航空高速薄辐板弧齿锥齿轮行波共振动力学响应特性与试验-CSCIED科技核心评价数据库-手机版

航空高速薄辐板弧齿锥齿轮行波共振动力学响应特性与试验

Experiment on travelling wave resonance dynamic response characteristics of aviation high speed thin-walled spiral bevel gear

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DOI	10.13224/j.cnki.jasp.20240452
刊名	航空动力学学报
年，卷(期)	2025, 40(04)
作者	栾孝驰1；王胜红1；柳贡民2；沙云东1；张茂强3,
作者单位	1.沈阳航空航天大学; 2.哈尔滨工程大学; 3.中国航发沈阳发动机研究所
摘要	针对航空高速薄辐板弧齿锥齿轮在工作中由于行波共振导致轮齿断裂故障频发，其行波共振动力学响应特性不清晰的问题，建立了一种基于显式算法的航空薄辐板弧齿锥齿轮瞬态接触动力学分析模型。考虑齿轮转速、扭矩以及时变啮合刚度的影响，计算齿轮动频值进而对行波共振点进行精准预测，研究了行波共振下齿轮轴向振动位移和动应力的动态响应特性以及振动位移场和应力场的分布规律。研究结果表明：在三节径前行波共振工况下，从动锥齿轮轴向振动位移场在周向呈现谷峰交替的三峰三谷扇形分布快速迁移的特征，行波迁移方向与齿轮转动方向相同、迁移速度远高于齿轮的旋转速度；振动应力场在周向表现为三峰的花瓣状分布形式，在齿根槽位置和齿面啮合位置存在应力集中现象；振动位移和应力响应均表现为高次谐波振动密集分布的特征。试验测量从动锥齿轮三节径前行波共振转速与仿真计算预测的行波共振转速的相对误差为1.1%，试验测量的应力值与仿真提取分析的应力值两者量级相当，验证了行波共振点预测的准确性及瞬态接触动力学分析模型的有效性。
Abstract	Aiming at the problem that the travelling wave resonance(TWR) of the aviation high speed thin-walled spiral bevel gear causes frequent tooth fracture faults during operation, and the dynamic response characteristics of the TWR are not clear, a transient contact dynamics analysis model of the aviation thin-walled spiral bevel gear based on the explicit algorithm is established. Considering the influence of gear speed, torque and time-varying meshing stiffness, the dynamic frequency value of the gear is calculated and the TWR point is accurately predicted. The dynamic response characteristics of the axial vibration displacement and dynamic stress of the gear under the TWR and the distribution law of the vibration displacement field and the stress field are studied. The results show that the axial vibration displacement field of the driven bevel gear presents a three-peak and three-valley distribution form with alternating valleys and peaks in the circumferential direction under the condition of forward traveling wave (FTW) resonance with the third nodal diameter (3rd ND). The traveling wave migration direction is the same as the rotation direction of the gear, and the migration speed is much higher than the rotation speed of the gear, which is characterized by the rapid migration of the sector distribution displacement field. The vibration stress field shows a petal-shaped distribution of three peaks in the circumferential direction, and there is a stress concentration phenomenon at the root groove position and the tooth surface meshing position. The vibration displacement and stress response are characterized by the dense distribution of high-order harmonic vibration. The relative error between the FTW resonant speed with the 3rd ND of the driven bevel gear measured by the test and predicted by the simulation calculation is 1.1%, and the stress value measured by the test is consistent with the stress value extracted by the simulation, which verifies the accuracy of the prediction of the TWR point and the validity of the transient contact dynamics analysis model.
关键词	弧齿锥齿轮;行波共振;瞬态动力学分析;振动响应;振动应力;
KeyWord	spiral bevel gears; travelling wave resonance; transient dynamic analysis; vibration response; vibration stress
基金项目
页码	44-54

参考文献
相关文献

[1] 杨昌祺, 蔚夺魁, 张茂强, 等. 航空发动机中央传动失效故障分析
[J]. 航空发动机, 2022, 48(2): 83-89.

YANG Changqi, YU Duokui, ZHANG Maoqiang, et al. Failure analysis of central transmission system for an aeroengine
[J]. Aeroengine, 2022, 48(2): 83-89. (in Chinese)

[2] 韩二中, 郭星辉, 颜世英, 等. 圆锥齿轮行波共振应力响应仿真计算
[J]. 航空动力学报, 1988, 3(3): 207-210, 280.

HAN Erzhong, GUO Xinhui, YAN Shiying, et al. Simulatinc calculations for stress responses of travelling wave resonance in bevel cear
[J]. Journal of Aerospace Power, 1988, 3(3): 207-210, 280. (in Chinese)

[3] TALBERT P B, JANKOWICH E M. Effect of tooth load distribution on bull gear vibration
[R]. ASME Paper DETC2005-84686, 2005.

[4] BOGACZ R, NOGA S. Passive control of vibration of thin-walled gears: Advanced modelling of ring dampers
[J]. Nonlinear Dynamics, 2013, 76(01): 263-280.

[5] 刘天文. 某型航空发动机中心锥齿轮动力学特性研究
[D]. 南京: 南京航空航天大学, 2015.

LIU Tianwen. Study on dynamic characteristics of central bevel gear of an aero-engine
[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015. (in Chinese).

[6] 欧阳旭靖, 郭梅, 王建军. 基于共振分析的发动机附件传动系统危险齿轮的确定
[J]. 航空发动机, 2016, 42(1): 25-31.

OUYANG Xujing, GUO Mei, WANG Jianjun. Determine the dangerous gear in accessory gear system of engine based on resonance analysis
[J]. Aeroengine, 2016, 42(1): 25-31. (in Chinese)

[7] 王大勇. 航空薄辐板齿轮固有特性及稳态响应分析
[J]. 机械传动, 2016, 40(5): 145-147.

WANG Dayong. Inherent characteristic and steady response analysis of aviation gear with thin-spoke
[J]. Journal of Mechanical Transmission, 2016, 40(5): 145-147. (in Chinese)

[8] 李躲. 高速重载弧齿锥齿轮振动分析与控制
[D]. 重庆: 重庆大学, 2018.

LI Duo. Vibration analysis and control of spiral bevel gear with high speed and heavy load
[D]. Chongqing: Chongqing University, 2018. (in Chinese)

[9] 栾孝驰, 沙云东, 郭小鹏, 等. 航空发动机高速锥齿轮瞬态动力学分析与试验研究
[J]. 推进技术, 2019, 40(12): 2806-2815.

LUAN Xiaochi, SHA Yundong, GUO Xiaopeng, et al. Transient dynamics analysis and experimental research of high-speed bevel gear in aero-engine
[J]. Journal of Propulsion Technology, 2019, 40(12): 2806-2815. (in Chinese)

[10] 陈向前. 航空高速薄辐板锥齿轮行波共振特性与试验研究
[D]. 重庆: 重庆大学, 2022.

CHEN Xiangqian. Traveling wave resonance characteristics and experimental study of high-speed thin spoke bevel gear in aviation
[D]. Chongqing: Chongqing University, 2022. (in Chinese)

[11] 魏静, 刘指柔, 魏海波, 等. 高速薄辐板齿轮传动节径型振动位移与动应变时空变换方法
[J]. 机械工程学报, 2024, 60(5): 70-80.

WEI Jing, LIU Zhirou, WEI Haibo, et al. Time-space transformation method of vibration displacement and dynamic strain in nodal-diameter vibration of high-speed thin-walled gear
[J]. Journal of Mechanical Engineering, 2024, 60(5): 70-80. (in Chinese)

[12] 徐子扬, 魏静, 魏海波, 等. 薄辐板齿轮柔性化动力学模型与行波共振表征
[J/OL]. 机械工程学报, 2024 (2024-03-13). https://kns.cnki.net/kcms/detail/11.2187.TH.20240312.1141.010.html.

XU Ziyang, WEI Jing, WEI Haibo, et al. Dynamics model of thin-walled gears considering elasticity and its traveling wave vibration characterization
[J/OL]. Journal of Mechanical Engineering.
[2024-06-20].https://kns.cnki.net/kcms/detail/11.2187.TH.20240312.1141.010.html. (in Chinese)

[13] LIU Zimeng, HUANGFU Yifan, MA Hui, et al. Traveling wave resonance analysis of flexible spur gear system with angular misalignment
[J]. International Journal of Mechanical Sciences, 2022, 232: 107617.

[14] FUNG Y C, SECHLER E E, KAPLAN A. On the vibration of thin cylindrical shells under internal pressure
[J]. Journal of the Aeronautical Sciences, 1957, 24(9): 650-660.

[15] 艾贻人, 鞠秀庭, 宇培孚, 等. 齿轮共振转速及动频测量
[J]. 航空动力学报, 1988, 3(3): 211-214, 281.

AI Yiren, JU Xiuting, YU Peifu, et al. Measurement of resonance speeds and dynamic frequencies of a bevel gear
[J]. Journal of Aerospace Power, 1988, 3(3): 211-214, 281. (in Chinese)

[16] KIM M E, LEE C W. Use of dFRFs for identification of travelling wave modes in rotating disks
[J]. Journal of Vibration and Acoustics, 1998, 120(3): 719-726.

[17] TIAN Jifang, HUTTON S G. Traveling-wave modal identification based on forced or self-excited resonance for rotating discs
[J]. Journal of Vibration and Control, 2001, 7(1): 3-18.

[18] 胡国安, 何刘海, 吴桂娇, 等. 航空高速锥齿轮行波共振的噪声与动应力测试研究
[J]. 推进技术, 2019, 40(1): 166-174.

HU Guoan, HE Liuhai, WU Guijiao, et al. Acoustic noise and dynamic stress experimental study on travelling wave vibration of high-speed bevel gear in aero-engine
[J]. Journal of Propulsion Technology, 2019, 40(1): 166-174. (in Chinese)

[19] LUAN Xiaochi, LIU Gongmin, SHA Yundong, et al. Experiment study on traveling wave resonance of fatigue fracture of high-speed bevel gear in aero-engne based on acoustic measurement method
[J]. Journal of Sound and Vibration, 2021, 511: 116345.

[20] 姜贵林, 张茂强, 王海旭, 等. 基于振动应力分析的齿轮结构优化方法研究
[J]. 机械传动, 2021, 45(12): 124-129, 149.

JIANG Guilin, ZHANG Maoqiang, WANG Haixu, et al. Research of gear structure optimization method based on vibration stress analysis
[J]. Journal of Mechanical Transmission, 2021, 45(12): 124-129, 149. (in Chinese)

[21] 郭小鹏, 吴法勇, 安中彦, 等. 基于声测法的齿轮行波共振测试方法
[J]. 航空发动机, 2023, 49(6): 115-120.

GUO Xiaopeng, WU Fayong, AN Zhongyan, et al. Gear travelling wave resonance testing method based on acoustic measurement method
[J]. Aeroengine, 2023, 49(6): 115-120. (in Chinese)

[22] 晏砺堂, 李其汉. 盘形锥齿轮的横向振动特性分析
[J]. 航空动力学报, 1988, 3(3): 199-202, 279.

YAN Litang, LI Qihan. Analysis of transverse vibration characteristics of disc bevel gears
[J]. Journal of Aerospace Power, 1988, 3(3): 199-202, 279. (in Chinese)

引用本文

栾孝驰；王胜红；柳贡民；沙云东；张茂强. 航空高速薄辐板弧齿锥齿轮行波共振动力学响应特性与试验 [J]. 航空动力学学报. 2025; 40; (04). 44 - 54.

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