Influence of planet pin position errors on the fatigue reliability of planetary mechanisms for large wind turbines

IF 1.9 3区 工程技术 Q3 MECHANICS
Ming Li, Zhixuan Yang, Bo Fan, Wanyu Jiang, Liyang Xie
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引用次数: 0

Abstract

Planet pin position error is a critical geometric quality characteristic that significantly influences key attributes of planetary systems, including power density, load sharing, and operational reliability. Its tolerance parameters are among the key design factors determining the fatigue reliability of planetary systems in large wind turbines. In order to analyze the mechanism of these errors on the fatigue reliability of wind turbine planetary systems, a fatigue reliability evaluation model is established based on an extension of the computational logic of the full probability formula. It considers the failure correlation among the gear teeth and the temporal sequencing of the gear teeth meshing. Starting from balancing the contradiction between evaluation accuracy and evaluation costs, a hybrid finite element simulation including planet pin position errors and planet carrier flexibility, and an accelerated lifetime test for tooth probabilistic lifetime transformation are employed to respectively provide load and strength input variables for the reliability model. In particular, the Monte Carlo method is incorporated in the simulation and analysis process to take into account the randomness of planet pin position errors and the coupling influence mechanism between the error individuals. Finally, a mapping relationship from the planet pin position tolerance to the fatigue reliability of the planetary system is established. Depending on the specific reliability requirements, the upper limit of the planet pin positional tolerance zone can be determined at an early stage of the design in order to achieve as much as possible a balance between the service reliability of the planetary system and the manufacturing economy.

行星销位置误差对大型风力发电机行星机构疲劳可靠性的影响
行星销位误差是一个关键的几何质量特性,它显著影响行星系统的关键属性,包括功率密度、负载分担和运行可靠性。其公差参数是决定大型风力发电机行星系统疲劳可靠性的关键设计因素之一。为了分析这些误差对风力机行星系统疲劳可靠性的影响机理,在扩展全概率公式计算逻辑的基础上建立了疲劳可靠性评估模型。它考虑了齿间的失效关系和齿间啮合的时间顺序。从平衡评估精度和评估成本之间的矛盾出发,采用包含行星销位误差和行星载体柔性的混合有限元仿真,采用齿概率寿命变换的加速寿命试验,分别为可靠性模型提供载荷和强度输入变量。特别是在仿真分析过程中引入蒙特卡罗方法,考虑了行星销位误差的随机性和误差个体之间的耦合影响机制。最后,建立了行星销位公差与行星系统疲劳可靠性的映射关系。根据具体的可靠性要求,可以在设计初期就确定行星销位置公差带的上限,以尽可能在行星系统的使用可靠性和制造经济性之间取得平衡。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Meccanica
Meccanica 物理-力学
CiteScore
4.70
自引率
3.70%
发文量
151
审稿时长
7 months
期刊介绍: Meccanica focuses on the methodological framework shared by mechanical scientists when addressing theoretical or applied problems. Original papers address various aspects of mechanical and mathematical modeling, of solution, as well as of analysis of system behavior. The journal explores fundamental and applications issues in established areas of mechanics research as well as in emerging fields; contemporary research on general mechanics, solid and structural mechanics, fluid mechanics, and mechanics of machines; interdisciplinary fields between mechanics and other mathematical and engineering sciences; interaction of mechanics with dynamical systems, advanced materials, control and computation; electromechanics; biomechanics. Articles include full length papers; topical overviews; brief notes; discussions and comments on published papers; book reviews; and an international calendar of conferences. Meccanica, the official journal of the Italian Association of Theoretical and Applied Mechanics, was established in 1966.
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