A Three-Dimensional Body Force Modeling of Fans in Windmilling Condition and Its Application

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Aerospace America Pub Date : 2023-08-18 DOI:10.3390/aerospace10080724
Q. Kong, W. Jia
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Abstract

To investigate the aerodynamic characteristics of the fan in windmilling conditions, a new body force model with the fan rotational speed prediction model was developed. The fan rotational speed prediction model was built based on the balance of fan output torque and resistance torque. The rotational speed of the fan spool can be iteratively solved simultaneously with solving the governing equations without requiring mass flow rate or other inputs. The comparison with the experimental results shows that using the body force model can accurately predict the rotational speed of the fan spool under different operating conditions. The radial distribution of flow parameters can be obtained. Moreover, numerical simulations of the fan under different circumferential total pressure distortion inflow conditions were conducted using the body force model. The results show that, unlike the design point and non-design point at which the fan operates normally, the high radius region of the fan is in the “turbine mode” while the low radius region is in the “compressor mode” under windmilling conditions. The different effects on the longitudinal vortex in the two regions deepen and alleviate the circumferential distortion, respectively. There are strong circumferential and radial pressure gradients at the junction of the distortion-affected zone and the non-distortion-affected zone, adding additional mixing losses.
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风机在风力工况下的三维体力建模及其应用
为研究风机在风力工况下的气动特性,建立了结合风机转速预测模型的机体力模型。基于风机输出转矩与阻力转矩的平衡,建立了风机转速预测模型。风机阀芯转速可与控制方程同时迭代求解,不需要质量流量或其他输入。与实验结果的对比表明,利用体力模型可以准确地预测风机阀芯在不同工况下的转速。可以得到流动参数的径向分布。此外,采用体力模型对风机在不同周向总压畸变入流条件下进行了数值模拟。结果表明:与风机正常运行的设计点和非设计点不同,风机高半径区域处于“涡轮模式”,而低半径区域处于“压缩机模式”。两个区域对纵向涡的不同影响分别加深和减轻了周向畸变。在畸变影响区和非畸变影响区交界处存在很强的周向和径向压力梯度,增加了额外的混合损失。
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
0.00%
发文量
9
审稿时长
4-8 weeks
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