首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >EXPERIMENTAL INVESTIGATION OF THE NOISE GENERATION AND PROPAGATION FOR DIFFERENT TURNING MID TURBINE FRAME SETUPS IN A TWO-STAGE TWO-SPOOL TEST TURBINE
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EXPERIMENTAL INVESTIGATION OF THE NOISE GENERATION AND PROPAGATION FOR DIFFERENT TURNING MID TURBINE FRAME SETUPS IN A TWO-STAGE TWO-SPOOL TEST TURBINE

机译:两段式两段试验涡轮中不同回转中间涡轮框架设置的噪声产生和传播的实验研究

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The paper deals with the investigation of the noise generation in the two-stage two-spool test turbine located at the Institute for Thermal Turbomachinery and Machine Dynamics (ITTM) at Graz University of Technology. The rig went into operation within the EU-project DREAM, where the target was to investigate the aerodynamics of interturbine flow ducts. The facility is a continuously operating cold-flow open-circuit plant which is driven by pressurized air. The flow path contains a transonic turbine stage (HP) followed by a low pressure turbine stage consisting of a turning mid turbine frame and a counter-rotating LP-rotor. Downstream of the low pressure turbine a measurement section is instrumented with acoustic sensors. The acquisition system consists of a fully circumferentially traversable microphone array located at the outer casing, while at the hub endwall a stationary flush mounted microphone is placed as a reference. Additionally a new embedded concept for the turning mid turbine frame was tested. Here, two zero-lift splitters were located into the vane passage. In order to evaluate the noise emission of the turbine the facility was instrumented with a new acoustic measurement setup which is presented in the paper. Therefore the emitted sound pressure level and the microphones signal spectra are compared for both configurations. The acoustic field was characterized by azimuthal modes by means of a microphone array traversed over 360 degrees. In the multisplitter configuration, the propagating modes due to the HP turbine are found suppressed by 5 dB, while the increase in amplitude of the modes related to the LP turbine is negligible. The overall effect is a reduction of the acoustic emission for the turning mid turbine frame with embedded design.
机译:本文研究了位于格拉茨工业大学热力涡轮机械和机械动力学研究所(ITTM)的两级两阀测试涡轮机中噪声的产生。该钻机在欧盟DREAM项目中投入运行,目标是研究涡轮流道的空气动力学特性。该设施是一个连续运行的冷流开路设备,由压缩空气驱动。流动路径包含一个跨音速涡轮机级(HP),其后是一个低压涡轮机级,该低压涡轮机级由一个旋转中型涡轮机框架和一个反向旋转的LP转子组成。在低压涡轮机的下游,测量部分装有声传感器。采集系统由位于外壳上的全周向可遍历麦克风阵列组成,而在集线器端壁处放置了一个固定的齐平安装式麦克风作为参考。此外,还测试了用于旋转中型涡轮机框架的新嵌入式概念。在这里,两个零升力分离器位于叶片通道中。为了评估涡轮机的噪声排放,在设备中安装了一种新的声学测量装置,该装置已在本文中进行了介绍。因此,比较了两种配置的发射声压级和麦克风信号频谱。声场通过在360度上移动的麦克风阵列以方位角模式进行表征。在多分流器配置中,发现由HP涡轮引起的传播模式被抑制了5 dB,而与LP涡轮相关的模式的幅度增加可忽略不计。总体效果是减少了嵌入式设计的旋转中型涡轮机框架的声发射。

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