船舶力学
船舶力學
선박역학
JOURNAL OF SHIP MECHANICS
2014年
6期
678-689
,共12页
王珂%王芳%崔维成%李冬琴
王珂%王芳%崔維成%李鼕琴
왕가%왕방%최유성%리동금
疲劳小裂纹%疲劳裂纹扩展速率%疲劳裂纹门槛值
疲勞小裂紋%疲勞裂紋擴展速率%疲勞裂紋門檻值
피로소렬문%피로렬문확전속솔%피로렬문문함치
short fatigue cracks%fatigue crack propagation rate%crack propagation threshold%unified fatigue life prediction
在低应力强度因子范围下,许多材料都表现出疲劳小裂纹扩展速率高于长疲劳裂纹扩展速率,这对于准确预报材料寿命具有很大影响。文章在统一疲劳寿命预报模型基础上,提出疲劳小裂纹扩展速率预报公式。该预报公式不但考虑了疲劳小裂纹尖端的弹塑性行为,还考虑了疲劳小裂纹阶段控制裂纹扩展的是疲劳极限,而不是控制大裂纹扩展的应力强度因子门槛值,小裂纹扩展门槛值是裂纹长度的函数。利用该预报公式计算常幅载荷下切口试件和无切口试样的疲劳小裂纹扩展速率,并对试样进行寿命预报,预报结果与试验结果吻合较好。
在低應力彊度因子範圍下,許多材料都錶現齣疲勞小裂紋擴展速率高于長疲勞裂紋擴展速率,這對于準確預報材料壽命具有很大影響。文章在統一疲勞壽命預報模型基礎上,提齣疲勞小裂紋擴展速率預報公式。該預報公式不但攷慮瞭疲勞小裂紋尖耑的彈塑性行為,還攷慮瞭疲勞小裂紋階段控製裂紋擴展的是疲勞極限,而不是控製大裂紋擴展的應力彊度因子門檻值,小裂紋擴展門檻值是裂紋長度的函數。利用該預報公式計算常幅載荷下切口試件和無切口試樣的疲勞小裂紋擴展速率,併對試樣進行壽命預報,預報結果與試驗結果吻閤較好。
재저응력강도인자범위하,허다재료도표현출피로소렬문확전속솔고우장피로렬문확전속솔,저대우준학예보재료수명구유흔대영향。문장재통일피로수명예보모형기출상,제출피로소렬문확전속솔예보공식。해예보공식불단고필료피로소렬문첨단적탄소성행위,환고필료피로소렬문계단공제렬문확전적시피로겁한,이불시공제대렬문확전적응력강도인자문함치,소렬문확전문함치시렬문장도적함수。이용해예보공식계산상폭재하하절구시건화무절구시양적피로소렬문확전속솔,병대시양진행수명예보,예보결과여시험결과문합교호。
The observation that the short fatigue cracks grow faster than long fatigue cracks at the same nominal driving force and even grow at stress intensity factor range below the threshold value for long cracks in many materials. The anomalous behaviors of short cracks have a great influence on the accurate fatigue life prediction of marine structure. Based on the unified fatigue life prediction model developed in the authors group, a modified model of short fatigue crack propagation is pro-posed in this paper. The elastic-plastic behavior of short fatigue cracks in the vicinity of crack tips is considered in the modified model. The modified model includes that the rate of crack propagation for very short cracks is determined by the range of cyclic stress rather than the range of the intensity factor controlling the long cracks propagation. The threshold stress intensity factor range of short fa-tigue cracks is a function of crack length. The proposed model is used to calculate short cracks prop-agation rate and the corresponding fatigue life for notched specimens under constant amplitude load-ing. And the model is validated by comparing model prediction results with the experimental data.