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基于缺陷概率特点的粉末冶金材料寿命预测概率模型 被引量:10

A Probabilistic Model for Prediction of Life Based on Probabilistic Character of Defects in PM Alloys
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摘要 粉末冶金材料由于其制造工艺的特点,强度和寿命对微缺陷(夹杂、气孔、表面划伤)十分敏感,导致了粉末冶金材料的破坏具有较大的分散性,使得寿命预测更为困难.本文根据国内粉末材料中缺陷的分布特点,基于文献[7~9]中概率断裂分析的思路,对原有方法进行了修正和推广,重新给出了缺陷在表面、亚表面以及内部时的定义及缺陷在这些不同位置时出现概率断裂的确定方法,建立了一个可考虑缺陷形状、大小、位置等分布特征的粉末冶金材料寿命预测概率模型,并基于此计算了不同尺寸缺陷位于不同位置时材料的失效概率及总失效概率.分析表明:所给出的方法可以很好的表征国内工艺条件下粉末冶金材料缺陷的概率特征对强度寿命的影响,方法是有效的. Due to manufacturing characteristic, the strength and life of powder metallurgy alloy are sensitive to micro defects,such as nonmetallic inclusion ,pores,and nicks on the surface. A distinct character of failure of this kind of material is scatter,which makes life prediction more difficult. In this paper,based on the defect populations of domestic PM alloy and some probability failure methods established in reference [7- 9] ,definition of the probability for the presence of a defect inside the surface,sub-surface and internal region is given first, and then a probabilistic model is set up, which can calculate the failure probability caused by defects having different shapes and different sizes, being in different regions, and also can calculate the total failure probability. It is concluded that the method can describe the effect of probabilistic character of defects on the strength and life of PM alloy,and it is proved to be valid.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2005年第6期951-957,共7页 Journal of Aerospace Power
关键词 航空 航天推进系统 粉末冶金 缺陷 临界尺寸 概率 aerospace propulsion system probabilistic powder metallurgy defects critical size probabilistic
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参考文献18

  • 1Bernstein H L.An Evaluation of Four Current Models to Predict the Creep-Fatigue Interaction in Rene 95 [R].AFMLTR-79-4075,1979. 被引量:1
  • 2Hyzak 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. 被引量:1
  • 3Gayda J,Gabb T P,Miner R V.Fatigue Crack Propagation of Nickel-Base Superalloys at 650C [R].NASA-TM-87150,1985. 被引量:1
  • 4Pelloux R M,Romanoski G R,Feng J.Study of the Fatigue Behavior of Short Cracks in Nickel-Based Superalloys[R].AFOSRTR-86-0224,1986. 被引量:1
  • 5Pelloux R M.Study of the Fatigue Behavior of Small Cracks in Nickel-Based Superalloys [R].AFOSR-TR-88-0457,1988. 被引量:1
  • 6BrüCkner-Foit A.Prediction of the Lifetime Distribution of High-Strength Components Subjected to Fatigue Loading[J].Fatigue Fract.Engng.Mater.Struct.,1993,16 (8):891 ~908. 被引量:1
  • 7Bussac A de,Lautridou J C.A Probabilistic Model for Prediction of LCF Surface Crack Initiation in PM Alloys[J].Fatigue Fract.Engng Mater.Struct.,1993,16 (8):861 ~ 874. 被引量:1
  • 8Bussac A de.Prediction of the Competition between Surface and Internal Fatigue Crack Initiation in PM Alloys [J].Fatigue Fruct.Engng Mater.Struct.,1994,17 (11):1319 ~1325. 被引量:1
  • 9Grison J,Remy L.Fatigue Failure Probability in a Powder Metallurgy Ni-Base Superalloy[J].Engineering Fracture Mechanics,1997,57(1):41~55. 被引量:1
  • 10Timothy P Gabb.Assessments of Low Cycle Fatigue Behavior of Powder Metallurgy Alloy U720[J].Fatigue and Fracture Mechanics,2000,31:110 ~ 127. 被引量:1

二级参考文献14

  • 1宋迎东,温卫东,高德平,宋迎.粉末冶金涡轮盘的应用及寿命研究[J].航空动力学报,1996,11(3):294-298. 被引量:17
  • 2侯静泳.粉末冶金的疲劳断裂性能研究.第七届航空发动机结构强度振动学术会论文集[M].洛阳,1994.. 被引量:1
  • 3汪武祥 邹金文.FGH95粉末高温合金的缺陷对材料低周疲劳性能的影响[J].北京科技大学学报(增刊),1991,13:125-125. 被引量:2
  • 4邹金文 汪武祥.粉末高温合金中夹杂物特性及其对材料断裂行为的影响[J].金属学报,1999,35(10):381-381. 被引量:2
  • 5侯静泳.粉末盘合金的疲劳断裂性能研究.第七届航空发动机结构强度振动学术会议论文集[M].洛阳,1994.. 被引量:1
  • 6邹金文,金属学报,1999年,35卷,增刊,381页 被引量:1
  • 7汪武祥,北京科技大学学报,1991年,13卷,增刊,125页 被引量:1
  • 8张德堂,钢中非金属夹杂物鉴别,1991年,6卷,220页 被引量:1
  • 9 Marguez C etal.International Journal of powder Metallurgy,1989,25(4):308,301 被引量:1
  • 10АношкинН,Ф,кошелевВЯидр.жаропрочныеитугоплавкиесплавы,ВИЛС,Москва,1990,р341-346 被引量:1

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二级引证文献47

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