首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >EXPERIMENTAL AND TOMOGRAPHY-BASED CFD INVESTIGATIONS OF THE FLOW IN OPEN CELL METAL FOAMS WITH APPLICATION TO AERO ENGINE SEPARATORS
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EXPERIMENTAL AND TOMOGRAPHY-BASED CFD INVESTIGATIONS OF THE FLOW IN OPEN CELL METAL FOAMS WITH APPLICATION TO AERO ENGINE SEPARATORS

机译:基于断层摄影和实验的CFD研究,用于航空发动机分离器

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Oil-air separation is a key function in aero engines with closed-loop oil systems. Typically, aero engine air/oil separators employ the use of a porous medium such as open cell metal foams, as a secondary separation mechanism. Assessing its impact on overall separation is important since non-captured oil is released overboard. Computational fluid dynamics offers a possibility to evaluate the metal foam separation effectiveness. A pore scale numerical modelling methodology is applied to determine the transport properties of fluid flow through open cell metal foams. Microcomputer tomography scans were used to generate a 3D digital representation of commercial open cell metal foams of different grades. Foam structural properties such as porosity, specific surface, pore size distribution and the minimum size of a representative elementary volume are directly extracted from the CT scans. Subsequently, conventional finite volume simulations are carried out on the realistic tomography-based foam samples. Simulations were performed for a wide range of Reynolds numbers. The feasibility of using standard Reynolds-averaged Navier-Stokes (RANS) turbulence models is investigated here. As part of the method validation, samples with varying lengths were simulated. Pressure drop values were compared on a length-normalized basis against in-house experimental data. The oil phase was modelled using a Lagrangian particle tracking approach. Boundary conditions for the oil phase were extracted from a previous CFD simulation of a full breather de- vice in the ground idle regime (worst separation effectiveness). Steady state particle tracking simulations were run for droplet diameters ranging from 0.5 - 15 μm, and for flow inlet velocities ranging from 10 - 60 m/s. Stochastic tracking was taken into account in order to model the effects of turbulence on the particle trajectories. Simulations were run on different types of foam and the results are compared qualitatively. The procedure has shown that pore scale modelling is a valid tool to capture the flow field and model oil separation inside open cell metal foams. However, at the moment there is no experimental data available for validation of the oil phase modelling.
机译:油气分离是带有闭环机油系统的航空发动机的关键功能。通常,航空发动机的空气/油分离器采用多孔介质(例如开孔金属泡沫)作为第二分离机制。评估其对总体分离的影响很重要,因为未捕获的油会释放到船外。计算流体动力学为评估泡沫金属分离效果提供了可能性。应用孔尺度数值建模方法来确定流体流过开孔金属泡沫的传输特性。使用微型计算机断层扫描技术生成不同等级的商用开孔金属泡沫的3D数字表示。直接从CT扫描中提取泡沫的结构特性,例如孔隙率,比表面积,孔径分布和代表性基本体积的最小尺寸。随后,对基于实际层析成像的泡沫样品进行常规的有限体积模拟。针对广泛的雷诺数进行了仿真。在此研究了使用标准雷诺平均Navier-Stokes(RANS)湍流模型的可行性。作为方法验证的一部分,模拟了不同长度的样品。在长度归一化的基础上,将压降值与内部实验数据进行了比较。使用拉格朗日粒子跟踪方法对油相进行建模。油相的边界条件是从以前在地面空转状态(最差的分离效果)下的全通气装置的CFD模拟中提取的。进行了稳态粒子跟踪模拟,液滴直径范围为0.5-15μm,流入口速度范围为10-60 m / s。为了模拟湍流对粒子轨迹的影响,考虑了随机跟踪。对不同类型的泡沫进行了模拟,并对结果进行了定性比较。该程序表明,孔尺度建模是捕获流场并建模开孔金属泡沫内部油分离的有效工具。但是,目前尚无用于验证油相模型的实验数据。

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