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ANALYTICAL AND NUMERICAL SIMULATION OF THE TWO PHASE FLOW HEAT TRANSFER IN THE VENT AND SCAVENGE PIPES OF THE CLEAN ENGINE DEMONSTRATOR

机译:清洁发动机演示机排气孔和排气管中两相流动传热的解析和数值模拟

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Advanced aircraft engine development dictates high standards of reliability for the lubrication systems, not only in terms of the proper lubrication of the bearings and the gears, but also in terms of the removal of the large amounts of the generated heat. Heat is introduced both internally through the rotating hardware and externally through radiation, conduction and convection. In case where the bearing chamber is in close proximity to the engine's hot section, the external heat flux may be significant. This is, for example, the case when oil pipes pass through the turbine struts and vanes on their way to the bearing chamber. There; the thermal impact is extremely high, not only because of the hot turbine gases flowing around the vanes, but also because of the hot cooling air which is ingested into the vanes. The impact of this excessive heat on the oil may lead to severe engine safety and reliability problems which can range from oil coking with blockage of the oil tubes to oil fires with loss of part integrity, damage or even failure of the engine. It is therefore of great importance that the oil system designer is capable of predicting the system's functionality. As part of the European Research program EEFAE (Efficient and Environmentally Friendly Aero Engine), the project CLEAN (Component vaLidator for Environmentally-friendly Aero-eNngine) [1], [2] was initiated with the goal to develop future engine technologies. Within the scope of this program, MTU Aero Engines has designed the lubrication system and has initiated an investigation of the heat transfer in the scavenge and vent tubes passing through the high thermally loaded TCF (Turbine Center Frame). The objective was to evaluate analytical and numerical models for the heat transfer into the air and oil mixtures and benchmark them. Three analytical models were investigated. A model which was based on the assumption that the flow of air and oil is a homogeneous mixture which was applied on the scavenge flow. The other two models assumed annular two-phase flows and were applied on the vent flows. Additionally, the two phase flow in the scavenge and vent pipes was simulated numerically using the ANSYS CFX package. The evaluation of the models was accomplished with test data from the heavily instrumented test engine with special emphasis on the TCF. Both the analytical and the numerical models have demonstrated strengths and weaknesses. The homogeneousflow model correlation and the most recent correlation by Dr. Busam for vent flows have demonstrated very good agreement between test and computed results. On the other hand the numerical analysis produced remarkable results, however at the expense of significant modeling and computing efforts. This particular work is unique compared to published investigations since it was conducted in a real engine environment and not in a simulating rig. Nevertheless, research in two-phase flow heat transfer will continue in order mitigate any deficiencies and to further improve the correlations and the CFD tools.
机译:飞机发动机的先进发展要求润滑系统具有高标准的可靠性,不仅在轴承和齿轮的正确润滑方面,而且在大量热量散发方面也是如此。热量通过旋转的硬件内部引入,也通过辐射,传导和对流引入外部。如果轴承腔非常靠近发动机的高温区域,则外部热通量可能会很大。例如,当油管穿过涡轮机支柱和叶片到达轴承腔的过程中就是这种情况。那里;热冲击极高,这不仅是因为热的涡轮机气体在叶片周围流动,还因为吸入了叶片中的热冷却空气。过多的热量对机油的影响可能会导致严重的发动机安全性和可靠性问题,其范围可能从因油管堵塞而导致的焦化到因零件完整性受损,发动机甚至出现故障而引起的机油起火。因此,油系统设计人员能够预测系统的功能非常重要。作为欧洲研究计划EEFAE(高效和环保的航空发动机)的一部分,启动了CLEAN(环保型航空发动机的组件验证器)[1],[2]项目,旨在开发未来的发动机技术。在此计划的范围内,MTU航空发动机公司设计了润滑系统,并开始研究通过高热负荷TCF(涡轮中心框架)的排气管和排气管中的热传递。目的是评估将热量传递到空气和机油混合物中的分析模型和数值模型,并对它们进行基准测试。研究了三种分析模型。一个基于以下假设的模型:空气和油的流动是均匀的混合物,被应用于清除流。其他两个模型假定为环形两相流,并应用于排气流。此外,使用ANSYS CFX软件包对扫气管和排气管中的两相流进行了数值模拟。对模型的评估是通过使用配备有大量仪器的测试引擎的测试数据完成的,其中特别强调了TCF。解析模型和数值模型都显示出优点和缺点。同质 流量模型相关性和Busam博士最近对排气流量的相关性已证明测试和计算结果之间具有很好的一致性。另一方面,数值分析产生了显着的结果,但是以大量的建模和计算工作为代价。与公开的研究相比,这项特殊工作是独一无二的,因为它是在真实的发动机环境中而不是在仿真平台上进行的。然而,将继续进行两相流传热的研究,以减轻任何缺陷并进一步改善相关性和CFD工具。

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