服役经历对7N01铝合金断裂力学性能的影响

doi:10.12068/j.issn.1005-3026.2017.10.015

东北大学学报:自然科学版 ›› 2017, Vol. 38 ›› Issue (10): 1442-1446.DOI: 10.12068/j.issn.1005-3026.2017.10.015

服役经历对7N01铝合金断裂力学性能的影响

张啸尘^1,2，谢里阳¹，胡杰鑫¹，张诗健¹

(1. 东北大学航空动力装备振动及控制教育部重点实验室，辽宁沈阳110819; 2. 沈阳建筑大学机械工程学院，辽宁沈阳110168)

收稿日期:2016-05-03 修回日期:2016-05-03 出版日期:2017-10-15 发布日期:2017-10-13
通讯作者: 张啸尘
作者简介:张啸尘(1985-)，男，辽宁鞍山人，东北大学博士研究生，沈阳建筑大学讲师；谢里阳(1962-)，男，安徽岳西人，东北大学教授，博士生导师.
基金资助:
国家自然科学基金重点资助项目(51335003)；辽宁重大装备制造协同创新中心资助项目；国家自然科学基金资助项目(51675353)；教育部长江学者创新团队计划项目(IRT_15R45)；沈阳市科技局计划项目(F16-096-1-00).

Effect of Service on Fracture Mechanical Properties of 7N01 Aluminum Alloy

ZHANG Xiao-chen^1,2， XIE Li-yang¹， HU Jie-xin¹， ZHANG Shi-jian¹

1.Key Laboratory of Aero Power Equipment Vibration and Control， Ministry of Education， Northeastern University， Shenyang 110819， China; 2.School of Mechanical Engineering， Shenyang Jianzhu University， Shenyang 110168， China.

Received:2016-05-03 Revised:2016-05-03 Online:2017-10-15 Published:2017-10-13
Contact: ZHANG Xiao-chen
About author:-
Supported by:
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摘要/Abstract

摘要： 材料在服役过程中的可靠性和耐久性是结构安全评估的基础，针对某型高速列车上服役多年的7N01铝合金材料，进行实验室空气环境下断裂力学性能参数测试，并分析服役前后疲劳裂纹扩展行为差异.结果表明:服役经历促使材料的各项断裂力学性能退化，呈规律性下降趋势;服役材料稳态疲劳裂纹扩展阶段da/dN-ΔK关系曲线呈折线现象，分段拟合方法能够精确描述其疲劳裂纹扩展行为.微观形貌的结果显示:服役后7N01铝合金的疲劳裂纹早期扩展区、稳定扩展区和快速断裂区的断裂表面依次为脆性断裂特征、塑性疲劳条带和脆性疲劳条带混合模式及沿晶和穿晶的混合断裂形貌.

关键词: 7N01铝合金, 断裂力学, 疲劳裂纹扩展, 折线现象, 断口形貌

Abstract: The reliability and durability of materials in service are the assessment foundation of the structural safety. Aimed at the 7N01 aluminum alloy experienced a long term service in high speed trains， the fatigue mechanical properties were investigated in laboratorial atmosphere， and the fatigue cracks propagation (FCP) behaviors of materials with/without service were analyzed. The results showed that the experience of service deteriorates the mechanical properties， showing a regular decline trend. The da/dN-ΔK curve in the FCP zone after service showed a turning phenomenon， and a piecewise Paris’ curve fitting method was used to describe the FCP behavior. The results of the fracture surface morphologies showed that the are crack initiation zone， steady growth zone and rapid growth zone of 7N01 alloy after service corresponding to cleavage fracture mode， mixed plastic and cleavage fatigue striation， and mixed intergranular and transgranular fracture， respectively.

Key words: 7N01 aluminum alloy, fracture mechanics, fatigue crack propagation, turning phenomenon, fracture morphology

中图分类号:

U270.32

张啸尘，谢里阳，胡杰鑫，张诗健. 服役经历对7N01铝合金断裂力学性能的影响[J]. 东北大学学报:自然科学版, 2017, 38(10): 1442-1446.

ZHANG Xiao-chen， XIE Li-yang， HU Jie-xin， ZHANG Shi-jian. Effect of Service on Fracture Mechanical Properties of 7N01 Aluminum Alloy[J]. Journal of Northeastern University Natural Science, 2017, 38(10): 1442-1446.

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服役经历对7N01铝合金断裂力学性能的影响

Effect of Service on Fracture Mechanical Properties of 7N01 Aluminum Alloy

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