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作 者:李淼泉[1] 王小津[1] 苏少博[2] 王海荣[2]
机构地区:[1]西北工业大学,西安710072 [2]西安航空发动机集团有限公司,西安710021
出 处:《中国机械工程》2008年第15期1867-1870,共4页China Mechanical Engineering
基 金:国家自然科学基金资助项目(50475144);高等学校优秀青年教师教学科研奖励计划项目(CJ0402)
摘 要:通过GH4169合金的热模拟压缩实验,研究了变形工艺参数对GH4169合金高温变形时流动应力的影响规律,建立了GH4169合金高温变形时的加工图,结果表明:变形温度升高和应变速率减小使GH4169合金高温变形时峰值流动应力和稳态流动应力显著降低;GH4169合金高温变形时存在三个非稳定区域,第一个区域的变形温度在970~1030℃之间,应变速率在10.0~50.0s^-1之间;第二个区域的变形温度在930~940℃之间,应变速率在0.15~7.Os^-1之间;第三个区域的变形温度在930~960℃之间,应变速率在7.0~50.0s^-1之间的区域。Isothermal compression for the nickel--based superalloy GH4169 was carried out at a Thermecmaster-Z simulator, effect of the process parameters on the flow stress was investigated and the processing map was obtained in isothermal compression of the nickel--based superalloy GH4169 according to the analyses of experimental results. The research results show that the peak and steady stress significantly decreases with an increasing of the deformation temperature and a decreasing of the strain rate in the high temperature deformation of the nickel-based superalloy GH4169. The processing map was drawn from the experimental data. From the processing map of nickel--based superalloy GH4169, three unstable regions are in the following: the first is as 970-1030℃ of deformation temperature and 10. 0-50.0s^-1 of strain rate, the second is as 930-940℃ of deformation temperature and 0. 15-7.0s 1 of strain rate, and the third is as 930-960℃ of deformation temperature and 7.0-50.0s^-1 of strain rate.
分 类 号:TG311[金属学及工艺—金属压力加工] TB125[理学—工程力学]
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