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About the impact of wind turbine blade tip vortices on helicopter rotor trim and rotor blade motion

机译:关于风力涡轮机叶片尖端涡流对直升机旋翼饰板和旋翼叶片运动的影响

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Abstract With increasing numbers of large wind turbines on-shore and off-shore, interactions of their wake with helicopters become a subject worth investigating. In this paper, the wake is modeled as a tip vortex helix with a vortex strength estimated from the wind turbine thrust. Helicopter rotors of different size and hub layout are subjected to the wake and the collective and cyclic control inputs required to keep the trim are compared to the maximum available control range of the rotorcraft. In addition, the blade flapping response due to the vortex influence without pilot action is computed and compared to maximum allowed flapping angles. It is found that typical on-shore wind turbines could be a hazard for ultralight helicopters, but not for larger helicopters. Large off-shore wind turbines, however, could even be a danger for small helicopters that may be used for maintenance. In addition, the results are compared to fixed-wing wake vortex interaction with a helicopter as given in the literature.
机译:摘要随着陆上和海上大型风力涡轮机数量的增加,其尾流与直升机的相互作用成为值得研究的课题。在本文中,将尾流建模为具有由风力涡轮机推力估算出的涡旋强度的尖端涡旋螺旋。不同大小和轮毂布局的直升机旋翼受到尾流的影响,将保持纵倾所需的集体和循环控制输入与旋翼飞机的最大可用控制范围进行比较。另外,计算了在没有先导作用的情况下由于旋涡影响而产生的叶片拍打响应,并将其与最大允许拍打角进行了比较。发现典型的陆上风力涡轮机可能对超轻型直升机造成危害,但对大型直升机则没有危害。但是,大型海上风力涡轮机甚至可能对用于维护的小型直升机构成危险。此外,将结果与文献中给出的与直升机的固定翼尾流涡流相互作用进行了比较。

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