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钛合金疲劳裂纹扩展速率试验及预报方法
引用本文:王珂,黄翔宇,李永正,张世鑫,卞程程,高龙乾.钛合金疲劳裂纹扩展速率试验及预报方法[J].舰船科学技术,2021(3):14-18.
作者姓名:王珂  黄翔宇  李永正  张世鑫  卞程程  高龙乾
作者单位:江苏科技大学船舶与海洋工程学院
基金项目:国家自然科学基金青年基金资助项目(BK20160559);国家自然科学基金资助项目(51709134);国家重点研发计划(2016YFCO300603-02)。
摘    要:本文针对深海载人潜水器耐压壳用钛合金,开展疲劳性能试验研究,得到该类型钛合金的室温断裂韧性,载荷比R=0.1下的疲劳裂纹扩展门槛值及疲劳裂纹扩展速率,基于选用的疲劳裂纹扩展预报模型,对载荷比R=0.1下的钛合金疲劳裂纹扩展行为进行了预报研究。结果表明:在载荷比不变的前提下,应力强度因子范围是疲劳裂纹扩展速率的主要影响因素,应力强度因子范围的增加会导致疲劳裂纹扩展速率增加;考虑小裂纹效应的疲劳裂纹扩展预报模型可对钛合金的疲劳裂纹扩展行为进行准确预报。

关 键 词:钛合金  断裂韧性  疲劳裂纹扩展门槛值  疲劳裂纹扩展速率  疲劳裂纹扩展预报

Test and prediction of fatigue crack growth rate of titanium alloy materials
WANG Ke,HUANG Xiang-yu,LI Yong-zheng,ZHANG Shi-xin,BIAN Cheng-cheng,GAO Long-qian.Test and prediction of fatigue crack growth rate of titanium alloy materials[J].Ship Science and Technology,2021(3):14-18.
Authors:WANG Ke  HUANG Xiang-yu  LI Yong-zheng  ZHANG Shi-xin  BIAN Cheng-cheng  GAO Long-qian
Institution:(School of Naval Architecture and Ocean Engineering,Jiangsu University of Science and Technology,Zhenjiang 212003,China)
Abstract:In this paper, the fatigue performance test of titanium alloy materials for pressure-resistant shells of deep-sea manned submersibles is carried out. The fracture toughness of titanium alloy and the fatigue crack growth threshold and fatigue crack growth rate curve at load ratio R=0.1 are obtained. Finally, using the fatigue crack propagation prediction model of titanium alloy material, the fatigue crack propagation behavior of titanium alloy at load ratio R=0.1 was predicted. The results show that the stress intensity factor range is the main influencing factor of fatigue crack growth rate under the premise of constant load ratio. The increase of stress intensity factor range will lead to the increase of fatigue crack growth rate. The fatigue crack propagation prediction model which considering small fatigue crack effect can predict of fatigue crack growth behavior of titanium alloys accurately.
Keywords:titanium alloy material  fracture toughness  fatigue crack growth threshold  fatigue crack growth rate  fatigue crack propagation prediction
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