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TRANSIENT TWO-PHASE EFFECTS IN AN AEROENGINE BEARING CHAMBER SCAVENGE TEST RIG

机译:航空发动机轴承室清除试验台的瞬态两相效应

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Aeroengine bearing chambers typically contain bearings, seals, shafts and static parts. Oil is introduced for lubrication and cooling and this creates a two phase flow environment that may contain droplets, mist, film, ligaments, froth or foam and liquid pools. Efficient and effective liquid removal from a bearing chamber is a functional requirement and in recent years the University of Nottingham Technology Centre in Gas Turbine Transmission Systems has been conducting an experimental and computational research program one strand of which is investigating bearing chamber off-take flows. Initial investigations focussed on a chamber where there was a relatively deep pocket for oil collection below the chamber [1, 2]. In more recent studies Chandra et al have investigated a shallower geometry [3]. In both sets of studies, chamber residence volume and wall film thickness data have been obtained for a range of shaft speeds, scavenge ratios and liquid supply rates. Two methods of introducing liquid to the chamber have been used: a film generator that puts liquid directly onto the chamber wall and a droplet inlet system that distributes droplets from the rotating shaft. During some of the previous investigations, visual data relating to the two phase flow in the outlet pipe immediately below the chamber was gathered together with data from pressure transducers one located in this pipe and one on the chamber itself. It has been observed that for some parameter combinations the chamber flow is gravity dominated whereas for others (typically at higher shaft speeds) the flow is shear dominated. During transition between regimes a pressure spike on the pipe pressure transducer is observed and this may be linked to a change in two phase flow regime within the outlet pipe. A study by Baker et al [4] on transient effects in gas-liquid separation has shown pressure spikes during transitions to new equilibrium conditions for two-phase pipe flow where the gas flow rate is suddenly increased. In this paper outlet visualisation, chamber visualisation and pressure data are combined and conclusions are drawn relating to the parameters controlling whether shear or gravity dominate. The effect of the chamber flow regime on the outlet flow regime is assessed and presented. An implication of the analysis is that during transitional conditions a bearing chamber may contain a different quantity of liquid than in steady state conditions.
机译:航空发动机轴承室通常含有轴承,密封件,轴和静态部件。引入润滑和冷却的油,这产生了两种相流环境,可能含有液滴,雾,薄膜,韧带,泡沫或泡沫和液体池。高效且有效的液体从轴承室中移除是一种功能性要求,近年来燃气轮机传输系统中的诺丁汉技术中心大学已经进行了一种实验和计算研究计划,其中一股是调查轴承腔的轴承腔。初步调查专注于腔室,其中腔室下面有一个相对深的口袋[1,2]。在最近的研究中,Chandra等人已经调查了一个浅几何形状[3]。在两组研究中,已经获得了一系列轴速度,清除比率和液体供应率的腔室住宅和壁膜厚度数据。已经使用了将液体引入腔室的两种方法:薄膜发生器,其将液体直接放到腔室壁上和分配旋转轴的液滴系统。在一些先前的研究期间,与腔室紧接在腔室下方的出口管中的两个相流有关的视觉数据与位于该管子中的压力换能器的数据一起聚集在一起,一个在腔室本身上。已经观察到,对于一些参数组合,腔室流量是重力占据主导的,而对于其他(通常在较高的轴速度)上,流量被剪切。在改造之间的转变期间,观察到管压换能器上的压力尖峰,并且这可以与出口管内的两个相流状态的变化连接。 Baker等人[4]在气液分离中的瞬态效应上的研究表明,在转变期间对两相管流动的新平衡条件进行了压力尖峰,其中气体流速突然增加。在本文的出口可视化中,结合了腔室可视化和压力数据,并绘制了与控制剪切或重力占主导地位的参数的结论。评估和呈现腔室流动状态对出口流动状态的影响。分析的含义是在过渡条件期间,轴承室可以包含与稳态条件不同的液体量。

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