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第四代粉末高温合金成分选取范围研究 被引量:14

STUDY ON COMPOSITION VARIATION RANGE OF THE FOURTH GENENRATION PM SUPERALLOYS
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摘要 在综合分析第一至三代粉末高温合金发展思路并借鉴叶片合金的基础上,从高强度、高损伤容限和高工作温度要求出发,围绕固溶强化、沉淀强化和晶界强化,研究并确定了第四代粉末高温合金的成分选取范围:①γ '相形成元素Al+Ti+Ta+Nb≈9%~15%;②固溶强化元素Cr+Co+Mo+W≈30%~40%;③TCP相形成元素Cr+Mo+W≤20%;④一定量晶界强化元素(C、B、Zr、Hf). The study of the fourth generation PM superalloys was performed to develop compositions that exhibit required integration of significantly high strength,high damage tolerance and high-temperature capability.Based on the integrated analysis of the development of the first,second and third generation PM superalloys as well as superalloys for blade applications,the study was carried out primarily following the mechanisms of solution strengthening,precipitation strengthening and grain boundary strengthening.Finally,the composition variation range of the fourth generation PM superalloys was determined as:① the mass ratio of gamma prime forming elements Al+Ti+Ta+Nb is 9%~15%; ② the mass ratio of solution strengthening elements Cr+Co+Mo+W is 30%~40%; ③ the mass ratio of TCP formers Cr+Mo+W is not more than 20% ; ③ a certain amount of grain boundary strengthening elements C,B,Zr and Hf.
出处 《粉末冶金工业》 CAS 北大核心 2014年第1期20-25,共6页 Powder Metallurgy Industry
关键词 第四代粉末高温合金 成分选取范围 the fourth generation PM superalloys composition variation range
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参考文献26

  • 1张义文,上官永恒.粉末高温合金的研究与发展[J].粉末冶金工业,2004,14(6):30-43. 被引量:76
  • 2贾建,陶宇,张义文,张莹,刘建涛.第三代粉末冶金高温合金René104的研究进展[J].粉末冶金工业,2007,17(3):36-43. 被引量:27
  • 3CHANG D R,KRUEGER D D,SPRAGUE R A. Superalloy Powder Processing,Properties and Turbine Disk Applications[A].Warrendale,PA:The Metallurgical Society of AIME,1984.245-273.
  • 4KRUEGER D D,KISSINGER R D,MENZIES R G. Development and Introduction of a Damage Tolerant High Temperature Nickel Base Disk Alloy,René88DT[A].Warrendale,PA:TMS,1992.277-286.
  • 5RAYMONDE L,SRIVATSA S K. Isothermal Forging of Nickel-Base Superalloys in Air[P].US Patent,2004/221927,2004.
  • 6TELESMAN J,KANTZOS P,GAYDA J. Microstructural Variables Controlling Time-Dependent Crack Growth in A P/M Superalloy[A].Warrendale,PA:TMS,2004.215-224.
  • 7GAYDA J,GABBT P,KANTZOS P T. The Effect of Dual Microstructure Heat Treatment on an Advanced Nickel-Base Disk Alloy[A].Warrendale,PA:TMS,2004.323-329.
  • 8SMALL C J,SAUNDERS N. The Application of Calphad Techniques in the Development of A New Gas-Turbine Disk Alloy[J].{H}MRS Bulletin,1999,(4):22-26.
  • 9REYNOLDS PAUL L. Superalloy Compositions,Articles and Methods of Manufacture[P].US Patent,8147749,2012.
  • 10HARADA H. High Temperature Materials for Gas Turbines:The Present and Future[A].Tokyo,Japan:IGTC Tokyo KS-2,2003.

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