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基于缺陷分布形式的粉末冶金涡轮盘可靠度计算模型 被引量:5

Model for Calculating the Reliability of Powder Metallurgy Turbine Disk Based on Distribution of Defects
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摘要 为研究微缺陷对粉末冶金涡轮盘可靠性的影响,在有限元分析结果的基础上,基于国内粉末盘中缺陷分布的概率特点,建立针对低循环疲劳裂纹萌生和裂纹扩展失效模式的可靠度计算模型。该模型可计算不同缺陷分布形式、不同循环载荷条件下的轮盘可靠度。对某型粉末盘失效概率的分析表明:表面质量是导致粉末盘失效的重要因素,这同大量试验研究结果相一致,对粉末盘的设计和使用具有工程指导意义。 In order to research the effect of micro defects on the performance of powder metallurgy (PM) turbine disk, a reliability calculation model based on the probabilistic character of distribution of defects is established by using the results of finite element analysis, which is aimed at the failure mode of crack initiation and propagation under low cycle fatigue. The model can be used to calculate the reliability of PM turbine disk under different distribution of defects and different cyclic loading conditions. Then failure analysis ofa PM turbine disk indicates that the surface quality is an important factor leading to failure of PM turbine disk, and that is in good agreement with a great deal of experimental results. So the model can be used to guide the engineering design and application of PM turbine disk.
出处 《机械工程学报》 EI CAS CSCD 北大核心 2008年第11期132-137,共6页 Journal of Mechanical Engineering
关键词 粉末冶金涡轮盘 缺陷 临界尺寸 可靠性 Powder metallurgy turbine disk Defects Critical size Reliability
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  • 1周晓明,汪武祥,杨洪涛,唐定中,颜鸣皋.HIP态FGH96合金中人工加入非金属夹杂物的特征[J].航空材料学报,2005,25(4):1-5. 被引量:12
  • 2张莹 陈生大 等.用等离子旋转电极法制取镍基高温合金粉末工艺的研究[J].金属学报,1999,35(2):343-347.
  • 3[2]中国航空材料手册编委会.中国航空材料手册,第五卷:粉末高温合金[M].第二版.北京:中国标准出版社,2002.29-47.
  • 4[3]WANG Wu-xiang,MAO Jian,YANG Wan-hong,et al.The development and application of HIP of superalloys in aviation industries of China[A].International Conference on (HIP'99)[C].Beijing:IAP,1999.58-69.
  • 5邹金文,汪武祥.粉末高温合金中夹杂物特征及其对材料断裂行为影响的研究[J].金属学报,1999,35(10):81-84.
  • 6[6]HE Feng,WANG Wu-xiang.Study of P/M superalloy blisk prepared by HIP diffusion bonding[A].International Conference on (HIP' 02)[C].Moscow Russia:VILS,2002.75-80.
  • 7Bernstein H L.An Evaluation of Four Current Models to Predict the Creep-Fatigue Interaction in Rene 95 [R].AFMLTR-79-4075,1979.
  • 8Hyzak J M.The Effect of Defects on the Fatigue Crack Initiation Process in Two P/M Superalloys[R].AFML-TR-80-4063,Air Force Materials Laboratory,Wright-Patterson AFB,Ohio,1980.
  • 9Gayda J,Gabb T P,Miner R V.Fatigue Crack Propagation of Nickel-Base Superalloys at 650C [R].NASA-TM-87150,1985.
  • 10Pelloux R M,Romanoski G R,Feng J.Study of the Fatigue Behavior of Short Cracks in Nickel-Based Superalloys[R].AFOSRTR-86-0224,1986.

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