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2Cr13与1Cr18Ni9Ti两种材质喷嘴环热疲劳性能对比

Comparative Thermal-Fatigue Characteristics of the Jet of 2Cr13 and 1Cr18Ni9Ti Alloy

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【作者】 董显平郁金星张源虎孙景斌徐建英

【Author】 Dong Xianping Yu Jinxing Zhang Yuanhu (Shanghai Jiaotong University Shanghai 200030 PRC) Sun Jingbin Xu Jianying (Ministry of Railways Beijing 100844 PRC)

【机构】 上海交通大学教育部高温材料及高温测试开放实验室!上海200030铁道部机务局!北京100844

【摘要】 在试验室条件下观察了2Cr13 与1Cr18Ni9Ti两种材质整铸式喷嘴环的热疲劳行为。结果表明,在特定环境条件下工作的喷嘴环,2Cr13 材质的抗热疲劳性能优于1Cr18Ni9Ti材质,前者喷嘴环在一定次数热循环后无开裂现象,后者喷嘴环严重开裂。其热疲劳裂纹在构件薄弱处出现,萌生于晶界,并沿晶界扩展。

【Abstract】 The thermal fatigue behaviors of the cast jet of 2Cr13 and 1Cr18Ni9Ti alloy were observed by laboratory testing. The results show that thermal fatigue resistance of 2Cr13 alloy is superior to that of 1Cr18Ni9Ti alloy under a special environment. After a certain number of thermal cycles, few cracks were found in the jet of 2Cr13 alloy, the cracks appeared in the jet of 1Cr18Ni9Ti alloy were serious. Thermal fatigue cracks which occurred to the weak position were intercrystalline in origin and mode of propagation.

【关键词】 喷嘴环热疲劳涡轮增压器
  • 【文献出处】 机械工程材料 ,MATERIALS FOR MECHANICAL ENGINEERING , 编辑部邮箱 ,1999年05期
  • 【分类号】TG115.57
  • 【被引频次】1
  • 【下载频次】141
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