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Influence of incident angle of hydrogen in the ventilation ducts on multi-physical fields of 1100 MW turbine-generator rotor

机译:通风管道中氢气的入射角对1100 MW汽轮发电机转子多物理场的影响

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During the operation of a large-scale turbine-generator, hydrogen enters the ventilation ducts of the rotor with turbulent state, so that the inlet direction of hydrogen is difficult to solve under the influence of rotor rotation. The cooling effect of the rotor coil can be effected by the mainstream of hydrogen entering the ventilation ducts. With regard to this, it takes an 1100 MW turbine-generator with axial ventilation system, as a test generator, global fluid network equation is carried out to calculate the pressure field and velocity field of hydrogen in the rotor ventilation ducts. Based on the calculations, the fluid and heat transfer nonlinear equation for the rotor is established and calculated via finite volume method (FVM). First, the hydrogen flow law in the complex ventilation duct is investigated and the pressure losses of hydrogen in the corners from the rotor radial inlet area to the axial flow area and then into the radial outlet area are analyzed. Second, the rotor temperature fields are highlighted and investigated in the condition of incident angle alpha = 0 degrees, 15 degrees, 30 degrees, 45 degrees. The incident angle alpha = 0 degrees indicates vertical state between hydrogen flow direction and the rotor vent inlet. Simultaneously, the calculations of the average temperature in the rotor coils are compared with the experimental results to verify the accuracy of the calculation method. Additionally, the temperature distribution of rotor varying with the circumferential direction is investigated, which can provide theoretical basis for the larger scale turbine-generator. (C) 2019 Elsevier Ltd. All rights reserved.
机译:在大型涡轮发电机的运转过程中,氢以湍流状态进入转子的通风管道,因此在转子旋转的影响下氢的入口方向难以求解。转子线圈的冷却效果可能受到进入通风管道的氢气的主流的影响。对此,以一台带有轴向通风系统的1100 MW涡轮发电机作为试验发电机,通过整体流体网络方程式计算转子通风管道中氢气的压力场和速度场。基于这些计算,建立了转子的流体和热传递非线性方程,并通过有限体积法(FVM)进行了计算。首先,研究了复杂通风管道中的氢气流动规律,分析了从转角径向入口区域到轴向流动区域再到径向出口区域的角落中的氢气压力损失。其次,在入射角α= 0度,15度,30度,45度的条件下,突出并研究了转子温度场。入射角α= 0度表示氢气流动方向与转子排气口之间的垂直状态。同时,将转子线圈中平均温度的计算结果与实验结果进行了比较,验证了计算方法的准确性。另外,研究了随周向变化的转子温度分布,可为大型汽轮发电机提供理论依据。 (C)2019 Elsevier Ltd.保留所有权利。

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