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As the widely used connection in the low-pressure rotor of aeroengine, rigid spline joint will transfer multi-axial load such as axial force, bending moment, shearing force and torque at work. Therefore,multi-axial load will change contact states of centering surfaces, end faces and spline surfaces, which results in complex change law of the structure stiffness. To solve this problem, based on the contact finite element method, a nonlinear simulation model of spline joint with multiple contact surface is established under multiaxial load. Two quantitative evaluation parameters, the sensitivity of equivalent stiffness to the contact surface and the ratio of contact state of the contact surface are proposed. According to these two parameters, the nonlinear characteristics of the stiffness of the spline joint, and the change law of the contact state of the contact surface are revealed, with key influencing factors. The results show that the incensement of external load results to the loss of the equivalent stiffness of the spline joint. During this process, the contact state of each contact surface changes. Centering surface B is the greatest influence on spline joint. End face B and centering surface A are the main reason of the nonlinear change of the stiffness of the spline joint. The contact of meshing spline surface can improve the connection stiffness, without effect on the nonlinear characteristics.The stiffness of the spline joint increases with the increase of the dimension tolerance of centering surfaces,preload and torque of the nut.
[1]李英杰,赵广,吴学深,等.航空花键-转子系统自激振动研究综述[J].航空学报,2022,43(8):21-35.
[2]王永亮,赵广,孙绪聪,等.航空花键研究综述[J].航空制造技术,2017(3):91-100.
[3]李伦绪,陈果,杨默晗.航空发动机套齿连接结构刚度特性仿真分析及试验研究[J].中国机械工程,2022,33(18):2249-2257.
[4]康丽霞,曹义华,梅庆.直升机传动系统花键连接轴的动力失稳[J].北京航空航天大学学报,2010,36(6):645-649.
[5]高腾,荆建平,梅庆,等.花键连接转子系统稳定性研究[J].噪声与振动控制,2016,36(2):40-45.
[6] Zhang C,Cao P,Zhu R,et al. Dynamic modeling and analysis of the spline joint-flexible coupling-rotor system with misalignment[J]. Journal of Sound and Vibration,2023,554:117696.
[7] Huang W,Tian H,Ma H,et al. An improved method for calculating the lateral and angular stiffness of spline couplings considering parallel misalignment[J]. Mechanism and Machine Theory,2023,189:105436.
[8] Yu P,Wang C,Liu Y,et al. Analytical modeling of the lateral stiffness of a spline coupling considering teeth engagement and influence on rotor dynamics[J]. European Journal of Mechanics-A/Solids,2022,92:104468.
[9]廖仲坤,陈果,王海飞.套齿联轴器对航空发动机振动特性的影响[J].中国机械工程,2015,26(10):1312-1319.
[10]胡正根,朱如鹏,靳广虎,等.航空渐开线花键副微动摩擦接触参数分析[J].中南大学学报(自然科学版),2013,44(5):1822-1828.
[11]高腾.花键连接转子系统稳定性研究[D].上海:上海交通大学,2016.
[12]李英杰,赵广,袁运博,等.航空花键接触刚度仿真与试验[J].航空动力学报,2024,39(12):187-194.
[13]侯志强.航空花键连接结构刚度仿真、试验、识别及应用[D].大连:大连理工大学,2022.
[14] Liu S,Wang J,Hong J,et al. Dynamics design of the aero-engine rotor joint structures based on experimental and numerical study[C]. Turbo Expo:Power for Land,Sea,and Air,USA,2010,44014:49-60.
[15] Wu F Y,Liang Z C,Ma Y H,et al. Bending stiffness and dynamic characteristics of a rotor with spline joints[C]. Proceedings of the ASME 2013 International Mechanical Engineering Congress and Exposition,San Diego,2013:2-8.
[16] Zhang Q C,Li W X,Liang Z C,et al. Study on the stiffness loss and its affecting factors of the spline joint used in rotor systems[J]. Proceedings of the ASME Turbo Expo,2014:2-12.
[17]李俊慧,马艳红,洪杰.转子系统套齿结构动力学设计方法研究[J].航空发动机,2009,35(4):36-39.
[18]王亭月.花键连接结构接触刚度及其转子动力学特性[D].大连:大连理工大学,2021.
[19]赵广,刘占生,陈锋,等.花键联轴器对转子-轴承系统稳定性影响研究[J].振动工程学报,2009,22(3):280-286.
[20]陈曦,廖明夫,李全坤.带套齿联轴器的转子系统动力学特性研究[J].推进技术,2015,36(7):1069-1077.
[21]朱彬,杨诚,刘烨辉,等.套齿连接结构力学模型及其刚度影响因素[J].机械设计与制造,2019,(S1):86-90+94.
[22]成大先.机械设计手册:连接与紧固[M].第6版.北京:化学工业出版社,2017,60-85.
[23]王珊,王栋.导弹舱段间复杂连接件弯曲应力分析[J].战术导弹技术,2017,185(5):62-67.
[24]杨炳渊,宋伟力.导弹舱段连接分离面的试验建模和参数识别法[J].战术导弹技术,1989(2):20-27.
Basic Information:
DOI:10.16358/j.issn.1009-1300.20240135
China Classification Code:V231.96
Citation Information:
[1]Zheng Huaqiang,Jiang Ke,Yu Pingchao ,et al.Study on nonlinear stiffness of spline joint with the influence of multiple contact surfaces and multi-axial loads[J].Tactical Missile Technology,2025,No.229(01):83-93.DOI:10.16358/j.issn.1009-1300.20240135.
Fund Information:
国家自然科学基金(52372387,52005252); 民航飞机健康监测与智能维护重点实验室自主基金(NJ2024022); 博士后科学基金面上项目(2022M711615); 南京航空航天大学研究生科研与实践创新计划项目(xcxjh20240721); 航空科学基金(2020Z039052007)
2025-02-15
2025-02-15