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某型发动机第2级涡轮叶片低循环疲劳寿命分析 被引量:4
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作者 刘存 孙志刚 +1 位作者 胡绪腾 宋迎东 《航空发动机》 2009年第2期30-33,共4页
对改型后的某型发动机第2级涡轮叶片进行了热弹性有限元应力分析,结果表明在发动机各功率状态下,第2级涡轮叶片始终处于弹性应力范围,最大应力始终位于叶片和轮盘的交界部位;采用EGD-3应力标准中的应力疲劳分析方法,分别按假设的最好和... 对改型后的某型发动机第2级涡轮叶片进行了热弹性有限元应力分析,结果表明在发动机各功率状态下,第2级涡轮叶片始终处于弹性应力范围,最大应力始终位于叶片和轮盘的交界部位;采用EGD-3应力标准中的应力疲劳分析方法,分别按假设的最好和最差的S-N曲线,估算了第2级涡轮叶片的低循环飞行小时寿命。 展开更多
关键词 航空发动机 涡轮叶片 热弹性有限元分析 低循环疲劳 寿命预测
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Determination of a U-Notch Stress Concentration Factor Using Thermoelasticity
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作者 R. B. Vieira S. Kurunthottikkal Philip +3 位作者 G. L. G. GonzAiles Jose L. F. Freire B. Yang R. E. Rowlands 《Journal of Mechanics Engineering and Automation》 2016年第2期66-76,共11页
This paper uses the TSA (therrnoelastic stress analysis) technique to determine the stress concentration factor (Kt) of a U-notch in an aluminum plate, and then compares the results with those obtained from a FEA ... This paper uses the TSA (therrnoelastic stress analysis) technique to determine the stress concentration factor (Kt) of a U-notch in an aluminum plate, and then compares the results with those obtained from a FEA (finite elements analysis) of the same specimen. In order to do so, it devises a calculation procedure to extrapolate the thermoelastic data near the tip of the notch and then applies the resulting algorithm to seven distinct experiments that had different loading frequencies, mean loads and load ranges. The overall positive results suggest that the technique may be suitable for Kt measurements in real-world structures. A discussion about the calibration factor of the thermoelastic data is included by confronting the calibration results using independent tensile uniaxial tests and using the U-notch TSA and FEA paired specimen data. 展开更多
关键词 THERMOELASTICITY INFRARED TSA stress concentration U-notch.
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