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The Unsteady Flow and Forced Response for a Variable Nozzle Turbine

机译:变量喷嘴涡轮机的不稳定流和强制响应

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摘要

Variable nozzle turbine (VNT) has become a popular technology for diesel application. While one of the major challenges for VNT is resonant vibration due to the fluctuating pressure in unsteady flow. Both the leakage flow forms inside the nozzle clearances and the shock produces under small nozzle openings increase the flow unsteadiness inside downstream rotor tunnel. In this paper, the unsteady simulation of the turbine was conducted to investigate the effects of nozzle clearances and openings on the transient load fluctuation of the blades. Then a finite element model of turbine wheel was built and blade forced response was simulated with harmonic analysis. The results showed that the decrease of nozzle opening would intensify rotor vibration and increase the blade dynamic stress. The simulation of blade resonance showed that the 1st order resonance located at the blade trailing edge while the 2nd order resonance happened at the leading edge, which was consistent with the blade actual crack.
机译:可变喷嘴涡轮(VNT)已成为柴油应用的流行技术。虽然VNT的主要挑战之一由于不稳定流动的压力波动而具有共振振动。在喷嘴间隙内部的泄漏流体均在小喷嘴开口下产生冲击,增加了下游转子隧道内的流量不稳定。在本文中,进行了涡轮机的不稳定模拟,以研究喷嘴间隙和开口对叶片瞬态负荷波动的影响。然后建造了涡轮机叶轮的有限元模型,并用谐波分析模拟了叶片强制响应。结果表明,喷嘴开口的减少会加剧转子振动并增加叶片动态应力。叶片谐振的模拟表明,位于叶片后缘的第一阶谐振,而第二阶谐振发生在前缘,这与叶片实际裂缝一致。

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