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研究生: 黃嘉銘
Huang, Jia-Ming
論文名稱: 聲音及振動訊號之時頻分析
Time-Frequency Analysis of Acoustic and Vibration Data
指導教授: 鄭育能
Jeng, Yih-Nen
學位類別: 碩士
Master
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2007
畢業學年度: 95
語文別: 中文
論文頁數: 79
中文關鍵詞: 聲音數據傅立葉正弦頻譜傅立葉正弦時頻圖滾珠軸承
外文關鍵詞: ball bearing, acoustic data, Fourier sine spectrogram, Fourier sine spectrum
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  • 本文應用傅立葉正弦頻譜和傅立葉正弦時頻圖產生器,對一架遙控電動直升機和無人遙控飛行載具的聲音數據,以及滾珠軸承的振動數據做分析討論。時頻產生器包括:使用疊代式高斯平滑法移除非週期和極低頻部份,再用單調式三次方分段內插法,幫忙定出所剩的週期性部份數據兩端的零點,經內插重新分佈點及奇函數轉換,以快速傅立葉級數轉換法,求取傅立葉正弦頻譜後。隨後對頻譜取有限的帶狀頻帶後,對頻譜做快速傅立葉級數逆轉換,求得傅立葉正弦時頻圖之實數部份,再應用希爾伯特轉換式求振幅並畫出時頻圖。而從時頻圖中可以詳細而正確地看到一堆模組(modes)和其諧波(harmonics),其頻率跟振幅隨著時間變動,因此可以從中檢測出是否有異常情形。本文將對遙控電動直升機分別做主旋翼、尾旋翼及整架直升機之手持狀態做分析。而無人遙控飛行載具部份將單就對其引擎測試,然後實機地面測試最後實地飛行。最後滾珠軸承將對正常狀態、內環損傷、滾珠損傷和外環損傷做時頻分析比較。這些測試顯示本文所用的頻譜和時頻圖,具有可以作為監測完整系統的一種工具之潛力。

    The Fourier sine spectrum and Fourier sine spectrogram generators are employed to examine acoustic data of a remote control unmanned electrical helicopter, an Unmanned Aerial Vehicle (UAV) and vibration data of ball bearing. The transformation contains the following steps. For a given data string whose non-sinusoidal part have been removed, zero points around the two ends are identified by searching and interpolation. After dropping segments beyond two zero ends, the corresponding Fourier sine spectrum is obtained. The time-frequency transform imposes finite bandwidth Gaussian window upon the Fourier sine spectrum centered at a given frequency. The inverse Fourier transform of the band-pass limited spectrum gives the real part of the resulting spectrogram. Form the resulting spectrums much information concerning the dominate modes and corresponding harmonics can be captured. Moreover, the associated amplitude and frequency variations are partially reflected by the spectrum scattering around a mode. The detailed variations can be obtained by examining the spectrogram. This study separately examined the acoustic data of main rotor wing, tail rotor wing and holding by hand of the unmanned electrical helicopter. Many detailed information can be precisely extracted. For the UAV, the engine test information, the ground test information and take-off operation are examined. The result shows that the engine test facility is too rough. For the bearing test, defects of the inner race, rolling element and outer race are compared with the normal state. The resulting spectrum and spectrogram show much new information. These tests show that the spectrum and spectrogram have the potential to monitor the operating state of a complete system.

    中文摘要 I 英文摘要 II 誌謝 IV 目錄 V 圖目錄 VIII 符號說明 XII 第一章 緒論 1 1.1 研究動機 2 1.2 研究目的 3 1.3 文獻回顧 4 第二章 實驗方法 6 2.1 實驗器材 6 2.2 實驗步驟 8 第三章 理論分析 9 3.1 時頻分析 9 3.1.1 修正型單調性三次方分段內插法 9 3.1.2 疊代式濾波器法 10 3.1.3 低誤差傅立葉正弦頻譜法 14 3.1.4 小波法-Morlet轉換式 17 3.1.5 強化的Morlet轉換式 19 3.1.6 希爾伯特(Hilbert)轉換式 20 3.1.7 Gabor轉換式 20 3.1.8 新時頻圖(spectrogram)產生器 21 3.2 滾珠軸承振動之分析 24 第四章 結果與討論 26 4.1 新時頻圖與最佳的Gabor轉換式結果比較 26 4.2 遙控電動直升機之時頻分析 27 4.2.1 尾旋翼部份 27 4.2.2 主旋翼部份 28 4.2.3 整架直升機之手持狀態 30 4.3 無人遙控飛行載具之時頻分析 31 4.3.1 OS.MAX-91FX RING 引擎測試 31 4.3.2 無人遙控飛行載具地面測試 32 4.3.3 無人遙控飛行載具起飛時 32 4.4 滾珠軸承之時頻分析 34 4.4.1 滾珠軸承之正常狀態 35 4.4.2 滾珠軸承之內環損傷 36 4.4.3 滾珠軸承之滾珠損傷 37 4.4.4 滾珠軸承之外環損傷 37 第五章 結論與未來工作 39 參考文獻 41 結果附圖 45 自述 78 著作權聲明 79

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    26. http://www.eecs.case.edu/laboratory/bearing/
    Case Western Reserve University Bearing Data Center Website

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