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以经过表面强化后的国产某轿车变速箱齿轮为例,根据齿根附近沿深度的残余应力和硬度的分布对单齿弯曲疲劳强度和疲劳裂纹萌生区域的预测进行了分析和试验验证.通过强度和硬度之间的转换关系以及疲劳强度与残余应力的作用关系,得到了齿根附近沿深度的弯曲疲劳极限分布,齿根次表面下0.25~0.45mm之间的区域是疲劳危险区.齿轮表面强化的结果使得齿轮弯曲疲劳裂纹源从表面转入到次表面,并初步得到了微观验证.研究结果说明了基于残余应力和硬度可以进行疲劳强度和疲劳裂纹萌生区域的预测.

参考文献

[1] Basinski Z S;Basinski S J .Low amplitude fatigue of copper single crystals-I].Surface obaervatioas[J].ACTA METALLURGICA,1985,33(07):1307-1317.
[2] E.A.REPETTO;M.ORTIZ .A MICROMECHANICAL MODEL OF CYCLIC DEFORMATION AND FATIGUE-CRACK NUCLEATION IN f.c.c. SINGLE CRYSTALS[J].Acta materialia,1997(6):2577-2595.
[3] D. Radaj .Review of fatigue strength assessment of nonwelded and welded structures based on local parameters[J].International Journal of Fatigue,1996(3):153-170.
[4] Suresh S.Fatigue of Materials[M].Cambridge,Mass:Cambridge University Press,1991:97-118.
[5] 姚枚;王声平;李金魁 等.表面强化件的疲劳强度分析及金属的内部疲劳极限[J].金属学报,1993,29(11):511-519.
[6] 姚枚,王仁智.金属材料工程力学行为学及其微细观过程理论[J].机械工程学报,2000(11):1-4,15.
[7] Yu-kui Gao;Mei Yao;Pei-ge Shao .Another Mechanism for Fatigue Strength Improvement of Metallic Parts by Shot Peening[J].Journal of Materials Engineering and Performance,2003(5):507-511.
[8] Brinckmann S;Van der Giessen E.Towards understanding fatigue crack initiation:a discrete dislocation dynamics study[A].Geneva,2003
[9] 张定铨.残余应力对金属疲劳强度的影响[J].理化检验-物理分册,2002(06):231-235.
[10] 赵少汴;王忠保.抗疲劳设计-方法与数据[M].北京:机械工业出版社,1997:248-258.
[11] 山田敏郎;王庆荣.金属材料疲劳设计手册[M].成都:四川科学技术出版社,1988:107-112.
[12] Masuda C;Nishijima S;Tanaka Y .Relationship between fatigue strength and hardness for high strength steels[J].Traas JSME,1986,52A:847-852.
[13] Kutz M.Mechanical Engineers' Handbook,Materials and Mechanical Design (Hardcover)[M].Wiley Press,2005:160.
[14] Shengping Wang .Relationship between the fatigue limit and the mechanical strength of metals[J].Journal of Materials Processing Technology,2000(1/3):42-46.
[15] Lankford J .Initiation and early growth of fatigue erecks in high strength ateels[J].Engineering Fractore Mechanies,1977,35(09):617-624.
[16] Walter Schlitz .A history of fatigue[J].Engineering Fracture Mechanics,1996,54(02):263-300.
[17] 郑修麟.屈服强度与裂纹形成寿命的关系[J].航空学报,1989(08):439.
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