| Citation: | CHEN Guowang, TANG Qian, LI Heng, et al. Response prediction modeling and experiment study of helicopter tail drive system[J]. Journal of Aerospace Power, 2025, 40（7）：20240364 doi: 10.13224/j.cnki.jasp.20240364
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To solve the problem of predicting the vibration response of the helicopter tail drive system during actual operation, a model for predicting the response of the helicopter tail drive system based on rigid-flexible coupled multibody dynamics was established. A simulation test bench of the system was built to analytically compare with the predicted value of the proposed model. The results showed that the response prediction model of the system can reflect the meshing frequency and the octave components consistent with the test data, and the error of the effective value of the vibration acceleration was within the range of −23.9%—20.6% under the conditions of variable rotational speed and variable load, which proved that the reliability of the proposed vibration response prediction method was demonstrated in the comparative results. The results provide a theoretical and experimental basis for the high safety service of helicopters.
| [1] |
许兆棠,朱如鹏. 直升机尾传动系扭转振动的分析[J]. 航空学报,2007,28(2): 425-431. XU Zhaotang,ZHU Rupeng. Torsional vibration analysis for a helicopter tail drive system[J]. Acta Aeronautica et Astronautica Sinica,2007,28(2): 425-431. (in Chinese doi: 10.3321/j.issn:1000-6893.2007.02.034
XU Zhaotang, ZHU Rupeng. Torsional vibration analysis for a helicopter tail drive system[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(2): 425-431. (in Chinese) doi: 10.3321/j.issn:1000-6893.2007.02.034
|
| [2] |
丛家勇. 直升机尾传动系统的动力学分析[D]. 南京: 南京航空航天大学,2008. CONG Jiayong. Dynamic analysis of helicopter tail drive system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2008. (in Chinese
CONG Jiayong. Dynamic analysis of helicopter tail drive system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2008. (in Chinese)
|
| [3] |
朱自冰,朱如鹏,鲍和云,等. 刚度对直升机尾传动系统弯曲振动固有频率影响的分析[J]. 航空动力学报,2009,24(1): 176-180. ZHU Zibing,ZHU Rupeng,BAO Heyun,et al. Analysis for stiffness on the bend vibration natural frequencies of a helicopter tail drive system[J]. Journal of Aerospace Power,2009,24(1): 176-180. (in Chinese
ZHU Zibing, ZHU Rupeng, BAO Heyun, et al. Analysis for stiffness on the bend vibration natural frequencies of a helicopter tail drive system[J]. Journal of Aerospace Power, 2009, 24(1): 176-180. (in Chinese)
|
| [4] |
RUI Xiaoting,ABBAS L K,YANG Fufeng,et al. Flapwise vibration computations of coupled helicopter rotor/fuselage: application of multibody system dynamics[J]. AIAA Journal,2018,56(2): 818-835. doi: 10.2514/1.J056591
|
| [5] |
杨扬. 直升机尾传动系统的动力学有限元分析研究[D]. 南京: 南京航空航天大学,2008. YANG Yang. Dynamic finite element analysis of helicopter tail drive system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2008. (in Chinese
YANG Yang. Dynamic finite element analysis of helicopter tail drive system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2008. (in Chinese)
|
| [6] |
艾平贵. 直升机尾传动系统的横向振动和扭转振动分析[D]. 南京: 南京航空航天大学,2009. AI Pinggui. Analysis of lateral vibration and torsional vibration of helicopter tail drive system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2009. (in Chinese
AI Pinggui. Analysis of lateral vibration and torsional vibration of helicopter tail drive system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009. (in Chinese)
|
| [7] |
朱自冰. 直升机尾传动系统动力学关键问题研究[D]. 南京: 南京航空航天大学,2012. ZHU Zibing. Research on key problems of helicopter tail drive system dynamics[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2012. (in Chinese
ZHU Zibing. Research on key problems of helicopter tail drive system dynamics[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012. (in Chinese)
|
| [8] |
龚明. 某轻型直升机尾传动系统动力学分析[D]. 沈阳: 东北大学,2014. GONG Ming. Dynamic analysis of tail drive system of a light helicopter[D]. Shenyang: Northeastern University,2014. (in Chinese
GONG Ming. Dynamic analysis of tail drive system of a light helicopter[D]. Shenyang: Northeastern University, 2014. (in Chinese)
|
| [9] |
NIE Junfeng,YU Guangbin,SONG Ye,et al. Dynamic characteristic simulation of helicopter tail drive shaft system[J]. International Journal of Smart Home,2016,10(6): 95-106. doi: 10.14257/ijsh.2016.10.6.11
|
| [10] |
李永超. 基于ANSYS的直升机尾传动系统动力学特性研究[D]. 沈阳: 东北大学,2017. LI Yongchao. Study on dynamic characteristics of helicopter tail drive system based on ANSYS[D]. Shenyang: Northeastern University,2017. (in Chinese
LI Yongchao. Study on dynamic characteristics of helicopter tail drive system based on ANSYS[D]. Shenyang: Northeastern University, 2017. (in Chinese)
|
| [11] |
ZHU Haimin,CHEN Weifang,ZHU Rupeng,et al. Modeling and dynamic analysis of spiral bevel gear coupled system of intermediate and tail gearboxes in a helicopter[J]. Proceedings of the Institution of Mechanical Engineers: Part C Journal of Mechanical Engineering Science,2021,235(22): 5975-5993. doi: 10.1177/0954406221992798
|
| [12] |
李德玉,胡玉梅,杨广勇,等. 基于精细有限元法的直升机尾传动系统振动特性研究[J]. 机械研究与应用,2022,35(2): 1-5. LI Deyu,HU Yumei,YANG Guangyong,et al. Study on vibration characteristics of helicopter tail drive system based on fine finite element method[J]. Mechanical Research & Application,2022,35(2): 1-5. (in Chinese
LI Deyu, HU Yumei, YANG Guangyong, et al. Study on vibration characteristics of helicopter tail drive system based on fine finite element method[J]. Mechanical Research & Application, 2022, 35(2): 1-5. (in Chinese)
|
| [13] |
陈岩. 直升机尾传动系统结合部参数识别与动态特性分析[D]. 重庆: 重庆大学,2022. CHEN Yan. Parameter identification and dynamic characteristics analysis of helicopter tail drive system joint[D]. Chongqing: Chongqing University,2022. (in Chinese
CHEN Yan. Parameter identification and dynamic characteristics analysis of helicopter tail drive system joint[D]. Chongqing: Chongqing University, 2022. (in Chinese)
|
| [14] |
陈材,石全,王广彦,等. 基于ADAMS 的齿轮传动系统刚柔耦合模型的动力学仿真[J]. 东华大学学报,2016,33(2): 192-195. CHEN Cai,SHI Quan,WANG Guangyan,et al. Dynamic simulation of rigid-flexible coupling model of gear transmission system based on ADAMS[J]. Journal of Donghua University: English Edition,2016,33(2): 192-195. (in Chinese
CHEN Cai, SHI Quan, WANG Guangyan, et al. Dynamic simulation of rigid-flexible coupling model of gear transmission system based on ADAMS[J]. Journal of Donghua University: English Edition, 2016, 33(2): 192-195. (in Chinese)
|
| [15] |
CHEN Cheng,GUO Wei,HUANG Lingjian. A rigid-flexible coupled model for a planetary gearbox with tooth crack and its dynamic response analyses[C]//Proceedings of Prognostics and System Health Management Conference. Piscataway,US: IEEE,2016: 1-6.
|
| [16] |
LIU Hongbin,WANG Haiyang,SHI Yongsheng,et al. Multi-body dynamic modelling and simulation of the torsional vibration system of converters based on rigid-flexible coupling[J]. Proceedings of the Institution of Mechanical Engineers: Part K Journal of Multi-Body Dynamics,2016,230(3): 281-290. doi: 10.1177/1464419316643620
|
| [17] |
CAO Daijia,ZHU Caichao,GUO Peilin,et al. Dynamic transmission accuracy analysis of an RV reducer rigid-flexible coupled effect: DETC2017-67063 [R]. Cleveland,US: ASME,2017.
|
| [18] |
HAO Chiyu,FENG Guangbin,SUN Huagang,et al. Rigid-flexible coupling dynamics simulation of planetary gear transmission based on MFBD[J]. Journal of Vibroengineering,2017,19(8): 5668-5678. doi: 10.21595/jve.2017.18208
|
| [19] |
LAI Qinghui,YU Qingxu,DONG Jiayu. Dynamic analysis of rotary tiller gearbox based on EDEM,ADAMS and ANSYS[J]. Journal of Intelligent & Fuzzy Systems,2019,36(2): 1153-1160.
|
| [20] |
ZHANG Kongliang,LI Hongkun,CAO Shunxin,et al. Investigation on planetary gearbox fault mechanism under variable speed conditions based on rigid-flexible coupling dynamics model[J]. Engineering Failure Analysis,2022,133: 105994. doi: 10.1016/j.engfailanal.2021.105994
|
| [21] |
刘进进. 机动飞行尾传动系统与机身振动的仿真分析[D]. 南京: 南京航空航天大学,2013. LIU Jinjin. Simulation analysis of tail drive system and fuselage vibration of maneuvering flight[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2013. (in Chinese
LIU Jinjin. Simulation analysis of tail drive system and fuselage vibration of maneuvering flight[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2013. (in Chinese)
|
| [22] |
CHENG Qiyou,ZHU Yan,FENG Zhizhuang,et al. A coupled helicopter rotor/fuselage dynamics model using finite element multi-body[C]//Proceedings of MATEC Web of Conferences. Chongqing: EDP (Edition Diffusion Press) Sciences,2016: 01016.
|
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