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直升机传动系统主减速器健康监测技术研究进展

刘文正 朱如鹏 朱欣华 李苗苗 周文广 佘亦曦

刘文正, 朱如鹏, 朱欣华, 等. 直升机传动系统主减速器健康监测技术研究进展[J]. 航空动力学报, 2026, 41(10):20250064 doi: 10.13224/j.cnki.jasp.20250064
引用本文: 刘文正, 朱如鹏, 朱欣华, 等. 直升机传动系统主减速器健康监测技术研究进展[J]. 航空动力学报, 2026, 41(10):20250064 doi: 10.13224/j.cnki.jasp.20250064
Liu Wenzheng, Zhu Rupeng, Zhu Xinhua, et al. Research progress on health monitoring technology for helicopter main gearbox in transmission systems[J]. Journal of Aerospace Power, 2026, 41(10):20250064 doi: 10.13224/j.cnki.jasp.20250064
Citation: Liu Wenzheng, Zhu Rupeng, Zhu Xinhua, et al. Research progress on health monitoring technology for helicopter main gearbox in transmission systems[J]. Journal of Aerospace Power, 2026, 41(10):20250064 doi: 10.13224/j.cnki.jasp.20250064

直升机传动系统主减速器健康监测技术研究进展

doi: 10.13224/j.cnki.jasp.20250064
基金项目: 某传动预研专项(KY-1044-2023-0493)
详细信息
    作者简介:

    刘文正(1997-),男,工程师,博士,从事直升机传动系统动力学及健康监测研究。E-mail:wz_liu@nuaa.edu.cn

    通讯作者:

    朱如鹏(1959-),男,教授,博士,从事航空动力传动技术、先进机械结构和系统设计理论研究。E-mail:rpzhu_nuaa@163.com

  • 中图分类号: V275.1;TP306.3

Research progress on health monitoring technology for helicopter main gearbox in transmission systems

  • 摘要:

    随着低空经济的快速发展和直升机应用场景的不断拓展,直升机的安全性、维护性和可靠性要求持续升级。主减速器作为直升机传动系统的核心部件,其健康状态直接影响整机服役寿命与飞行安全。然而,主减复杂的结构与苛刻的工况使得健康监测面临信号成分复杂、特征提取困难、传感器布置受限等挑战。近三十年来,围绕直升机主减速器健康监测技术开展了大量研究,主要涵盖振动信号处理、状态监测指标、传感器技术、机器学习与数字孪生等方向。通过对比分析各类技术的优势边界与适用局限,总结未来研究应聚焦于构建系统化全域研究体系、发展多源传感信息融合技术、增强状态指标物理可解释性,深化数字孪生及迁移学习的工程化应用。研究成果可为主减速器健康监测系统的优化提供技术支撑,提升直升机安全性、可靠性及维护效率。

     

  • 图 1  某型直升机主减速器结构[8]

    Figure 1.  Structure of the main gearbox of a certain type of helicopter[8]

    图 2  通过振动分析进行状态维护[11]

    Figure 2.  Condition-based maintenance through vibration analysis[11]

    图 3  TSA处理流程[14]

    Figure 3.  Flowchart of TSA Processing[14]

    图 4  UH-60A变速箱底板裂纹引起的TSA能量变化[16]

    Figure 4.  TSA energy variation caused by cracks in the bottom plate of the UH-60A gearbox[16]

    图 5  CS-29试验台及其小波分解信号对比[25]

    Figure 5.  Comparison of CS-29 test bench and its wavelet decomposition signal[25]

    图 6  行星轮系振动信号分离过程[29]

    Figure 6.  Planetary gear train vibration signal separation process[29]

    图 7  OH-58直升机试验台及传感器布置[29]

    Figure 7.  OH-58 500HP helicopter transmission test bench and sensor layout[29]

    图 8  轴承故障信号分离结果[31]

    Figure 8.  Bearing fault signal separation results[31]

    图 9  Bell 412 直升机HUMS传感器位置及故障样本[33]

    Figure 9.  Bell 412 helicopter HUMS sensor locations and fault sample conditions[33]

    图 10  FM4计算流程[38]

    Figure 10.  FM4 calculation process[38]

    图 11  弧齿锥齿轮故障试验台及指标对比[41]

    Figure 11.  Spiral bevel gear fault test bench and index comparison[41]

    图 12  光纤传感器及加速度传感器布置及结果对比[48]

    Figure 12.  Arrangement of fiber optic sensors and acceleration sensors and comparison of results[48]

    图 13  直升机传动试验台滑油磨粒监测结果[52]

    Figure 13.  500HP helicopter transmission test bench lubricating ODM results[52]

    图 14  声发射无线传输方案[62]

    Figure 14.  AE Wireless Transmission Solution[62]

    图 15  用于传递HUMS数据的机器学习算法流程[64]

    Figure 15.  ML algorithm flow for delivering HUMS data[64]

    图 16  基于传感器融合的自适应加权卷积神经网络[69]

    Figure 16.  Adaptive channel weighted convolutional neural network based on sensor fusion[69]

    图 17  基于数字孪生的传动系统故障诊断[75]

    Figure 17.  Transmission system fault diagnosis based on digital twin[75]

  • [1] 孙灿飞, 王友仁. 直升机行星传动轮系故障诊断研究进展[J]. 航空学报, 2017, 38(7): 020892. Sun Canfei, Wang Youren. Advance in study of fault diagnosis of helicopter planetary gears[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(7): 020892. (in Chinese doi: 10.7527/S1000-6893.2017.020892

    Sun Canfei, Wang Youren. Advance in study of fault diagnosis of helicopter planetary gears[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(7): 020892. (in Chinese) doi: 10.7527/S1000-6893.2017.020892
    [2] LaGrone S. UPDATED: Navy, Marine V-22 Ospreys Under ’operational pause’ after AFSOC incident[EB/OL]. (2024-12-09)[2025-02-10]. https://news.usni.org/2024/12/09/navy-marine-v-22-ospreys-under-operational-pause-after-afsoc-incident.
    [3] Johnson O. Norway H225 crash report recommends changes to super puma type design[EB/OL]. (2018-07-05)[2025-02-10]. https://verticalmag.com/news/norway-h225-crash-report-recommends-changes-to-super-puma-type-design/.
    [4] 左丽华. 国外直升机HUMS系统的应用[J]. 直升机技术, 2000(3): 48-53. Zuo Lihua. Application of HUMS system in foreign helicopters[J]. Helicopter Technique, 2000(3): 48-53. (in Chinese

    Zuo Lihua. Application of HUMS system in foreign helicopters[J]. Helicopter Technique, 2000(3): 48-53. (in Chinese)
    [5] 王卫刚. 直升机传动系统设计方法研究[D]. 南京: 南京航空航天大学, 2011. Wang Weigang. Research on design method of helicopter transmission system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011. (in Chinese

    Wang Weigang. Research on design method of helicopter transmission system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011. (in Chinese)
    [6] 车明. 直九武装直升机主减速器改进设计研究[D]. 哈尔滨: 哈尔滨工程大学, 2006. Che Ming. Designing research of the improvement design for the-Z9 military helicopter main gearbox[D]. Harbin: Harbin Engineering University, 2006. (in Chinese

    Che Ming. Designing research of the improvement design for the-Z9 military helicopter main gearbox[D]. Harbin: Harbin Engineering University, 2006. (in Chinese)
    [7] Jacobson F M. Acoustic and dynamic models of a NASA helicopter gearbox housing[D]. Columbus: The Ohio State University, 1994.
    [8] Build A Helicopter. Helicopter Transmissions And Gearboxes[EB/OL]. [2025-02-10]. https://www.buildahelicopter.com/homebuilt-helicopter-transmissions.php.
    [9] 王锐, 徐忠岩, 徐云山, 等. 直升机传动系统健康管理需求分析及应用研究[C]//第六届中国航空科学技术大会论文集. 北京: 中国航空学会, 2023: 7. Wang Rui, Xu Zhongyan, Xu Yunshan, et al. Demand Analysis and Application Research on Health Management of Helicopter Transmission System[C]//Proceedings of the 6th China Aeronautical Science and Technology Conference. Beijing: Chinese Society of Aeronautics, 2023: 7. (in Chinese

    Wang Rui, Xu Zhongyan, Xu Yunshan, et al. Demand Analysis and Application Research on Health Management of Helicopter Transmission System[C]//Proceedings of the 6th China Aeronautical Science and Technology Conference. Beijing: Chinese Society of Aeronautics, 2023: 7. (in Chinese)
    [10] Zhou Linghao. Helicopter main gearbox planetary bearing fault diagnosis using vibration signal processing techniques[D]. London: London South Bank University, 2020.
    [11] Matania O, Bachar L, Bechhoefer E, et al. Signal processing for the condition-based maintenance of rotating machines via vibration analysis: a tutorial[J]. Sensors, 2024, 24(2): 454. doi: 10.3390/s24020454
    [12] Braun S. Discover Signal Processing: An Interactive Guide for Engineers[M]. Chichester: John Wiley & Sons, Inc. 2008.
    [13] Huff E M, Mosher M, Barszcz E, et al. An exploration of discontinuous time synchronous averaging for helicopter HUMS using cruise and terminal area vibration data: ASH-2003[R]. Fairfax: American Helicopter Society, 2003.
    [14] Elasha F, Mba D. Improving condition indicators for helicopter health and usage monitoring systems[J]. International Journal of Structural Integrity, 2016, 7(4): 584-595. doi: 10.1108/IJSI-09-2015-0032
    [15] Hood A A. Fault Detection on a Full-Scale OH-58 a/C Helicopter Transmission[M]. College Park: University of Maryland, College Park, 2010.
    [16] Sparis P, Vachtsevanos G. A helicopter planetary gear plate crack analysis and feature extraction based on ground and aircraft data[C]//Proceedings of the 2005 IEEE International Symposium on, Mediterrean Conference on Control and Automation Intelligent Control. New York: Mediterranean Control Association, 2005.
    [17] Mironov A, Mironovs D. Condition monitoring of helicopter main gearbox planetary stage[C]//Reliability and Statistics in Transportation and Communication. Cham: Springer International Publishing, 2019: 421-430.
    [18] Paula J, Islam A, Feldman J. Investigation of Gearbox Vibration Transmission Paths on Gear Condition Indicator Performance[R]. Washington, D. C: NASA, 2013.
    [19] Dempsey P J, Keller J A, Wade D R, et al. Signal detection theory applied to helicopter transmission diagnostic thresholds: NASA/TM-2008-215262[R]. Washington DC: NASA, 2008.
    [20] Liu Wenzheng, Zhu Rupeng, Yu Hu, et al. Differential extraction and experimental validation of essential characteristics in gear faults[J]. IEEE Sensors Journal, 2024, 24(10): 16419-16428. doi: 10.1109/JSEN.2024.3382809
    [21] 刘立生, 杨宇航. 基于小波神经网络的直升机主减速器故障诊断系统[J]. 航空动力学报, 2012, 27(6): 1255-1260. Liu Lisheng, Yang Yuhang. Fault diagnostics system for helicopter main gearbox using wavelet neural network[J]. Journal of Aerospace Power, 2012, 27(6): 1255-1260. (in Chinese

    Liu Lisheng, Yang Yuhang. Fault diagnostics system for helicopter main gearbox using wavelet neural network[J]. Journal of Aerospace Power, 2012, 27(6): 1255-1260. (in Chinese)
    [22] Gouda K M, Tarbutton J A, Hassan M A, et al. A wavelet-based index for fault detection and its application in condition monitoring of helicopter drive-train components[J]. International Journal of Manufacturing Research, 2015, 10(1): 87. doi: 10.1504/ijmr.2015.067619
    [23] Niu Penghui, Shen Qiuyuan, Zhang Lei, et al. Research on noise reduction for helicopter vibration signals based on wavelet analysis[C]//2020 International Conference on Artificial Intelligence and Electromechanical Automation. Piscataway, US: IEEE, 2020: 490-494.
    [24] Hassan M A, Habib M R, Abul Seoud R A, et al. Wavelet-based multiresolution bispectral analysis for detection and classification of helicopter drive-shaft problems[J]. Journal of Dynamic Systems, Measurement, and Control, 2018, 140(6): 061009. doi: 10.1115/1.4038243
    [25] Elasha F, Li Xiaochuan, Mba D, et al. A novel condition indicator for bearing fault detection within helicopter transmission[J]. Journal of Vibration Engineering & Technologies, 2021, 9(2): 215-224. doi: 10.1007/s42417-020-00220-7
    [26] Nacib L, Sakhara S, Bouchama Z. Wavelet neural network application in helicopter gearbox gear fault diagnosis[J]. South Florida Journal of Development, 2024, 5(12): e4780. doi: 10.46932/sfjdv5n12-029
    [27] Samuel P D, Pines D J. Vibration separation methodology for planetary gear health monitoring[R]. Bellingham, US: SPIE Proceedings, 2000, 3985: 250.
    [28] Blunt D M, Keller J A. Detection of a fatigue crack in a UH-60A planet gear carrier using vibration analysis[J]. Mechanical Systems and Signal Processing, 2006, 20(8): 2095-2111. doi: 10.1016/j.ymssp.2006.05.010
    [29] Hood A, LaBerge K, Lewicki D, et al. Vibration based Sun gear damage detection[R]. Portland, US: ASME 2013 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, 2014.
    [30] Elasha F, Greaves M, Mba D. Bearing signal separation of commercial helicopter main gearbox[J]. Procedia CIRP, 2017, 59: 111-115. doi: 10.1016/j.procir.2016.09.030
    [31] Elasha F, Mba D, Greaves M. Bearing signal separation enhancement with application to a helicopter transmission system[J]. Journal of Aerospace Engineering, 2017, 30(5): 04017059. doi: 10.1061/(ASCE)AS.1943-5525.0000744
    [32] Brary S. Vibration Health monitoring (VHM)[EB/OL]. (2021-04-06)[2025-02-10]. https://skybrary.aero/articles/vibration-health-monitoring-vhm.
    [33] Helicopter B, Tucker B, Center N G R, et al. Health monitoring survey of bell 412EP transmissions[C]//Proceedings of the Vertical Flight Society 72nd Annual Forum. West Palm Beach, US: The Vertical Flight Society, 2016: 1-12.
    [34] Stewart R M. Some useful analysis techniques for gearbox diagnostics: MHM/R/10/77[R]. Hampshire, UK: Machine Health Monitoring Group, Institute of Sound and Vibration Research, 1977.
    [35] Antolick L J, Branning J S, Wade D R, et al. Evaluation of gear condition indicator performance on rotorcraft fleet[C]//AHS 66th Annual Forum and Technology Display: Rising to New Heights in Vertical Lift Technology. Washington DC: NASA, 2010.
    [36] Zakrajsek J J, Townsend D P, Decker H J. An analysis of gear fault detection methods as applied to pitting fatigue failure data[R]. Washington DC: National Aeronautics and Space Administration. 1993.
    [37] Samuel P D, Pines D J. Constrained adaptive lifting and the CAL4 metric for helicopter transmission diagnostics[J]. Journal of Sound and Vibration, 2009, 319(1/2): 698-718. doi: 10.1016/j.jsv.2008.06.018
    [38] Dempsey P J, Lewicki D G, Le D D. Investigation of current methods to identify helicopter gear health[C]//2007 IEEE Aerospace Conference. Piscataway, US: IEEE, 2007: 1-13.
    [39] Hochmann D, Bechhoefer E. Gear tooth crack signals and their detection via the FM4 measure in application for a helicopter HUMS (health usage and management system) [C]//2003 IEEE Aerospace Conference Proceedings. Piscataway, US: IEEE, 2003: 3313-3326.
    [40] 金小强, 袁志文, 熊天旸, 等. 基于状态指标的直升机减速器行星轮故障诊断[J]. 科学技术与工程, 2022, 22(35): 15598-15603. Jin Xiaoqiang, Yuan Zhiwen, Xiong Tianyang, et al. Planetary gear fault diagnosis of helicopter main gearbox based on condition indicators[J]. Science Technology and Engineering, 2022, 22(35): 15598-15603. (in Chinese doi: 10.3969/j.issn.1671-1815.2022.35.020

    Jin Xiaoqiang, Yuan Zhiwen, Xiong Tianyang, et al. Planetary gear fault diagnosis of helicopter main gearbox based on condition indicators[J]. Science Technology and Engineering, 2022, 22(35): 15598-15603. (in Chinese) doi: 10.3969/j.issn.1671-1815.2022.35.020
    [41] Dempsey P J. Investigation of spiral bevel gear condition indicator validation via AC-29-2C combining test rig damage progression data with fielded rotorcraft data: GRC-E-DAA-TN20164[R]. Washington DC: NASA, 2015.
    [42] Yuan Zhilong, Jin Xiaoqiang. Rolling bearing fault diagnosis of helicopter reducer based on condition indicators[C]//2024 10th International Symposium on System Security, Safety, and Reliability. Piscataway, US: IEEE, 2024: 512-517.
    [43] Camerini V, Coppotelli G, Bendisch S. Fault detection in operating helicopter drivetrain components based on support vector data description[J]. Aerospace Science and Technology, 2018, 73: 48-60. doi: 10.1016/j.ast.2017.11.043
    [44] Bechhoefer E, Janke C. Hunting tooth gear condition indicator: for epicycle gear fault detection[C]//2024 International Conference on Control, Automation and Diagnosis. Piscataway, US: IEEE, 2024: 1-6.
    [45] Leoni J, Tanelli M, Palman A. A new comprehensive monitoring and diagnostic approach for early detection of mechanical degradation in helicopter transmission systems[J]. Expert Systems with Applications, 2022, 210: 118412. doi: 10.1016/j.eswa.2022.118412
    [46] Adams C. HUMS technology[EB/OL]. (2012-05-01)[2025-02-10]. https://www.aviationtoday.com/2012/05/01/hums-technology/.
    [47] 严治强. 光纤传感器技术在直升机试飞测试中的应用[J]. 中国科技信息, 2023(19): 72-74. Yan Zhiqiang. Application of optical fiber sensor technology in helicopter flight test[J]. China Science and Technology Information, 2023(19): 72-74. (in Chinese

    Yan Zhiqiang. Application of optical fiber sensor technology in helicopter flight test[J]. China Science and Technology Information, 2023(19): 72-74. (in Chinese)
    [48] Kiddy J S, Lewicki D G, LaBerge K E, et al. Fiber optic strain sensor for planetary gear diagnostics: AHS 2011-000154[R]. Virginia Beach: 67th Annual Forum and Technology Display, 2011.
    [49] Lvov N, Khabarov S, Todorov A, et al. Versions of fiber-optic sensors for monitoring the technical condition of aircraft structures[J]. Civil Engineering Journal, 2018, 4(12): 2895-2902. doi: 10.28991/cej-03091206
    [50] National Archives. Code of federal regulations[EB/OL]. [2025-02-10]. https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-29/subpart-F/subject-group-ECFR12da8eabf96ea03/section-29.1337.
    [51] Lewicki D G, Blanchette D M, Biron G. Evaluation of an oil-debris monitoring device for use in helicopter transmissions: 92-C-007[R]. Washington DC: NASA, 1992.
    [52] Dempsey P J. A comparison of vibration and oil debris gear damage detection methods applied to pitting damage: NASA/TM-2000-210371[R]. Washington DC: NASA, 2000.
    [53] Dempsey P J, Bolander N, Haynes C, et al. Investigation of bearing fatigue damage life prediction using oil debris monitoring: NASA/TM-2011-217117[R]. Washington DC: NASA, 2011.
    [54] 龙舟, 黄炎, 陈兴明, 等. 直升机滑油在线屑末监测器研发及应用[J]. 测控技术, 2025, 44(1): 57-62. Long Zhou, Huang Yan, Chen Xingming, et al. Development and application of lubricant oil on-line debris monitor for helicopter[J]. Measurement & Control Technology, 2025, 44(1): 57-62. (in Chinese doi: 10.19708/j.ckjs.2024.10.261

    Long Zhou, Huang Yan, Chen Xingming, et al. Development and application of lubricant oil on-line debris monitor for helicopter[J]. Measurement & Control Technology, 2025, 44(1): 57-62. (in Chinese) doi: 10.19708/j.ckjs.2024.10.261
    [55] Sun Jiayi, Wang Liming, Li Jianfeng, et al. Online oil debris monitoring of rotating machinery: a detailed review of more than three decades[J]. Mechanical Systems and Signal Processing, 2021, 149: 107341. doi: 10.1016/j.ymssp.2020.107341
    [56] Zieja M, Golda P, Zokowski M, et al. Vibroacoustic technique for the fault diagnosis in a gear transmission of a military helicopter[J]. Journal of Vibroengineering, 2017, 19(2): 1039-1049. doi: 10.21595/jve.2017.18401
    [57] Lu Kaibo, Gu J X, Fan Hongwei, et al. Acoustics based monitoring and diagnostics for the progressive deterioration of helical gearboxes[J]. Chinese Journal of Mechanical Engineering, 2021, 34: 82. doi: 10.1186/s10033-021-00603-1
    [58] Duan Fang, Elasha F, Greaves M, et al. Helicopter main gearbox bearing defect identification with acoustic emission techniques[C]//2016 IEEE International Conference on Prognostics and Health Management. Piscataway, US: IEEE, 2016: 1-4.
    [59] Ruiz-carcel C, Starr A, Francese A. Experimental assessment of a broadband vibration and acoustic emission sensor for rotorcraft transmission monitoring[J]. PHM Society European Conference, 2022, 7(1): 440-448. doi: 10.36001/phme.2022.v7i1.3368
    [60] Ruiz-Carcel C, Starr A. Accelerated gearbox degradation monitoring using a combination of vibration and acoustic emission features[C]//20th Australian International Aerospace Congress. Virginia Beach: Vertical Flight Society, 2023.
    [61] Elasha F, Greaves M, Mba D. Planetary bearing defect detection in a commercial helicopter main gearbox with vibration and acoustic emission[J]. Structural Health Monitoring, 2018, 17(5): 1192-1212. doi: 10.1177/1475921717738713
    [62] Leaman F. Phenomenological study of acoustic emissions generated by gear meshing in planetary gearboxes[J]. Measurement Science and Technology, 2025, 36(1): 015136. doi: 10.1088/1361-6501/ad98b3
    [63] Adryan F A, Sastra K W. Predictive maintenance for aircraft engine using machine learning: trends and challenges[J]. AVIA, 2021, 3(1): 1-14. doi: 10.47355/avia.v3i1.45
    [64] Wade D, Lugos R, Szelistowski M. Using machine learning algorithms to improve HUMS performance[C]//71st Annual Forum & Technology Display. Virginia Beach: Vertical Flight Society, 2015.
    [65] Cody T, Dempsey P J. Application of machine learning to rotorcraft health monitoring: E-19307[R]. Washington DC: NASA, 2017.
    [66] Wilson A, Wade D, Ling J, et al. Convolutional neural networks for frequency response predictions: SNL-NM [R]. Albuquerque, New Mexico: Sandia National Lab, 2017.
    [67] Gildish E, Grebshtein M, Aperstein Y, et al. Helicopter bolt loosening monitoring using vibrations and machine learning[J]. PHM Society European Conference, 2022, 7(1): 146-155. doi: 10.36001/phme.2022.v7i1.3322
    [68] Li Tianfu, Zhao Zhibin, Sun Chuang, et al. Adaptive channel weighted CNN with multisensor fusion for condition monitoring of helicopter transmission system[J]. IEEE Sensors Journal, 2020, 20(15): 8364-8373. doi: 10.1109/JSEN.2020.2980596
    [69] Liu Dongdong, Cui Lingli, Cheng Weidong. A review on deep learning in planetary gearbox health state recognition: methods, applications, and dataset publication[J]. Measurement Science and Technology, 2024, 35(1): 012002. doi: 10.1088/1361-6501/acf390
    [70] Tuegel E J, Ingraffea A R, Eason T G, et al. Reengineering aircraft structural life prediction using a digital twin[J]. International Journal of Aerospace Engineering, 2011, 2011: 154798. doi: 10.1155/2011/154798
    [71] Lai Xiaonan, Yang Liangliang, He Xiwang, et al. Digital twin-based structural health monitoring by combining measurement and computational data: an aircraft wing example[J]. Journal of Manufacturing Systems, 2023, 69: 76-90. doi: 10.1016/j.jmsy.2023.06.006
    [72] Matania O, Bechhoefer E, Bortman J. Digital twin of a gear root crack prognosis[J]. Sensors, 2023, 23(24): 9883.
    [73] Zhu Daoyong, Li Zhinong, Hu Niaoqing. Multi-body dynamics modeling and analysis of planetary gearbox combination failure based on digital twin[J]. Applied Sciences, 2022, 12(23): 12290.
    [74] 李恒, 唐倩, 陈国旺, 等. 数字孪生辅助的直升机尾传动系统轴承与传动轴故障诊断[J]. 航空动力学报, 2025, 40(6): 20230818. Li Heng, Tang Qian, Chen Guowang, et al. Diagnosis of bearing and drive shaft faults in helicopter tail drive systems assisted by digital twin[J]. Journal of Aerospace Power, 2025, 40(6): 20230818. (in Chinese

    Li Heng, Tang Qian, Chen Guowang, et al. Diagnosis of bearing and drive shaft faults in helicopter tail drive systems assisted by digital twin[J]. Journal of Aerospace Power, 2025, 40(6): 20230818. (in Chinese)
    [75] Xia Jingyan, Huang Ruyi, Chen Zhuyun, et al. A novel digital twin-driven approach based on physical-virtual data fusion for gearbox fault diagnosis[J]. Reliability Engineering & System Safety, 2023, 240: 109542.
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出版历程
  • 收稿日期:  2025-02-10
  • 网络出版日期:  2026-07-30

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