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GH4169合金开坯锻造中组织演变的数值分析 被引量:8

Numerical analysis of microstructure evolution of GH4169 superalloy during cogging process
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摘要 GH4169合金的大直径锻棒是生产燃气涡轮发动机涡轮盘等大尺寸锻件的重要材料。主要由开坯锻造工艺制备,得到组织均匀细小、性能优良的锻棒,显著地提高锻件的性能。开发了GH4169合金的微观组织预测系统,对GH4169合金开坯锻造过程中的组织演变规律进行三维热力耦合数值分析。 Large diameter bars of GH4169 superalloy forged by cogging process are important for the production of large dimension components such as turbine disks of gas turbine engines. And, bars with fine grain and good performance can improve the performance of workpieces obviously. The microstructural prediction system of GH4169 superalloy was developed. In addition, the microstructure evolution of alloy during cogging process was simulated and analyzed using the prediction system and 3D thermal-mechanical coupled finite element method.
出处 《兵器材料科学与工程》 CAS CSCD 北大核心 2012年第2期19-23,共5页 Ordnance Material Science and Engineering
基金 宁波市自然科学基金资助项目(2011A610157)
关键词 GH4169合金 开坯锻造 组织模拟 二次开发 GH4169 superalloy cogging microstructural simulation secondary development
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参考文献12

  • 1Yang D Y,Lee N K,Yooh J H.A 3-dimensional simulation for isothermal turbine blade forging by the rigid-viscoplastic finite element method[J].Journal of Materials Engineer and Perform,1993,2(1):119-124.
  • 2Cho R,Lee N K,Yang D Y.A 3D simulation for non-isothermal forging of a steam turbine blade by the thermoviscoplastic finite element method[J].Journal of Engineer Manufacture,1993,207:265-273.
  • 3Lv C,Zhang L W,Wang Z K.3D rigid-viscoplastic FEM simulation of forging process of a gas turbine rotor blade[J].Materials Science Forum,2007,523/533:733-736.
  • 4Na Y S,Yeom J T,Park N K.Simulation of microstructures for alloy 718 blade forging using 3D FEM simulator[J].Journal of Materials Processing Technology,2003,141:337-342.
  • 5Dandre C A,Roberts S M,Evans R W,et al.Microstructural evolution of Inconel* 718 during ingot breakdown:process modelling and validation[J].Materials Science and Technology,2000,16(1):14-25.
  • 6Tin S,Lee P D,Kermanpur A.Integrated modeling for the manufacture of Ni-based superalloy discs from solidification to final heat treatment[J].Metallurgical and Materials Transactions A,2005,36:2493-2504.
  • 7Kermanpur A,Tin S,Lee P D,et al.Integrated Modeling for the Manufacture of Aerospace Discs:Grain Structure Evolution[J].Journal of the Minnerals,Metal and Materials Society,2004,56:72-78.
  • 8Yeom J T,Lee C S,Kim J H,et al.Finite-element analysis of microstructure evolution in the cogging of an alloy 718 ingot[J].Materials Science and Engineering A,2007,449/451:722-726.
  • 9赵长虹,孙恺红,王继红,彭永辉.GH4169合金大锭型真空白耗锭锻造开坯工艺及组织的研究[J].辽宁特殊钢,2003(1):21-26. 被引量:3
  • 10赵长虹,孙恺红,王继红,吴贵林,王健豪,金槿秀,田树森,庄景云,邓群,杜金辉.GH4169合金大锭型真空自耗锭的锻造开坯工艺及组织[J].钢铁研究学报,2003,15(z1):351-356. 被引量:4

二级参考文献1

  • 1[4]SjobergG,LngestenNG.GrainBoundary δ-phaseMorphologies, Carbides and Rupture Sensitivity of Cast Allo7118.Minerals and Materials Society,1991.

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