Surface and subsurface cracks in rolling contact fatigue of hardened components

被引:47
作者
Bormetti, E [1 ]
Donzella, G [1 ]
Mazzù, A [1 ]
机构
[1] Univ Brescia, Dipartimento Ingn Meccan, I-25073 Brescia, Italy
关键词
rolling contact fatigue; crack propagation; hardened components; inclusions;
D O I
10.1080/10402000208982550
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The competitive aspect of surface and subsurface fatigue crack propagation in hardened components subjected to rolling contact fatigue is highlighted, the farmer being greatly affected by the working conditions (in particular the presence of tangential stresses and lubricant), the latter depending mainly on the inclusions content and on the hardness profile. In order to determine which one of these kinds of damage is favoured, initial data consisting of contact load, rolling and sliding speed, rheological properties of the lubricant, material hardness and inclusions content are necessary. The concurrent role of asperities and Hertzian stress field in determining surface crack propagation is explained with the approach of the "quiescent zone," calculating the stress intensity factors range in a contact cycle and considering the pumping effect of the fluid possibly present on the contact surface. Inherent defects (especially oxides) are thought to be responsible for subsurface cracks origin and the Murakami formula,for short cracks is extrapolated to describe their growth threshold, which also depends on the hardness and therefore on the depth in surface hardened components. A crack propagation index is then defined as a ratio of applied to threshold stress intensity factor, both for surface and subsurface cracks. Evaluating this index for a general operating condition, it is possible to determine which damage mechanism is favoured, taking into account the decisive effect on the hardness profile.
引用
收藏
页码:274 / 283
页数:10
相关论文
共 38 条
[1]  
ADAMINI R, 2001, P 18 CONV TRATT TERM
[2]  
AUCLAIR G, 1997, ASTM STP, V978
[3]  
BEGHINI M, 1999, INT JOUR FRACTURE, P1
[4]  
BENEDETTI M, 2001, P 30 AIAS C ALGH, P263
[5]  
BENUZZI D, 2001, P 30 AIAS C ALGH, P293
[6]  
BERETTA S, 1998, 27 CONV NAZ AUAS PER, P249
[7]  
BUCHER E, 2000, P 5 INT C CONT MECH, P96
[8]   Semi-analytical modeling of crack initiation dominant contact fatigue life for roller bearings [J].
Cheng, WQW ;
Cheng, HS .
JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME, 1997, 119 (02) :233-240
[9]  
DONZELLA G, 2001, P 10 INT C FRACT HON
[10]  
DONZELLA G, 2000, P 29 AIAS C RIM, P407