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Design of the centrifugal fan of a belt-driven starter generator with reduced flow noise

机译:皮带驱动起动发电机离心风机的设计

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Large eddy simulations based on the explicit algebraic subgrid-scale stress model were carried out to predict the flow-induced noise generated on the centrifugal fan of a belt-driven starter generator using Lighthill's analogy and the method of Ffowcs Williams and Hawkings. The surrounding air was approximated by an ideal gas at fixed room temperature (T-in = 300 K), and the rotating velocity of the fan was considered to be 6000 rpm. The blade array angles were designed using the modulation method, and a large blade curvature was adopted. We identified several centrifugal fan design parameters that could minimize the flow-induced noise while also minimizing fan efficiency losses. Three design parameters: the top serrated edge (theta(t)), the step leading edge (0.52 H-b) and the tail edge (d(b) and r(b)), played a critical role in preventing vortex generation and collision, significantly weakening the surface pressure fluctuations on the blade. The maximum sound pressure level at 800 Hz at a specific location was reduced by 5.5 dB (at the top serrated edge) and 6.8 dB (at the step leading edge) relative to the baseline case. The sound power, calculated over a hemisphere surface of 950 mm, was reduced by 77.3% (at the top serrated edge) and 61.0% (at the step leading edge) relative to the baseline whereas the mass flow rates were reduced by 5.2% and 10.6%, respectively. Experiments were performed using the optimally designed fan in a semi-anechoic chamber. The predicted sound pressure level and frequency were in good agreement with the experimentally measured values.
机译:基于Lighthill的类比和Ffowcs Williams和Hawkings的方法,基于显式代数子网格规模应力模型进行了大涡模拟,以预测皮带驱动起动发电机的离心风扇上产生的流致噪声。在固定的室温(T-in = 300 K)下,周围的空气被理想气体近似,风扇的转速被认为是6000 rpm。使用调制方法设计叶片阵列角度,并采用较大的叶片曲率。我们确定了几个离心风机设计参数,这些参数可以最大程度地减少流动引起的噪声,同时也可以将风机效率损失降至最低。三个设计参数:锯齿状的上边缘(theta(t)),阶跃前缘(0.52 Hb)和尾部边缘(d(b)和r(b))在防止涡旋产生和碰撞中起着至关重要的作用,大大减弱了叶片上的表面压力波动。相对于基线情况,特定位置在800 Hz处的最大声压级降低了5.5 dB(在锯齿状顶部)和6.8 dB(在阶跃前沿)。在950 mm的半球表面上计算出的声功率相对于基线降低了77.3%(在锯齿状顶部)和61.0%(在台阶前缘),而质量流率降低了5.2%和分别为10.6%。实验是在半消声室中使用优化设计的风扇进行的。预测的声压级和频率与实验测量值非常吻合。

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