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室温和650℃下晶粒尺寸对GH4169合金疲劳小裂纹萌生和扩展行为的影响 被引量:8

Grian Size Effect on the Initiation and Propagation of Small Fatigue Crack of GH4169 Alloy at Room Temperature and 650 ℃
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摘要 在室温和650℃条件下,研究晶粒尺寸对GH4169合金疲劳小裂纹萌生机理和扩展行为的影响。通过在960℃、1 010℃、1 020℃、1 050℃条件下,各保温1 h来改变试样晶粒尺寸。通过光学显微镜来观察不同热处理后的微观组织。利用覆膜法监测小裂纹扩展过程。结果表明,两种温度下疲劳小裂纹萌生机理和扩展模式在细晶组织和粗晶组织间均会发生转变。室温和650℃条件下,裂纹扩展速率在小裂纹阶段近似恒定。室温下,平均晶粒尺寸变化对小裂纹扩展速率几乎没有影响。650℃下,随着平均晶粒尺寸增加,小裂纹扩展速率增大。无论哪种温度下,一旦表面裂纹长度达到一定临界尺寸,小裂纹会加速扩展,进入长裂纹阶段。室温下不同平均晶粒尺寸试样临界裂纹长度基本相同,650℃下随着平均晶粒尺寸增加临界裂纹长度增加。 Addressing grain size effect on the initiation and propagation behavior of small fatigue crack of GH4169 alloy at room temperature and 650 ℃. Changing the grain size of specimen by solid solution heat treated at 960 ℃、1 010 ℃、1 020 ℃、1 050 ℃about 1 h. The microstructures after different heat treatments are investigated by optical microscope(OM). The replica method is used to measure the crack length. Results show that there are transition of fatigue crack initiation mechanism and crack propagation mode between fine-grained material and coarse-grained material at both room temperature and 650 ℃. Crack propagation rates are almost constant in small crack stages at both room temperature and 650 ℃. The variations of average grain size have almost no effect on the small crack rates at room temperature. But at 650 ℃ small crack propagation rates increase with the increase of average grain size. Once the length of surface cracks reach a critical size, the cracks propagate quickly. At room temperature the critical sizes of surface crack of specimens with different average grain size are almost uniform. However the critical size of surface cracks increase with the increase of average grain size.
作者 吴楠 张显程 涂善东 钱夏夷 王一宁 WU Nan ZHANG Xiancheng TU Shantung QIAN Xiayi WANG Yining(Key Laboratory of Pressure Systems and Safety of Ministry of Education, East China University of Science and Technology, Shanghai 200237 National Quality Supervision and Inspection Center of Pressure Pipe Components, Nanjing 211100)
出处 《机械工程学报》 EI CAS CSCD 北大核心 2016年第20期66-75,共10页 Journal of Mechanical Engineering
关键词 小裂纹 疲劳 晶粒尺寸 GH4169 室温 650℃ small crack fatigue grain size GH4169 room temperature 650 ℃
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  • 1Yu Yangui,Zhang Wenbin,(Wenzhou University).CALCULATIONS TO ITS FATIGUE DAMAGE FRACTURE AND TOTAL LIFE UNDER MANY-STAGE LOADING FOR A CRANK SHAFT[J].Chinese Journal of Mechanical Engineering,1994,7(4):281-288. 被引量:2
  • 2吴学仁,刘建中.基于小裂纹理论的航空材料疲劳全寿命预测[J].航空学报,2006,27(2):219-226. 被引量:48
  • 3YU Yangui,LIU Xiang,ZHANG Changsheng,TAN Yanhua.FATIGUE DAMAGE CALCULATED BY RATIO-METHOD TO METALLIC MATERIALS WITH SMALL CRACK UNDER UNSYMMETRIC CYCLIC LOADING[J].Chinese Journal of Mechanical Engineering,2006,19(2):312-315. 被引量:3
  • 4李细广 琚定一.疲劳损伤临界值和疲劳寿命[C]..疲劳损伤理论研讨会论文集[C].洛阳:中国航空学会,中国力学学会,1992.104.
  • 5李长春.裂纹体疲劳的微结构变化和损伤演变[C]..疲劳损伤理论研讨会论文集[C].洛阳:中国航空学会,中国力学学会,1992.35.
  • 6YU Yangui, ZHAO E J. Calculations to damage evolving rate under symmetric cyclic loading[C]//Proceedings of the Seventh International Fatigue Congress, 1999, Beijing. 1999: 1137-1142.
  • 7YU Yangui. The Calculations to its damage evolving rate and life for a component under un-symmetrical cyclic load[C]//Proceedings of Asian-Pacific Conference on Fracture and Strength of Structure'93, 1993, Japan, 1993: 615.
  • 8DOWLING N E, BROSE W R, WILSON W K. Notched member fatigue life predictions by the local strain approach, fatigue under complex loading[R]. SAE, 1977.
  • 9YU Yangui. Fatigue damage of materials with small crack calculated by the ratio method under cyclic loading[C]// International Symposium on Macro-, Meso-, Micro- and Nano-Mechanics of Materials, Dec. 8-10, 2003, Hong Kong. Switzerland: Trans. Tech. Publications, 2003, 79-86.
  • 10LANDGRAF R W. Fatigue life predictions for a notched member under complex load histories, fatigue under complex load[R]. SAE, 1977.

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