Investigation of Oil Jet Impingement on a Rotating Gear Using Lattice Boltzman Method (LBM)

S. Ambrose, H. Morvan, K. Simmons
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引用次数: 7

Abstract

In the drive for greater increases in fuel efficiency and reductions in CO2 emissions from aero engines, an epicyclic reduction gearbox can be used to break the link between the turbine and fan, enabling the engine to run at a higher bypass ratio. However, even small power losses can generate significant amounts of heat, due to the high loads transmitted from the gearbox. A substantial amount of cooling is required to remove this heat and a large part of this is supplied directly to the gear face. Assessing the performance of coolants and minimising the buildup of oil in the system is therefore a critical stage in the design process. Traditionally, finite volume CFD methods have been used to compute flow and heat transfer solutions. More recently, Lagrangian methods such as Smoothed Particle Hydrodynamics (SPH) have also been applied. The Lattice Boltzman Method (LBM) is a mesoscopic particle based method which uses statistical properties of particles based at each point of a lattice to calculate flow properties. This is a fully transient method and allows for a simple and efficient derivation of LES turbulence properties. In this work the Lattice Bolztman Method is used to investigate the impingement of an oil jet on a rotating spur gear. A comparison of LBM simulations is made against published work using other methods such as SPH and CFD — utilising the Volume of Fluid method — as well as a qualitative comparison with published experimental high speed images. These all show an excellent agreement and the simulations take the same order of magnitude of computational power as 3D single phase SPH, but are fully multiphase and have LES turbulence. This method is then used to investigate how changes to the oil feed delivery rate affect the spreading of the oil jet on the gear tooth and the splashing profiles. The potential for applying this method to other scenarios, such as lubricating and cooling meshing gears, is also discussed.
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基于点阵玻尔兹曼法(LBM)研究油射流对旋转齿轮的冲击
为了提高燃油效率和减少航空发动机的二氧化碳排放,可以使用周转减速齿轮箱来断开涡轮和风扇之间的联系,使发动机能够以更高的涵道比运行。然而,即使是很小的功率损失也会产生大量的热量,这是由于变速箱传递的高负荷。需要大量的冷却来去除这些热量,其中很大一部分直接提供给齿轮表面。因此,在设计过程中,评估冷却剂的性能并最大限度地减少系统中的油积聚是一个关键阶段。传统上,有限体积CFD方法已被用于计算流动和传热解。最近,拉格朗日方法,如光滑粒子流体力学(SPH)也被应用。晶格玻尔兹曼方法(Lattice Boltzman Method, LBM)是一种基于介观粒子的方法,它利用粒子在晶格上每一点的统计特性来计算流动特性。这是一种完全瞬态的方法,可以简单而有效地推导LES湍流特性。本文采用点阵玻尔兹曼方法研究了油射流对旋转直齿轮的冲击。将LBM模拟与已发表的使用SPH和CFD(利用流体体积法)等其他方法的工作进行了比较,并与已发表的实验高速图像进行了定性比较。模拟结果与三维单相SPH的计算能力相同,但完全是多相的,并且具有LES湍流。然后使用该方法来研究油送进率的变化如何影响油射流在齿轮齿和飞溅剖面上的扩散。还讨论了将这种方法应用于其他场景的可能性,例如润滑和冷却啮合齿轮。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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