FGH4096合金盘件双组织热处理的数值模拟及试验验证

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• 英文论文题名：Numerical Simulation and Experimental Verification of DMHT Process for FGH4096 Superalloy Turbine Disk
• 论文作者：刘建涛 ; 陶宇 ; 张义文 ; 张国星 ; 刘明东 ; 钟燕 ; 董志国
• 英文论文作者：Liu Jiantao ; Tao Yu ; Zhang Yiwen ; Zhang Guoxing ; Liu Mingdong ; Zhong Yan ; Dong Zhiguo ; High Temperature Materials Research Division ; Central Iron &Steel Research Institute ; Beijing Key Laboratory of Advanced High Temperature Materials ; China Gas Turbine Establishment ; Shenyang Aeroengine Research Institute
• 年：2015
• 作者机构：钢铁研究总院高温材料研究所;高温合金新材料北京市重点实验室;中国燃气涡轮研究院;沈阳发动机设计研究所;
• 论文关键词：FGH4096合金 ; 双组织热处理 ; 温度场 ; 晶粒度
• 英文论文关键词：FGH4096 superalloy ; DMHT ; temperature field ; grain size
• 会议召开时间：2015-05-20
• 会议录名称：第十三届中国高温合金年会论文集
• 英文会议录名称：Proceedings of the 13th China Superalloys Conference
• 语种：中文
• 分类号：V263
• 学会代码：ZGJS
• 会议名称：第十三届中国高温合金年会
• 会议地点：中国北京
• 主办单位：中国金属学会高温材料分会
• 学会名称：中国金属学会
• 页数：4
• 文件大小：1226k
• 原文格式：O
• 会议级别：全国

摘要

对FGH4096合金盘件的双组织热处理进行了数值模拟和试验验证:数值模拟结果表明,通过选定合适的工艺参数,可实现盘件不同部位的温度梯度。在数值模拟的基础上,进行了盘件双重组织热处理,获得了轮缘部位为5~6级晶粒度,轮毂部位为10级晶粒度,辐板区域组织平缓过渡的双晶粒组织涡轮盘件。
By means of numerical simulation and experiment,dual microstructure heat treatment(DMHT) process is simulated and corresponding experimental DMHT processes have been performed.The numerical simulation showed that DMHT processes is reasonable for dual microstructure turbine disk production.Under certain conditions,temperature gradient for different zones can be acquired for FGH4096 PM superalloys turbine disk.Based on the numerical simulation results,A experimental DMHT processes are performed,the experimental result showed that the pancake rim zone grain growth is noticeable,the bore zone grain size of pancake is still fine,the hub zone grain size is between rim zone and bore zone.The numerical simulation and experimental result proved that DMHT process is feasible for FGH4096 superalloy Dual microstructure turbine disk production.

引文

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