采用超声高频疲劳试验机进行了LC4CS铝合金实验样本容量为66的超高周疲劳寿命实验.结果表明,超高周疲劳寿命具有双峰分布特征,这一特征与疲劳裂纹的萌生点有关:较短疲劳寿命的样品的裂纹萌生于夹杂等缺陷处,而较长疲劳寿命的样品的裂纹萌生于表面.寿命分布的双峰特征使得传统的升降法不能用于确定材料的超高周疲劳的条件疲劳极限,超高周疲劳寿命的分散性远大于低周和高周疲劳寿命的分散性.
参考文献
[1] | Naito T,Ueda H,Kikuchi M.J Soc Mater Sci,1983; 32:1162 |
[2] | Lukas P,Kunz L.Fatigue Fract Eng Mater Struct,2002;25:747 |
[3] | Emura H,Asami K.Trans JSME,1989; 55A:45 |
[4] | Kuroshima Y,Saito Y,Shimizu M,Kawasaki K.Trans JSME,1994; 60A:2710 |
[5] | Nakamura T,Kaneko M,Tanabe T,Jinbo K,Nagai F.Trans JSME,1995; 61A:441 |
[6] | Wang Q Y.J Mech Strength,2002; 24:81(王清远.机械强度,2002;24:81) |
[7] | Umezawa O,Nagai K.Metall Mater Trans,1998; 29A:809 |
[8] | Umezawa O,Nagai K.ISIJ Int,1997; 37:1170 |
[9] | Danninger H,Spoljaric D,Weiss B,Stickler R.Z Metallkd,1998; 89:135 |
[10] | Bathias C.Eng Mater Struct,1999; 22:559 |
[11] | Mugahrabi H.Fatigue Fract Eng Mater Struct,1999; 22:633 |
[12] | Murakami Y,Nomoto T,Ueda T.Mater Struct,1999; 22:581 |
[13] | Murakami Y,Takada M,Toriyama T.Int J Fatigue,1998;16:661 |
[14] | Wang Q Y,Berard J Y,Dubarre A,Baudry G,Rathery S,Bathias C.Fatigue Fract Eng Mater Struct,1999; 22:667 |
[15] | Wang Q Y,Wang Z G,Li S X.Electr Drive Locomot,2003; (Suppl.):28(王清远,王中光,李守新.机车电传动,2003;(增刊):28) |
[16] | Xue H Q,Tao H,Wang H.Mech Sci Technol,2004; 23(4):471(薛红前,陶华,王弘.机械科学与技术,2004;23(4):471) |
[17] | Xue H Q,Tao H,Wang H.J Northwest Polytech Univ,2004; 22:108(薛红前,陶华,王弘.西北工业大学学报,2004;22:108) |
[18] | Doi K,Hanami K,Teraoka T,Terauchi S,Sugimoto T.Powder Metall Technol,2005; 23:88(Doi K,Hanami K,Teraoka T,Terauchi S,Sugimoto T.粉末冶金技术,2005;23:88) |
[19] | Shao H H,Chen G.Trans Chin Soc Agric Mach,2004;35(6):185(邵红红,陈光.农业机械学报,2004;35(6):185) |
[20] | Masuda C,Nishijiama S,Tanaka Y.Trans JSME,1986;52A:847 |
[21] | Kanazawa K,Nishijima S.J Soc Mater Sci,1997; 46:1396 |
[22] | Gao Z T.Handbook of Fatigue Properties of Aeronautical Metals.Beijing:Institute of Aeronautical Materials,1981:155(高镇同.航空金属材料疲劳性能手册.北京:北京航空材料研究所,1981:155) |
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