Estimation of vibrational state of mistuned blade assemblies of gas turbine compressor rotor wheel

机译：燃气涡轮压缩机转子轮型迷雾叶片组件振动状态的估计

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Results of investigations involving the determination of possible causes of disk rim failure of a rotor wheel with blades, having the root of a dovetail joint type, are presented. The numerical experiments were performed using the theory of coupling vibration of mechanical systems. Numerical investigations of specific features of natural vibration spectrum of the rotor design considered and of the influence of the blade frequencies mistiming upon resonant vibrations have been performed to elucidate the cause of rather high vibration stresses in the disk rim.

机译：提出了涉及确定具有叶片的叶片的磁盘RIM失效的可能原因的研究结果，具有燕尾件的叶片的根部。使用机械系统的耦合振动理论进行数值实验。已经进行了考虑的转子设计的自然振动谱的特定特征的数值研究，并且已经进行了旋转振动对谐振振动的影响，以阐明盘边缘中相当高的振动应力的原因。

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《International Conference on Flow-Induced Vibration》|2000年||共5页
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A. P. Zinkovskii;
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1. Experimental and calculated estimations of dynamic stability of rotor wheel blade assemblies of gas-turbine engine compressors [J] . V. A. Tsimbalyuk, A. P. Zinkovskii, A. V. Poberezhnikov Проблемы прочностиПроблемы прочности: на рус．укр．и анг．языках . 2001,第6期

机译：燃气轮机压缩机转子叶片总成动态稳定性的实验和计算估计
2. Experimental and calculated estimations of dynamic stability of rotor wheel blade assemblies of gas-turbine engine compressors [J] . V. A. Tsimbalyuk, A. P. Zinkovskii, A. V. Poberezhnikov Проблемы прочностиПроблемы прочности: на рус．укр．и анг．языках . 2001,第6期

机译：燃气轮机压缩机转子轮叶片组件动态稳定性的实验性和计算估计
3. EXPERIMENTAL-CALCULATION DETERMINATION OF DYNAMIC STABILITY OF BLADE ASSEMBLIES OF GTE COMPRESSOR ROTOR WHEELS [J] . V. A. Tsymbalyuk, A. P. Zinkovskii, A. V. Poberezhnikov Strength of Materials . 2001,第6期

机译：GTE压气机转子叶片叶片动态稳定性的实验计算确定。
4. Estimation of vibrational state of mistuned blade assemblies of gas turbine compressor rotor wheel [C] . A. P. Zinkovskii International Conference on Flow-Induced Vibration . 2000

机译：燃气涡轮压缩机转子轮型迷雾叶片组件振动状态的估计
5. Three-Dimensional Finite Element Analysis of Rotors in Gas Turbines, Steam Turbines and Axial Pumps Including Blade Vibrations [D] . Chaudhry, Jawad Altaf 2011

机译：燃气轮机，蒸汽轮机和轴流泵中包括叶片振动的转子的三维有限元分析
6. Assessment of the Impact of Shot-Peening on the Fatigue Life of a Compressor Blade Subjected to Resonance Vibrations [O] . Arkadiusz Bednarz, Wojciech Z. Misiolek 2020

机译：评估射击喷丸对压缩机叶片疲劳寿命的影响经受共振振动
7. Discussion: “An Experimental Study of the Compressor Rotor Blade Boundary Layer” (Pouagare, M., Galmes, J. M., and Lakshminarayana, B., 1985, ASME J. Eng. Gas Turbines Power, 107, pp. 364–372) [O] . J. Moore 1985

机译：讨论：“压缩机转子叶片边界层的实验研究”（Pougare，M.，Galmes，J. M.和Lakshminarayana，B.，1985，Asme J. Eng。燃气轮机功率，107，PP。364-372）

Estimation of vibrational state of mistuned blade assemblies of gas turbine compressor rotor wheel

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