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Yaw Systems for wind turbines - Overview of concepts, current challenges and design methods

机译:风力涡轮机的偏航系统 - 概念概述,当前挑战和设计方法

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Looking at the upscaling of the rotor diameter not only the loss in power production but the aerodynamic loads arising from yaw misalignment will have an increasing impact on the yaw system design in future wind turbines. This paper presents an overview of yaw systems used in current wind turbines and a review of patents with regards to the yaw system. The current state of the art of yaw systems has been analyzed through a systematic literature review. Further a patent analysis has been done through the European Patent Office. Todays design and strength requirements as per IEC and GL standards will be reviewed and alternative design calculations will be discussed. Over 100 patents have been identified as relevant to the yaw system and have been analyzed. It has been found that most patents are dealing with load reduction possibilities on the yaw system, where fatigue loads seem more of a problem than ultimate loads. Most of these patents concern especially the yaw actuator, which consists of multiple electrical motors, reduction gears and shaft pinions. This is due to the nature of the gearing in the actuator and the gearing between the shaft pinion and the ring gear. This coincides with the patents for yaw brakes, which mostly aim to reduce the fatigue loads during yaw maneuverer and during nacelle standstill. Patents for the yaw bearing are incorporating the reduction of loads through the usage of friction bearings or different bearing arrangement approaches. The paper shows that the conventional yaw system designs are still trying to meet the high requirements regarding the lifetime of a wind turbine and turbulent wind loads. New designs for yaw systems in general are hard to find. Many patents concentrate on control algorithms that depend on additional instruments and incorporate electromechanical systems.
机译:看着转子直径的上升不仅是电力生产的损失,而且偏航未对准产生的空气动力载荷将对未来风力涡轮机的偏航系统设计产生越来越大的影响。本文介绍了当前风力涡轮机中使用的偏航系统以及关于偏航系统的专利综述。通过系统的文献综述分析了偏航系统领域的现状。此外,通过欧洲专利局完成了专利分析。根据IEC和GL标准将进行今天的设计和强度要求,并将讨论替代设计计算。已识别100多项专利与偏航系统相关,并已被分析。已经发现,大多数专利正在处理偏航系统上的负载减少可能性,其中疲劳负载似乎更多的是最终负载的问题。这些专利中的大部分尤其是偏航致动器,其包括多个电动机,减速齿轮和轴小齿轮。这是由于致动器中的齿轮和轴小齿轮和齿圈之间的齿轮的性质。这与偏航制动器的专利一致,主要是旨在减少偏航运动员和机舱静止期间的疲劳负荷。偏航轴承的专利通过使用摩擦轴承或不同的轴承布置方法来结合负载的减少。本文表明,传统的偏航系统设计仍在试图满足有关风力涡轮机和湍流风力载荷的寿命的高要求。偏航系统的新设计通常很难找到。许多专利集中在控制算法上,依赖于附加仪器并包含机电系统。

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