| Citation: | Cheng Chi, Liao Mingfu, Lei Xinliang, et al. Bearability of cross-excitation modes of aero-engine dual-rotor system and its experimental verification[J]. Journal of Aerospace Power, 2026, 41(8):20240782 doi: 10.13224/j.cnki.jasp.20240782 |
To elucidate the contradictory phenomenon of the cross-excitation mode that the displacement or deformation of the excitation source rotor is very small while that of the excited rotor is absolutely dominant, the orthogonality between the force and the vibration mode is analyzed based on rotor modal analysis method and a dual-rotor model with inter-shaft bearing. A dual-rotor experimental setup was built, and modal experiment, response experiment and long-term resonance experiment were carried out. The experimental results showed that the critical speed error between the experimental results and the calculation results of the dual-rotor experimental setup was up to 3.7%, and the modal shape error was up to 9.5%. The unbalanced response during the acceleration and deceleration process had no peak at the cross-excitation mode. A long-time resonance exceeding 62 minutes was performed under the cross-excitation mode. Even if the maximum amount of applied imbalance was 145% of the coupling mode, the peak response was still less than 25% of the coupling mode. The research results fully prove that the cross-excitation mode is a mode with high acceptability, presenting vey low risk of severe vibration.
| [1] |
Meirovitch L. Fundamentals of vibrations[M]. Boston: McGraw-Hill, 2001.
|
| [2] |
顾家柳. 转子动力学[M]. 北京: 国防工业出版社, 1985.
|
| [3] |
钟一谔, 何衍宗, 王正, 等. 转子动力学[M]. 北京: 清华大学出版社, 1987.
|
| [4] |
沈达宽. 航空发动机强度计算[M]. 北京: 国防工业出版社, 1980.
|
| [5] |
廖明夫. 航空发动机转子动力学[M]. 西安: 西北工业大学出版社, 2015. Liao Mingfu. Rotor dynamics of aero-engine[M]. Xi’an: Northwestern Polytechnical University Press, 2015. (in Chinese
Liao Mingfu. Rotor dynamics of aero-engine[M]. Xi’an: Northwestern Polytechnical University Press, 2015. (in Chinese)
|
| [6] |
廖明夫, 王四季, 李全坤, 等. 航空发动机转子-支承系统的振动: 上册[M]. 北京: 科学出版社, 2023. Liao Mingfu, Wang Siji, Li Quankun, et al. Vibration of aeroengine rotor-support system: Part Ⅰ[M]. Beijing: Science Press, 2023. (in Chinese
Liao Mingfu, Wang Siji, Li Quankun, et al. Vibration of aeroengine rotor-support system: Part Ⅰ[M]. Beijing: Science Press, 2023. (in Chinese)
|
| [7] |
金路. 航空发动机转子系统动力学优化设计方法研究[D]. 西安: 西北工业大学, 2013. Jin Lu. Research on dynamic optimization design method of aero-engine rotor system[D]. Xi’an: Northwestern Poly-technical Uni-versity, 2013. (in Chinese
Jin Lu. Research on dynamic optimization design method of aero-engine rotor system[D]. Xi’an: Northwestern Poly-technical Uni-versity, 2013. (in Chinese)
|
| [8] |
王东华, 刘占生, 窦唯. 基于混合遗传算法的转子系统优化设计[J]. 振动与冲击, 2009, 28(5): 87-91. Wang Donghua, Liu Zhansheng, Dou Wei. Rotordynamics optimization based on a hybrid genetic algorithm[J]. Journal of Vibration and Shock, 2009, 28(5): 87-91. (in Chinese
Wang Donghua, Liu Zhansheng, Dou Wei. Rotordynamics optimization based on a hybrid genetic algorithm[J]. Journal of Vibration and Shock, 2009, 28(5): 87-91. (in Chinese)
|
| [9] |
刘展翅. 弹支挤压油膜阻尼器设计与特殊工况下阻尼器减振特性研究[D]. 西安: 西北工业大学, 2016. Liu Zhanchi. Study of the squeeze film dampers design and the vi-bration attenuating characteristics under special conditions[D]. Xi’an: Northwestern Polytechnical University, 2015. (in Chinese
Liu Zhanchi. Study of the squeeze film dampers design and the vi-bration attenuating characteristics under special conditions[D]. Xi’an: Northwestern Polytechnical University, 2015. (in Chinese)
|
| [10] |
李岩, 廖明夫, 蒋云帆, 等. 航空发动机双转子系统“临界跟随”现象的机理及影响[J]. 航空动力学报, 2019, 34(11): 2403-2413. Li Yan, Liao Mingfu, Jiang Yunfan, et al. Mechanism and effect of “critical follower speed” on dual-rotor system of aero-engines[J]. Journal of Aerospace Power, 2019, 34(11): 2403-2413. (in Chinese doi: 10.13224/j.cnki.jasp.2019.11.012
Li Yan, Liao Mingfu, Jiang Yunfan, et al. Mechanism and effect of “critical follower speed” on dual-rotor system of aero-engines[J]. Journal of Aerospace Power, 2019, 34(11): 2403-2413. (in Chinese) doi: 10.13224/j.cnki.jasp.2019.11.012
|
| [11] |
李岩. 航空发动机转子系统可容模态优化设计方法与实验研究[D]. 西安: 西北工业大学, 2020. Li Yan. Optimization design and experimental verification of tolerable modes of aero-engine rotor systems[D]. Xi’an: Northwestern Polytechnical University, 2020. (in Chinese
Li Yan. Optimization design and experimental verification of tolerable modes of aero-engine rotor systems[D]. Xi’an: Northwestern Polytechnical University, 2020. (in Chinese)
|
| [12] |
黄江博, 廖明夫, 雷新亮, 等. 航空发动机低压转子系统的“可容模态”设计及实验验证[J]. 航空动力学报, 2022, 37(5): 964-979. Huang Jiangbo, Liao Mingfu, Lei Xinliang, et al. Workable mode design and experimental verification of aero-engine low-pressure rotor system[J]. Journal of Aerospace Power, 2022, 37(5): 964-979. (in Chinese doi: 10.13224/j.cnki.jasp.20210578
Huang Jiangbo, Liao Mingfu, Lei Xinliang, et al. Workable mode design and experimental verification of aero-engine low-pressure rotor system[J]. Journal of Aerospace Power, 2022, 37(5): 964-979. (in Chinese) doi: 10.13224/j.cnki.jasp.20210578
|
| [13] |
赵璐, 廖明夫, 薛永广, 等. 航空发动机高压转子“可容模态”设计及实验验证[J]. 推进技术, 2022, 43(2): 318-330. Zhao Lu, Liao Mingfu, Xue Yongguang, et al. Workable mode design and experimental verification of aero-engine high pressure rotor[J]. Journal of Propulsion Technology, 2022, 43(2): 318-330. (in Chinese
Zhao Lu, Liao Mingfu, Xue Yongguang, et al. Workable mode design and experimental verification of aero-engine high pressure rotor[J]. Journal of Propulsion Technology, 2022, 43(2): 318-330. (in Chinese)
|
| [14] |
王瑞, 廖明夫, 雷新亮, 等. 带中介轴承双转子系统“可容模态”优化设计及实验[J]. 推进技术, 2023, 44(5): 240-256. Wang Rui, Liao Mingfu, Lei Xinliang, et al. Optimization design and experiment of workable mode for dual-rotor system with inter-shaft bearing[J]. Journal of Propulsion Technology, 2023, 44(5): 240-256. (in Chinese doi: 10.13675/j.cnki.tjjs.2208091
Wang Rui, Liao Mingfu, Lei Xinliang, et al. Optimization design and experiment of workable mode for dual-rotor system with inter-shaft bearing[J]. Journal of Propulsion Technology, 2023, 44(5): 240-256. (in Chinese) doi: 10.13675/j.cnki.tjjs.2208091
|
| [15] |
王瑞, 廖明夫, 程荣辉, 等. 带中介轴承双转子系统的“可容模态”优化设计方法[J]. 航空动力学报, 2024, 39(9): 47-58. Wang Rui, Liao Mingfu, Cheng Ronghui, et al. Workable mode optimization design method for dual-rotor system with inter-shaft bearing[J]. Journal of Aerospace Power, 2024, 39(9): 47-58. (in Chinese doi: 10.13224/j.cnki.jasp.20220623
Wang Rui, Liao Mingfu, Cheng Ronghui, et al. Workable mode optimization design method for dual-rotor system with inter-shaft bearing[J]. Journal of Aerospace Power, 2024, 39(9): 47-58. (in Chinese) doi: 10.13224/j.cnki.jasp.20220623
|
| [16] |
王瑞, 廖明夫, 程荣辉, 等. 航空发动机双转子系统的模态及其表达方法[J]. 振动与冲击, 2022, 41(21): 209-215, 278. Wang Rui, Liao Mingfu, Cheng Ronghui, et al. Modal characteristics and their expression method for aeroengine dual-rotor system[J]. Journal of Vibration and Shock, 2022, 41(21): 209-215, 278. (in Chinese doi: 10.13465/j.cnki.jvs.2022.21.023
Wang Rui, Liao Mingfu, Cheng Ronghui, et al. Modal characteristics and their expression method for aeroengine dual-rotor system[J]. Journal of Vibration and Shock, 2022, 41(21): 209-215, 278. (in Chinese) doi: 10.13465/j.cnki.jvs.2022.21.023
|
| [17] |
黄江博, 廖明夫, 程荣辉, 等. 航空发动机双转子系统模态正交性和不平衡响应[J]. 振动与冲击, 2022, 41(21): 176-189. Huang Jiangbo, Liao Mingfu, Cheng Ronghui, et al. Modal orthogonality and unbalance response of aeroengine dual-rotor system[J]. Journal of Vibration and Shock, 2022, 41(21): 176-189. (in Chinese
Huang Jiangbo, Liao Mingfu, Cheng Ronghui, et al. Modal orthogonality and unbalance response of aeroengine dual-rotor system[J]. Journal of Vibration and Shock, 2022, 41(21): 176-189. (in Chinese)
|
| [18] |
王瑞, 廖明夫, 黄江博. 建立双转子系统响应特性三面三维表达方式的方法: CN202210017008.3[P]. 2023-07-04.
|