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2D Simulation of the Aerodynamic Micro Air Journal Bearing for Micro Gas Turbine Engine

机译:微型燃气轮机气动微型空气轴颈轴承的二维模拟

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摘要

A micro air journal bearing for micro gas turbine engine is designed in this paper.2D simulation of the aerodynamic micro air bearing is conducted to investigate the effect of the main parameters of the air bearing on the load capacity,including the clearance between the air bearing and shaft,the gear number and height of the air journal bearing,the rotational speed of rotor.The optimum value of the important parameters are explored and presented.The time correlation method is used to solve the RANS (Reynolds Averaged Navier-Stokes) equations.Requirements both from load capacity and motion stability is considered and compromised for a better and stable performance of the air journal bearing.The shaft is stably rotated in a relatively low speed of 1.18× 105rpm,which is much lower than other researches and can be achieved easily.
机译:本文设计了一种用于微型燃气轮机发动机的微型空气轴颈轴承。对空气动力学微型空气轴承进行了二维模拟,以研究空气轴承的主要参数对负载能力(包括空气轴承之间的间隙)的影响。探讨并给出了重要参数的最佳值。采用时间相关法求解了雷诺兹平均纳维耶-斯托克斯方程考虑并限制了对负载能力和运动稳定性的要求,以使空气轴颈轴承具有更好的稳定性。轴以1.18×105rpm的相对较低的速度稳定旋转,这比其他研究要低得多,并且可以轻松实现。

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