Mater Sci Eng, 2007; A463: 238

[8] Jia G W, Hua L, Mao H J. J Mater Process Technol, 2007; 187–188: 562

[9] Ma B, Tieu A K, Lu C, Jiang Z. J Mater Process Technol, 2002; 125–126: 657

[10] Yang B, Zhao Y X. Adv Mater Res, 2012; 463: 85

[11] Zhao Y X, Gao Q, Wang J N. Acta Metall Sin, 2000; 36: 931

(赵永翔, 高庆, 王金诺. 金属学报, 2000; 36: 931)

[12] Zhao Y X, Gao Q, Wang J N. Acta Metall Sin, 2000; 36: 937

(赵永翔, 高庆, 王金诺. 金属学报, 2000; 36: 937)

[13] Zhao Y X, Yang B, Gao Q. Nucl Power Eng, 2003; 24: 127

(赵永翔, 杨冰, 高庆. 核动力工程, 2003; 24: 127)

[14] Zhao Y X, Yang B, Gao Q. Nucl Power Eng, 2005; 26:584

(赵永翔, 杨冰, 高庆. 核动力工程, 2005; 26: 584)

[15] Zhao Y X. PhD Thesis, Southwest Jiaotong University,Chengdu, 1998

(赵永翔. 西南交通大学博士学位论文, 成都, 1998)

[16] Zhao Y X, Gao Q, Wang J N. Fatigue Fract Eng Mater Struct, 1999; 22: 459

[17] Miller K J. Fatigue Fract Eng Mater Struct, 1987; 10: 75

[18] Miller K J. Fatigue Fract Eng Mater Struct, 1987; 10: 93

[19] Obrtl´?k K, Pol´ak J, H´ajek M, Vaˇsek A. Int J Fatigue, 1997; 19: 471

[20] Luo J, Bowen P. Int J Fatigue, 2004; 26: 113

[21] Ortiz J, Cisilino A P, Otegui J L. Fatigue Fract Eng Mater Struct, 2001; 24: 591

[22] Ding C F, Liu J Z, Wu X R. J Aeronaut Mater, 2005; 25(6): 11

(丁传富, 刘建中, 吴学仁. 航空材料学报, 2005; 25(6): 11)

[23] Zhao Y X, Gao Q, Wang J N. Fatigue Fract Eng Mater Struct, 1999; 22: 469

[24] Zhao Y X. J Mater Sci Technol, 2003; 19: 129

[25] Yang B, Zhao Y X. Int J Fatigue, 2012; 35: 71

[26] Yang B, Zhao Y X. Key Eng Mater, 2011; 474: 979

[27] Yang B, Zhao Y X. Adv Mater Res, 2010; 118: 75

[28] Zhao Y X, Sun Y F, Gao Q. J Mech Strength, 2001; 23: 102

(赵永翔, 孙亚芳, 高庆. 机械强度, 2001; 23: 102)
文章导航

/