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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >On the acoustics of a turning mid turbine frame with embedded design in a two-stage test-turbine
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On the acoustics of a turning mid turbine frame with embedded design in a two-stage test-turbine

机译:带有嵌入式设计的两级试验涡轮机的旋转中涡轮机框架的声学特性

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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 facility is a continuously operating cold-flow open-circuit plant which is driven by pressurized air. The flow path is formed by a transonic turbine stage (high pressure, HP) followed by a low pressure (LP) turbine stage consisting of a turning mid turbine frame and a counter-rotating LP rotor. Downstream of the low pressure turbine the measurement section is instrumented with acoustic sensors. The acquisition system consists of a fully circumferentially traversable microphone array located at the outer casing. Two configurations of turning mid turbine frames were tested. The baseline is an intermediate turbine duct with 16 turning struts. The second one is a new embedded concept for the turning mid turbine frame with two zero-lift splitters placed in the struts' passages. In total 48 vanes (16 struts plus 32 splitter vanes) guide the flow from the HP rotor to the LP rotor. In order to determine the noise emission of both configurations the microphones signal spectra and the emitted sound power level are compared. The acoustic field is characterized by azimuthal and radial modes by means of a microphone array traversed over 360 degrees. In the multi-splitter configuration, the overall sound power level depending on the blade passing frequency of the HP turbine is reduced by 7dB and depending on the blade passing frequency of the LP turbine by 4dB, respectively. The overall effect is a reduction of the acoustic emission for the turning mid turbine frame with embedded design.
机译:该论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。流动路径由跨音速涡轮机级(高压,HP)形成,随后是由旋转中型涡轮机框架和反向旋转LP转子组成的低压(LP)涡轮机级。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可沿周向遍历的麦克风阵列组成。测试了旋转中型涡轮机框架的两种配置。基线是具有16个转向支柱的中间涡轮机管道。第二个是用于旋转中型涡轮机机架的新嵌入式概念,在支柱的通道中放置了两个零升程分流器。总共48个叶片(16个支杆加上32个分流叶片)将流量从高压转子引导至低压转子。为了确定两种配置的噪声发射,比较了麦克风的信号频谱和发射的声功率级。声场的特征是通过横过360度的麦克风阵列的方位角模式和径向模式。在多分离器配置中,取决于HP涡轮机叶片通过频率的总声功率级分别降低7dB,取决于LP涡轮机叶片通过频率的总声功率级分别降低4dB。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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