Very high cycle fatigue properties of bainitic high carbon-chromium steel under variable amplitude conditions

被引:61
作者
Mayer, H. [1 ]
Haydn, W. [2 ]
Schuller, R. [1 ]
Issler, S. [2 ]
Bacher-Hoechst, M. [2 ]
机构
[1] BOKU, Inst Phys & Mat Sci, A-1190 Vienna, Austria
[2] Robert Bosch GmbH, Corp Res & Dev, Mat & Proc Dev Met, D-70442 Stuttgart, Germany
关键词
Very high cycle fatigue; Variable amplitude loading; Damage accumulation; High strength steel; Ultrasonic fatigue; REGIME N-GREATER-THAN-10(7) CYCLES; BEARING STEEL; CRACK INITIATION; LIFE REGIME; MECHANISM; BEHAVIOR; FAILURE; PROPAGATION; LIMIT;
D O I
10.1016/j.ijfatigue.2009.02.038
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Very high cycle fatigue (VHCF) properties of bainitic 100Cr6 (SAE 52100, JIS SUJ2) steel are studied under variable amplitude (VA) loading conditions with a cumulative frequency distribution of stress amplitudes similar to a Gauss distribution. Ultrasonic VA fatigue tests are performed at different maximum stress amplitudes, sigma(max) of the random sequence and fatigue lifetimes between 2 x 10(6) and 10(10) cycles. 42% of the fractured specimens failed from internal Al2O3-inclusions and 58% failed from the surface, predominantly from scratches or cavities produced during grinding. If sigma(max) is high, surface failures occur earlier than internal failures. If sigma(max) is close to the constant amplitude (CA) mean fatigue limit, fractures from internal inclusions occur earlier. Facets formed at inclusions in VA tests are larger than in CA tests. Linear damage accumulation calculation delivers mean damage sum S = 0.44 in experiments with mean lifetimes below 4 x 107 cycles. Decreasing sigma(max) leads to decreasing damage sums, e.g. VA experiments with mean lifetime of 9.9 x 10(8) cycles show S = 0.016. Considering surface and internal failures separately, the damage sums decrease with increasing VA lifetimes, more pronounced when the crack initiates at internal inclusions. When mean VA fatigue lifetimes are in the regime of 10(9) cycles or above, more than 99% of the stress amplitudes are below the CA mean endurance limit, and the deleterious influence of low load cycles is underestimated on the basis of CA fatigue data. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1300 / 1308
页数:9
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