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Test bench development for experimental characterisation of oil-air two-phase flow for breather in modern aero-engine oil system

机译:现代航空发动机油系统呼吸器防油两相流试验台的试验台开发

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Aero-engine oil system has to lubricate and cool down the bearings supporting the rotating shaft and gears. To avoid oil leaks the bearing chambers are sealed with compressed air. An oil-air mixture is thus created. As the oil volume is limited, it is important to recover this oil from the air flow before it leaves the engine, thus the flow must undergo a separation process. This task is assigned to the breather. Breathers are fed with a two-phase air-oil flow. Scavenging air flow rate transports oil drops from the inlet, it flows through the breather where the oil gets recovered and cleaner air is expelled through the exit pipes. To evaluate efficiency in different working conditions, variations of the oil flow rate, scavenging air flow rate, rotational speed and droplet size distribution are mandatory. An experimental test bench is developed at ULB - ATM department. It allows to measure and study the different parameters that affect the efficiency of the breathers. This bench is composed by two main line for the supply of air and oil. Parameters like pressure and temperature of the flows are monitored by pressure sensors and thermocouples placed in key points. An electrical driver rotate the breather to test. Part of the bench was dedicated to the definition of the droplet size distribution fed to the breathers. Two different technologies are used to generate droplets: impact injector (bigger granulometries) and air assisted injector (finer granulomerties). Laser diffraction was applied to define droplet size. The results show a common tendency linked to the different working conditions, a higher oil flow rate leads to larger droplets. An increase in the scavenging air flow rate lightly influences the distribution. For the same oil and air flow rate droplets of different sizes are generated by varying the outlet pressure or droplet generation system. This paper presents a description of the objectives, the test facility and the experimental results of granulometries that are generated to feed future breather system. The paper then explains how the inlet granulometries impact future breather performance test.
机译:航空发动机油系统必须润滑和冷却支撑旋转轴和齿轮的轴承。为避免油泄漏,轴承室用压缩空气密封。因此产生油气混合物。随着油量有限的,在留下发动机之前,重要的是从空气流中恢复这种油,因此流动必须经历分离过程。此任务已分配给呼吸状态。呼吸者用两相空气流量喂食。清除空气流量从入口输送油滴,流过呼吸泄漏,清洁空气通过出口管道排出清洁空气。为了评估不同的工作条件下的效率,强制性的油流量,清除空气流速,转速和液滴尺寸分布的变化是强制性的。 ULB - ATM部门开发了一个实验测试台。它允许测量和研究影响呼吸效率的不同参数。这款工作台由两个主要线路组成,供气供应空气和油。使用压力传感器和热电偶监测流量的压力和温度等参数。电驱动器旋转呼吸器以进行测试。部分工作台致力于将液滴尺寸分布的定义定义为呼吸呼吸呼吸。两种不同的技术用于生成液滴:冲击喷射器(更大的粒状化)和空气辅助喷射器(更精细的颗粒体)。施加激光衍射以限定液滴尺寸。结果表明,与不同的工作条件相关的常见趋势,更高的油流量导致较大的液滴。清除空气流量的增加轻微影响分布。对于相同的油和空气流量液滴,通过改变出口压力或液滴产生系统产生不同尺寸的液滴。本文介绍了目标,测试设施和生成的粒状化学的实验结果,以馈送未来的呼吸系统。然后本文解释了入口颗粒测量仪如何影响未来的呼吸器性能测试。

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