首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >FLOWFIELD AND TEMPERATURE PROFILES MEASUREMENTS ON A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION
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FLOWFIELD AND TEMPERATURE PROFILES MEASUREMENTS ON A COMBUSTOR SIMULATOR DEDICATED TO HOT STREAKS GENERATION

机译:专门用于热条纹生成的燃烧器模拟器上的流场和温度曲线测量

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In order to deepen the knowledge of the interaction between modern lean burn combustors and high pressure turbines, a real scale annular three sector combustor simulator has been assembled at University of Florence, with the goal of investigating and characterizing the generated aerothermal field and the hot streaks transport between combustor exit and the high pressure vanes location. To generate hot streaks and simulate lean burn combustors behavior, the rig is equipped with axial swirlers, fed by main airflow that is heated up to 531 K, and liners with effusion cooling holes that are fed by air at ambient temperature. The three sector configuration is used to reproduce the periodicity on the central sector and to allow to perform measurements inside the chamber, through the lateral walls. Ducts of different length have been mounted on the swirlers, preserving the hot mainflow from the interaction with coolant. Such configurations, together with the one without ducts, have been tested, using different measurement techniques, in order to highlight the differences in the resulting flow fields. First of all, isothermal PIV measurements have been performed on the combustion chamber symmetry plane, to highlight the mixing phenomena between the mainflow and cooling flows. Then a detailed investigation of the mean aerothermal field at combustor exit has been carried out, for nominal operating conditions, by means of a five hole pressure probe provided with a thermocouple, installed on an automatic traverse system. With the aim of analyzing the hot streaks transport and the flow field modification towards the vanes location, such measurements have been performed on two different planes: one located in correspondence of the combustor exit and the further one placed downstream, in the virtual location of the vanes leading edges. Therefore, an experimental database, describing the evolution of the flow field in a combustor simulator with typical traits of modern lean burn chambers, for different injector geometries, has been set up.
机译:为了加深对现代稀薄燃烧燃烧器和高压涡轮机之间相互作用的认识,佛罗伦萨大学已经组装了一个实际规模的环形三扇形燃烧室模拟器,目的是研究和表征产生的空气热场和热条纹。在燃烧室出口和高压叶片位置之间进行运输。为了产生热条纹并模拟稀薄燃烧燃烧器的行为,该钻机配备了轴向旋流器,该旋流器由加热到531 K的主气流供气,还配有带有积液冷却孔的衬套,该衬套由环境温度的空气供入。三扇区配置用于再现中心扇区的周期性,并允许通过侧壁在腔室内进行测量。不同长度的管道已安装在旋流器上,以防止与冷却剂相互作用而产生热的主流。为了突出产生的流场中的差异,已使用不同的测量技术对此类配置以及不带管道的配置进行了测试。首先,在燃烧室对称平面上进行了等温PIV测量,以突出主流和冷却流之间的混合现象。然后,对于标称工况,已通过安装在自动导线系统上的带有热电偶的五孔压力探头对燃烧器出口处的平均空气热场进行了详细研究。为了分析热条纹向叶片位置的传输和流场变化,已经在两个不同的平面上进行了这样的测量:一个位于燃烧室出口对应的平面,另一个位于下游的虚拟平面。叶片前缘。因此,建立了一个实验数据库,该数据库描述了燃烧器模拟器中流场的演变,该模拟器具有现代稀薄燃烧室的典型特征,适用于不同的喷射器几何形状。

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