冀洋锋, 林麒, 彭苗娇, 柳汀, 吴惠松. 绳系并联支撑机构的绳迟滞效应及影响实验研究[J]. 工程力学, 2019, 36(11): 212-221. DOI: 10.6052/j.issn.1000-4750.2018.11.0612
引用本文: 冀洋锋, 林麒, 彭苗娇, 柳汀, 吴惠松. 绳系并联支撑机构的绳迟滞效应及影响实验研究[J]. 工程力学, 2019, 36(11): 212-221. DOI: 10.6052/j.issn.1000-4750.2018.11.0612
JI Yang-feng, LIN Qi, PENG Miao-jiao, LIU Ting, WU Hui-song. EXPERIMENTAL RESEARCH OF HYSTERESIS EFFECT OF WIRE AND ITS INFLUENCE ON WIRE-DRIVEN PARALLEL SUSPENSION MECHANISM[J]. Engineering Mechanics, 2019, 36(11): 212-221. DOI: 10.6052/j.issn.1000-4750.2018.11.0612
Citation: JI Yang-feng, LIN Qi, PENG Miao-jiao, LIU Ting, WU Hui-song. EXPERIMENTAL RESEARCH OF HYSTERESIS EFFECT OF WIRE AND ITS INFLUENCE ON WIRE-DRIVEN PARALLEL SUSPENSION MECHANISM[J]. Engineering Mechanics, 2019, 36(11): 212-221. DOI: 10.6052/j.issn.1000-4750.2018.11.0612

绳系并联支撑机构的绳迟滞效应及影响实验研究

EXPERIMENTAL RESEARCH OF HYSTERESIS EFFECT OF WIRE AND ITS INFLUENCE ON WIRE-DRIVEN PARALLEL SUSPENSION MECHANISM

  • 摘要: 绳系并联机构因具有结构简单、工作空间大、惯性小等优势,得到了广泛的应用。该文针对支撑绳索中普遍存在的迟滞效应进行了实验研究。首先,分析了某绳系并联机器人(Wire-driven Parallel Robot,WDPR)样机中的绳迟滞曲线的数学模型,并利用实验数据识别出了模型中的相关参数;其次,通过不同条件下的绳索伸-缩实验,探讨了绳拉力迟滞效应的影响因素;接着,分析了迟滞效应对飞行器模型位姿和气动载荷参数解算的影响情况。最后,以某风洞试验模型支撑绳系并联机器人样机中支撑飞机模型的牵引绳的迟滞现象为例,对绳迟滞效应的影响情况进行了分析。研究结果表明:绳迟滞效应对模型位姿和利用绳拉力解算风洞试验的模型气动载荷都有一定的影响;绳索的材质与迟滞现象关系密切;预紧力对迟滞效应的影响程度具有决定性的作用,当绳预紧力增大到一定程度时,迟滞效应的影响是可以忽略的。

     

    Abstract: Due to the advantages of structural simplicity, large workspace and low inertia, wire-driven parallel suspension mechanism is widely used. An experimental study is carried out on the hysteresis effect of a suspension wire. Firstly, the mathematical model of hysteresis curve in a Wire-driven Parallel Robot (WDPR) is analyzed and the corresponding parameters of the model are identified through experimental data. Secondly, the influencing factors of hysteresis phenomenon are discussed through hysteresis experiments under different conditions. Then the influence of hysteresis effect on pose and aerodynamic parameter calculation of the model is analyzed. Finally, the magnitude of the influence is analyzed based on the parameters of a WDPR prototype. The results exhibit the influence of hysteresis effect on both the pose and aerodynamic parameter calculation through wire tensions, and the material of wire is also one of the factors that cannot be ignored in relation to the hysteresis. Furthermore, the influence of hysteresis effect, dominantly determined by the level of preload, can be ignored when the preload increases to a certain extent.

     

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