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Nacelle slippage of a multi MW wind turbine: Influence of different braking models for the yaw system

机译:多MW风力涡轮机的机舱滑动:偏航系统不同制动模型的影响

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The yaw system's braking torque is generally designed to withstand aerodynamic yaw loads and to hold the nacelle in a given position. Circumstances in which the yaw loads are higher than the yaw system's braking torque can occur a) because of reduced braking effectivity due to mechanical failures, brake wear or environmental influences [1; 2] and b) because of economic reasons the braking torque is designed not to withstand extreme aerodynamic loads as their appearance is considered rate and the consequences not serious [3]. In these cases, the nacelle will stip and turn around the tower axis. To analyze the loads and dynamics of the wind turbine during nacelle slippage a detailed yaw system model has been incorporated into a multibody system model based on a 3.3 MW wind turbine and load simulations have been conducted. The focus is to address uncertainties of the braking capabilities and compare different braking models during design load cases in which nacelle slippage can occur.
机译:偏航系统的制动扭矩通常设计成承受空气动力学偏航载荷并在给定位置保持机舱。偏航载荷高于偏航系统的制动扭矩的情况可以发生a)由于机械故障引起的制动效果降低,制动磨损或环境影响[1; 2]和B)由于经济原因,制动扭矩设计不承受极端的空气动力载荷,因为它们的外观被认为是速率,并且不严重的后果[3]。在这些情况下,机舱将终止塔架轴。为了分析机舱滑动期间风力涡轮机的负载和动力学,将详细的偏航系统模型结合到基于3.3 MW风力涡轮机的多体系系统模型中,并进行了负载模拟。重点是解决制动能力的不确定性,并比较在设计负载箱中的不同制动模型,其中可以发生机舱滑动。

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