欢迎登录材料期刊网

材料期刊网

高级检索

裂纹扩展速率不仅是高温合金涡轮盘的重要使用性能,同时也是涡轮盘损伤容量设计和寿命预测的重要指标之一.总结了高温合金的裂纹扩展速率的各种影响因素,包括外部因素和内部因素两大类.外部因素指试件或构件的实验条件或服役条件,如温度、环境、频率、应力比、保载时间以及其它因素等.内部因素指材料本身所具有的状态和性能,如材料的晶粒尺寸、析出相、晶界及化学成分等.这些因素单独作用或交互作用影响高温合金裂纹扩展速率.

参考文献

[1] Liu Xingbo;Shalini Rangararan;Ever Barbero.Fatigue crack propagation behaviors of new development Allvac 718 Plus superalloys[A].Champion:The TMS High Temperature Alloys Committee,2004:269.
[2] Hardy,M C;Zirbel,B;Shen,G.Developing tolerance and creep resistance in a high strength nickel alloy for disc applications[A].Champion:The TMS High Temperature Alloys Committee,2004:83.
[3] Pang H T;Reed P A S .Microstructure effects on high temperature fatigue crack initiation and short crack growth in turbine disc nickel-base superalloy udimet 720 Li[J].Materials Science and Engineering,2007,A448:67.
[4] Xiao L;Chen D L;Chaturvedi M C .Effect of boron on fatigue crack growth behavior in superalloy IN 718 at RT and 650℃[J].Materials Science and Engineering,2006,A428:1.
[5] Liu Xingbo;Xu Jing;Ever Barbero et al.Effect of thermal treatment on the fatigue crack propagation behavior of new Ni-based alloy[J].Materials Science and Engineering,2008,A474:30.
[6] Xingbo Liu;Bruce Kang;Keh-Minn Chang .The effect of hold-time on fatigue crack growth behaviors of WASPALOY alloy at elevated temperature[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2003(1/2):8-14.
[7] Osinkolu GA.;Onofrio G.;Marchionni M. .Fatigue crack growth in polycrystalline IN 718 superalloy[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2003(1/2):425-433.
[8] Woodford D A.Gas phase embitterment and time dependent cracking of nickel based super-alloys[J].Energy Materials,2006(01):59.
[9] 许忠勇,王利君,余和存.疲劳裂纹扩展的影响因素分析[J].机械强度,2004(z1):202-204.
[10] Longzhou Ma;Xingbo Liu;Keh-Minn Chang .Reply to Comment on "Identification of SAGBO-Induced Damage Zone Ahead of Crack Tip to Characterize Sustained Loading Crack Growth in Alloy 783"[J].Scripta materialia,2006(2):309-311.
[11] Tim P Gabb;Jack Telesman;Pete T Kantzos.Effect of high temperature exposures on fatigue life of disk superalloys[A].Champion:The TMS High Temperature Alloys Committee,2004:283.
[12] Zapatero J;Moreno B;Gonzdlez-Herrera A .Fatigue crack closure determination by means of finite element analysis[J].Engineering Fracture Mechanics,2008,75:41.
[13] 倪向贵,李新亮,王秀喜.疲劳裂纹扩展规律Paris公式的一般修正及应用[J].压力容器,2006(12):8-15,19.
[14] 师小红,敦怡,徐章遂.三参数全范围裂纹扩展公式[J].煤矿机械,2007(06):58-60.
[15] 吴欢,赵永庆,曾卫东.疲劳裂纹扩展行为的研究现状及钛合金的疲劳裂纹扩展特征[J].稀有金属快报,2007(07):1-6.
[16] 李晓,董建新,张丽娜,张麦仓,胡尧和,谢锡善,国为民.疲劳保载时间与固溶处理对PM René 95合金高温裂纹扩展速率的影响[J].金属学报,2001(10):1059-1063.
[17] Liu Xingbo;Xu Jing;Nate Deem.Effect of thermal-mechanical treatment on the fatigue crack propagation behavior of newly development allvac 718 plus alloy[A].Warrendale:The Mineral,Metals and Materials Society,2005:233.
[18] Hoffelner W;Scalin R B .On the correlation of microstructure,fatigue life and fatigue crack propagation in nickel base superalloys[J].Eng Mater Services,1984,3:1647.
[19] 张莹,张义文,陶宇.俄罗斯EP741NP粉末高温合金的研究[J].钢铁研究学报,2006(08):58-62.
[20] Telesman,J;Kantzos,P;Gayda,J.Microstructural variables controlling time-dependent crack growth in a P/M superalloy[A].Champion:The TMS High Temperature Alloys Committee,2004:215.
[21] 国为民,董建新,吴剑涛,张凤戈,陈淦生,陈生大.FGH96镍基粉末高温合金的组织和性能[J].钢铁研究学报,2005(01):59-63.
[22] Mao J.;Chang KM.;Yang WH.;Furrer DU.;Ray K.;Vaze SP. .Cooling precipitation and strengthening study in powder metallurgy superalloy Rene88DT[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2002(1/2):318-329.
[23] 田高峰,贾成厂,刘建涛,胡本芙.固溶冷却介质对FGH96合金γ'相和性能的影响[J].材料工程,2006(12):24-27.
[24] Krueger D D;Kissinger R D;Menzies R G.Development and introduction of a damage tolerant high temperature nickelbase disk alloy Rene88DT[A].Champion:The TMS High Temperature Alloys Committee,1992:277.
[25] John J Schirra;Paul L Reynolds.Effect of microstructure (and heat treatment) on the 649℃ properties of advanced P/M superalloy disk materials[A].Champion:The TMS High Temperature Alloys Committee,2004:341.
[26] Barbosa C;Nascimento J L;Caminha I M V .Microstructural aspects of the failure analysis of nickel base superalloy components[J].Engineering Failure Analysis,2005,12:348.
[27] Piard A;Gamby D;Carbou C et al.A numerical simulation of creep-fatigue crack growth in nickel-base superalloys[J].Engineering Fracture Mechanics,2004,71:2299.
[28] 赵勇铭,宋迎东.夹杂对粉末高温合金裂纹扩展寿命的影响[J].航空动力学报,2005(05):772-777.
[29] 凌刚 .Waspaloy合金的晶粒控制及其对力学行为的影响[D].北京:北京钢铁学院,1989.
[30] Chang K M;Henry M F;Benz M G;刘先曙,陈彦婷.高温合金疲劳裂纹扩展的冶金控制[J].宇航材料工艺,1992(03):49.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%