首页> 外文会议>ASME/JSME/KSME Joint Fluids Engineering Conference >DYNAMIC CHARACTERISTICS OF UNSHROUDED IMPELLERS EQUIPPED WITH BALANCE PISTON SYSTEMS FOR ROCKET TURBO PUMPS
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DYNAMIC CHARACTERISTICS OF UNSHROUDED IMPELLERS EQUIPPED WITH BALANCE PISTON SYSTEMS FOR ROCKET TURBO PUMPS

机译:火箭涡轮泵装有平衡活塞系统的无阻尼叶轮的动态特性。

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Turbo pumps for rocket engines often equipped balance piston (BP) systems at the back-shroud of the impellers for cancelling their axial thrust. The BP system is self-balancing and stable under quasi-static conditions, but it is known that the BP systems can be unstable under certain dynamic conditions. The performance characteristics of turbo pumps equipped with unshrouded impellers might be affected by the axial position of the rotor. Thus it is necessary to consider this effect when calculating the balance of axial thrust. Few experiments have determined the characteristics of unshrouded impellers equipped with BP systems yet. In this research, an experimental study of a model turbo pump for rocket engines was carried out. This pump had an unshrouded impeller, a BP system, a vaned diffuser, and a volute. Axial forced oscillations were applied on the rotor of the pump by an active magnetic bearing (AMB) test facility. This setup can oscillate with freely-selected amplitude and frequency applying thrust to the rotor. During the oscillations, the fluctuation of axial thrust under the operating conditions was monitored using strain gauges. The axial thrust compensation ability and the response of the BP system were evaluated by analyzing the magnitude, amplitude and phase delay of the axial position of the rotor. Moreover, 3D simulations and 1D simulations were carried out for the model pump. In the 3D simulations, computational fluid dynamics (CFD) was used to calculate the internal flow of the model pumps. The BP system was equipped with an impeller on which were applied forced oscillations. The impeller movement was modeled using a mesh morphing method. The 1D simulation predicted the axial thrust by calculating the mass flow balance using the geometry of the model pump. The phase lag between the axial position and the thrust was dominated by the pressure fluctuation at the BP chamber caused by the mass flow balance. The 3D simulations well predicted the fluctuation, but the characteristics of the BP system estimated by the 3D simulations were more stable than those determined by the experiments. On the other hand, the characteristics estimated by the 1D simulation was less stable than those by the experiments. However, these simulations grasped the tendency of the BP system to become unstable as the oscillation frequency increases, and are effective in predicting the characteristics.
机译:用于火箭发动机的涡轮泵通常在叶轮的后盖处装有平衡活塞(BP)系统,以抵消其轴向推力。 BP系统是自平衡的,并且在准静态条件下稳定,但是已知BP系统在某些动态条件下可能不稳定。配备无叶轮叶轮的涡轮泵的性能特征可能会受到转子轴向位置的影响。因此,在计算轴向推力平衡时,有必要考虑这种影响。很少有实验确定配备BP系统的无罩叶轮的特性。在这项研究中,对用于火箭发动机的模型涡轮泵进行了实验研究。该泵具有一个没有遮盖的叶轮,一个BP系统,一个带叶片的扩压器和一个蜗壳。轴向磁力振荡是通过主动磁轴承(AMB)测试设备施加到泵的转子上的。该设置可以自由选择的振幅和频率进行振荡,从而向转子施加推力。在振荡期间,使用应变仪监测工作条件下的轴向推力波动。通过分析转子轴向位置的大小,幅度和相位延迟,评估了轴向推力补偿能力和BP系统的响应。此外,对模型泵进行了3D模拟和1D模拟。在3D模拟中,使用计算流体动力学(CFD)来计算模型泵的内部流量。 BP系统配有叶轮,在其上施加了强制振荡。使用网格变形方法对叶轮运动进行建模。一维模拟通过使用模型泵的几何形状计算质量流量平衡来预测轴向推力。轴向位置和推力之间的相位差主要由质量流量平衡引起的BP腔压力波动引起。 3D模拟很好地预测了波动,但是3D模拟估计的BP系统的特性比实验确定的稳定。另一方面,通过一维模拟估算的特性比通过实验估算的特性不稳定。但是,这些模拟掌握了BP系统随着振荡频率的增加而变得不稳定的趋势,并有效地预测了特性。

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