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航空發(fā)動(dòng)機整機振動(dòng)測量和分析方法
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V216.8

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Vibration measurement and analysis of aero-engine
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    摘要:

    目前國內仍有很多航空發(fā)動(dòng)機試車(chē)臺使用的是模擬振動(dòng)測量?jì)x,濾波和積分選擇均需針對機型專(zhuān)門(mén)定制,靈活性不夠,同時(shí)也不能分析振動(dòng)頻率,滿(mǎn)足不了發(fā)動(dòng)機振動(dòng)分析的要求。選擇合適的振動(dòng)傳感器、振動(dòng)測量?jì)x并采用合適的軟件分析方法,迅速準確地測量發(fā)動(dòng)機的振動(dòng)值并分析振動(dòng)頻率是發(fā)動(dòng)機廠(chǎng)、所對發(fā)動(dòng)機整機臺架試驗的要求。在發(fā)動(dòng)機整機振動(dòng)測量選擇了壓電式加速度傳感器并使用帶有抗混濾波的差分放大器以消除頻率混疊和共模干擾,編寫(xiě)了專(zhuān)門(mén)的振動(dòng)分析軟件,在振動(dòng)分析軟件處理中采用Butterworth濾波器和Flat Top窗函數。該方法能夠滿(mǎn)足發(fā)動(dòng)機生產(chǎn)廠(chǎng)提出的通帶平滑度≤±5%,阻帶衰減大于-30dB/倍頻程的濾波要求以及對振動(dòng)測量精度≤±5%的要求。通過(guò)研究提出的航空發(fā)動(dòng)機整機振動(dòng)測量方法準確可靠,能夠滿(mǎn)足發(fā)動(dòng)機廠(chǎng)、所對試車(chē)臺架整機振動(dòng)測量的要求。

    Abstract:

    At present, there are still many aero-engine test cell using analog vibration measuring instruments. Filtering and integral selection need to be tailored for the aero-engine type. The flexibility is not enough, and the vibration frequency can not be analyzed, which can not meet the requirements of engine vibration analysis. Choosing the appropriate vibration sensor, vibration measuring instrument and adopting the appropriate software analysis method, measuring the engine vibration value quickly and accurately and analyzing the vibration frequency are the requirements of engine factory and engine test. In this paper, the piezoelectric accelerometer is selected for the vibration measurement of the engine and the differential amplifier with anti-aliasing filter is used to eliminate frequency aliasing and common mode interference. Special vibration analysis software has been compiled, Butterworth filter and Flat Top window function are used in the vibration analysis software. This method can satisfy the filtering requirements of pass-band smoothness < 5%, stopband attenuation greater than - 30dB / octave and vibration measurement accuracy < 5%. The vibration measurement method proposed in this paper is accurate and reliable, and can meet the requirements of engine factory and test cell vibration measurement.

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劉兵.航空發(fā)動(dòng)機整機振動(dòng)測量和分析方法計算機測量與控制[J].,2019,27(5):22-25.

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歷史
  • 收稿日期:2018-11-02
  • 最后修改日期:2018-12-03
  • 錄用日期:2018-12-03
  • 在線(xiàn)發(fā)布日期: 2019-05-15
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