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| 1 | Dynamic Characteristics of Rotor System with a Slant Crack Based on Fractional Damping显示文摘The traditional modeling method of rotor system with a slant crack considers only integer-order calculus.However,the model of rotor system based on integer-order calculus can merely describe local characteristics,not historical dependent process.The occur of fractional order calculus just makes up for the deficiency in integer-order calculus.Therefore,a new dynamic model with a slant crack based on fractional damping is proposed.Here,the stiffness of rotor system with a slant crack is solved by zero stress intensity factor method.The proposed model is simulated by Runge-Kutta method and continued fraction Euler method.The influence of the fractional order,rotating speed,and crack depth on the dynamic characteristics of rotor system is discussed.The simulation results show that the amplitude of torsional excitation frequency increases significantly with the increase of the fractional order.With the increase of the rotating speed,the amplitude of first harmonic component becomes gradually larger,the amplitude of the second harmonic becomes smaller,while the amplitude of the other frequency components is almost invariant.The shaft orbit changes gradually from an internal 8-type shape to an ellipse-type shape without overlapping.With the increase of the slant crack depth,the amplitude of the transverse response frequency in the rotor system with a slant crack increases,and the amplitude in the second harmonic component also increases significantly.In addition,the torsional excitation frequency and other coupling frequency components also occur.The proposed model is further verified by the experiment.The valuable conclusion can provide an important guideline for the fault diagnosis of rotor system with a slant crack. | Zhinong Li Yunlong Li Dong Wang Zhike Peng Haifeng Wang | 2021 | Chinese Journal of Mechanical Engineering2021，34，2： | 2 |
| 2 | 航空发动机轮盘模拟件裂纹预制分析与试验研究显示文摘航空事故数据显示,航空发动机轮盘运行可靠性已成为飞行安全的决定性因素之一,及时有效的发现并排除轮盘结构缺陷有着非常重大的实际价值。为了给轮盘损伤识别研究提供必要基础,提出一种可行的轮盘结构裂纹预制方法。为此,首先对轮盘模拟件中V型缺口根部应力奇异性分布特征进行了理论分析;其次,根据载荷条件和几何特征提出载荷等效方法,并进行了应力状态及疲劳分析。为了验证所提裂纹预制方法的可行性,对预制模型进行疲劳试验研究。试验结果显示,相应位置处x方向应力和疲劳循环载荷次数相对误差约为2.7%和12.7%。同时证实所采取的裂纹预制与相应数值分析方法可以应用于航空发动机轮盘损伤识别方法的研究中。 | 刘若楠 耿佳 张瑞玲 陈雪峰 | 2019 | 机械工程学报2019，55，13： | 2 |
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