首页> 外文会议>ASME(American Society of Mechanical Engineers) Turbo Expo vol.4 pt.B; 20070514-17; Montreal(CA) >ACOUSTIC AND VIBRATIONAL ANALYSES ON A MULTI-STAGE COMPRESSOR FOR UNSTABLE BEHAVIOR PRECURSOR IDENTIFICATION
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ACOUSTIC AND VIBRATIONAL ANALYSES ON A MULTI-STAGE COMPRESSOR FOR UNSTABLE BEHAVIOR PRECURSOR IDENTIFICATION

机译:多级压缩机的声学和振动分析,用于不稳定的行为前兆识别

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The analysis of compressor behavior in critical working conditions, such as rotating stall and surge, represents a key aspect in the turbomachinery research field. In fact, both phenomena can lead to severe damage to the compression system and so the identification of unstable behaviour precursors is needed. The paper shows the test results of an experimental campaign conducted on a small size compressor with six axial stages and one centrifugal stage. In particular, the paper focuses on the analysis of acoustic and vibration measurements for both stationary conditions and for varying-over-time (I.e. gradually increasing) inlet mass flow rate. The correlation between compressor behavior in the operating region close to the surge line and vibration and acoustic measurements is investigated.
机译:压缩机在关键工作条件下的性能分析,例如旋转失速和喘振,代表了涡轮机械研究领域的关键方面。实际上,这两种现象都可能导致压缩系统的严重损坏,因此需要确定不稳定行为的前兆。本文显示了在具有六个轴向级和一个离心级的小型压缩机上进行的实验活动的测试结果。特别是,本文着重分析了在固定条件下以及随时间变化(即逐渐增加)的入口质量流量的声学和振动测量结果。研究了在接近喘振线的工作区域中压缩机行为与振动和声学测量之间的相关性。

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