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焦胜博*,程礼,陈煊,陈皎,鲁凯举,高潮.Ti-6Al-4V钛合金振动弯曲超高周疲劳及寿命预测模型研究[J].实验力学,2016,31(6):730~740
Ti-6Al-4V钛合金振动弯曲超高周疲劳及寿命预测模型研究
On the Very High Cycle Fatigue and Life Prediction Model of Ti-6Al-4V Titanium Alloy Subjected to Vibration Bending
投稿时间:2016-08-15  修订日期:2016-10-10
DOI:10.7520/1001-4888-16-306
中文关键词:  超高周疲劳  振动弯曲  频率效应  寿命预测
英文关键词:very high cycle fatigue  vibration bending  frequency effect  life prediction model
基金项目:国家自然科学基金青年人才项目(11402302)
作者单位
焦胜博* 空军工程大学 航空航天工程学院 西安 710038 
程礼 1.空军工程大学 航空航天工程学院 西安 710038 2.先进航空发动机协同创新中心 北京 100000 
陈煊 空军工程大学 航空航天工程学院 西安 710038 
陈皎 空军工程大学 航空航天工程学院 西安 710038 
鲁凯举 空军工程大学 航空航天工程学院 西安 710038 
高潮 航空工程技术研究中心 北京 100000 
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中文摘要:
      运用超声疲劳试验系统和高频振动弯曲疲劳试验系统开展了Ti-6Al-4V钛合金在300Hz和20kHz下的高周和超高周振动弯曲疲劳试验。使用Hirox光学成像系统和扫描电镜观察了试样断口形貌,提出了使用振动幅值和共振频率的乘积af表征试样应力大小的方法,建立了基于af值的超高周弯曲振动疲劳寿命预测模型并进行了验证。结果表明:疲劳循环周数超过107以后,Ti-6Al-4V钛合金试样依然会发生疲劳断裂,不存在传统意义上的疲劳极限;同轴向拉压疲劳相比,相同疲劳寿命下,振动弯曲的应力水平显著小于轴向拉压加载;300Hz和20kHz两种频率下的试验数据吻合良好,加载频率对材料的疲劳性能没有明显影响。由于试样中应力梯度分布,裂纹均萌生于试样表面,试样断口平坦,裂纹源并未呈现“鱼眼”特征。基于af值的疲劳寿命预测模型能够很好地预测超高周振动弯曲疲劳寿命。
英文摘要:
      Vibration bending fatigue experiment of Ti-6Al-4V titanium alloy were carried out under 300Hz high cycle and 20kHz very high cycle condition respectively, based on ultrasonic fatigue test system and high frequency vibration bending fatigue test system. In this paper, the fracture morphology of specimen was observed by Hirox optical imaging system and scanning electron microscope; a method was proposed to characterize stress size of specimen by using the product af of vibration amplitude and resonance frequency; then, based on af value, a prediction model of vibration fatigue life under very high cycle bending vibration condition was established and verified. Results indicate that when fatigue cycle times exceed 107,Ti-6Al-4V titanium alloy still presents fatigue fracture, there is not conventional fatigue limit; comparing with axial tension-compression fatigue, the stress level in vibration bending is obviously smaller than that in tension-compression loading; the experimental data obtained under 300Hz and 20kHz frequency are in good agreement, which indicates that the loading frequency has not obvious effect on fatigue performance. All cracks initiate at specimen surface due to the gradient distribution of stress in specimen. The fracture surface of specimen is flat and smooth, and the crack source did not show “fish eye” features. The fatigue life prediction model based on af value can well predict bending fatigue life in very high cycle vibration bending.
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