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  1. NTU Theses and Dissertations Repository
  2. 工學院
  3. 機械工程學系
請用此 Handle URI 來引用此文件: http://tdr.lib.ntu.edu.tw/jspui/handle/123456789/16970
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dc.contributor.advisor黃光裕
dc.contributor.authorTing-Kang Yenen
dc.contributor.author顏廷剛zh_TW
dc.date.accessioned2021-06-07T23:51:17Z-
dc.date.copyright2014-03-08
dc.date.issued2013
dc.date.submitted2014-01-20
dc.identifier.citation[1] 賴耿陽,“超音波工學理論實務”,復漢出版社,2001.
[2] 蘇品書,“特殊加工”,復漢出版社,2001.
[3] Cleave, D.V., “Ultrasonic Gets Bigger Jobs in Machining and Welding”, Iron Age, 1976, pp. 69-72.
[4] Komaraiah, M., Manan, M.A., Reddy, P.N., and Victor, S., “Investigation of Surface Roughness and Accuracy in Ultrasonic Machining”, Precision Engineering, Vol.10, No.2, 1988, pp. 59-65.
[5] Treadwell, C. and Pei, Z.J., “Machining Ceramics with Rotary Ultrasonic Machining”, Ceramic Industry, 2003, pp. 39-42.
[6] Graff, K.F., “Ultrasonic Machining”, Ultrasonics, 1975, pp. 103-109.
[7] Pei, Z.J., Khanna, N., and Ferreira, P.M., “Rotary Ultrasonic Machining of Structural Ceramic - A Review”, Ceramic Engineering and Science Proceedings, 16 (1), 1995, pp. 259-278.
[8] Khoo, C.Y., Hamzah, E., and Sudin, I., “A Review on The Rotary Ultrasonic Machining of Advanced Ceramics”, Journal Mekanikal, No. 25, 2008, pp. 9-23.
[9] Onikura, H., Ohnishi, O., Feng, J., Kanda, T., Morita, T., and Bopp, U., “Effects of Ultrasonic Vibration on Machining Accuracy in Micro-drilling”, Int.J.JSPE, Vol. 30, No. 3, 1996, pp. 1633-1637.
[10] 丁貫中, “整合微型氣靜壓軸承之微型氣動加工具系統之設計開發與性能研究”, 台灣大學碩士論文, 2010.
[11] 陳維智, “整合於微型氣動轉子之軸向振動器設計開發與性能研究”, 台灣大學碩士論文, 2012.
[12] Dyson, J.E. and Darvell, B.W., “The Development of The Dental High Speed Air Turbine Handpiece – Part 1”, Aust Dent J, Vol. 38(1), 1993, pp. 49-58.
[13] Dyson, J.E. and Darvell, B.W., “The Development of The Dental High Speed Air Turbine Handpiece – Part 1”, Aust Dent J, Vol. 38(2), 1993, pp. 131-144.
[14] Dyson, J.E. and Darvell, B.W., “The Development of The Dental High Speed Air Turbine Handpiece – Part 1”, Aust Dent J, Vol. 38(6), 1993, pp. 131-143.
[15] 王識鈞, “精密微型雙動力超高速氣渦輪之設計與開發”, 台灣大學博士論文, 2012.
[16] Naudascher, E. and Rockwell, D., “Flow-Induced Vibrations: An Engineering Guide”, A.A. Balkema, Rotterdam, 1994.
[17] Chen, S.S. and Wambsganns, M.W., “Parallel Flow Induced Vibration of Fuel Rods”, Nuclear Engineering Design, Vol. 18, 1972, pp. 253
[18] Aguirre, J.E., “Flow-Induced, In-line Vibrations of A Circular Cylinder”, Dissertation, Imperial College of Science and Technology, London, 1977
[19] Den Hartog, J. P., “Mechanical Vibrations”, 3rd ed., McGraw-Hill, 1947.
[20] Nakamura, T. and Kaneko, S., “Flow-Induced Vibrations: Classifications and
Lessons from Practical Experiences”, Elsevier Ltd., 2008.
[21] 李宇修, “微型氣壓振動器之設計開發與性能研究”, 台灣大學碩士論文, 2009.
[22] Mattiat, O., “Transducers for Producing Ultrasonic Waves”, Journal of the Acoustical Society of America, Vol. 25, Issue 2, 1953, pp. 291-296.
[23] Dotson, Jr., U.S. Patent 4609368, Sep. 2, 1986.
[24] Ensminger, D. and Stulen, F.B., “Ultrasonics: Data, Equations, and Their Practical Uses”, Taylor and Francis Group, US, 2009.
[25] 宋碩, “噴注式聲波發生器在油田中的應用與優化”, 中國石油大學碩士論文, 2009.
[26] Brun, E. and Boucher, R.M.G., “Research on the Acoustic Air‐Jet Generator: A New Development”, Journal of the Acoustical Society of America, Vol. 29, Issue 5, 1957, pp. 573-583.
[27] Hartmann, J., “Construction, Performance and Design of the Acoustic Air-jet Generator”, Journal of Scientific Instruments, Vol. 16, Issue 5, 1939, pp. 140-149.
[28] The University New South Wales, Helmholz Resonance, http://www.phys.unsw.edu.au/jw/Helmholtz.html
dc.identifier.urihttp://tdr.lib.ntu.edu.tw/jspui/handle/123456789/16970-
dc.description.abstract超音波輔助鑽削經證實可以有效提升高硬度材料的切削效率。高頻振動能夠容易地以電能實現,但在牙醫手機潮濕使用環境會有漏電的安全疑慮。本論文目的在於設計開發軸向氣壓振動器整合於現有的微型氣渦輪筒匣,以高壓空氣為動力源來產生高頻率的軸向振動。
由於低能源消耗,自激式振動原理被選用來進行氣壓振動器的設計開發,激振源引用空腔共振現象,並利用壓力釋放與回復機制將氣體壓力能不間斷的轉換為振動動能。設計流程首先透過理論探討研究氣壓振動器的原理與影響因素,再依據開發得的實體設計模型,執行流場動態模擬(CFD)以深入瞭解最佳化設計參數與振動性能之間的關係。依據最佳化結果,一些雛型氣壓振動器被精密地開發出來。透過實驗測試,驗證負載對雛型氣壓振動器性能 - 振幅與頻率 - 之影響。最後透過氣壓振動器和微型氣渦輪筒匣的整合測試,證實了超音波輔助鑽削的性能。
實驗結果驗證了空腔共振式氣壓振動器的可行性,在無軸向負載的情況下,供氣壓力5.5 bar時,振動頻率最高可達674 Hz,振幅為91 μm。在軸向負載情況和供氣壓力4 bar時,氣壓振動器可以承受最大負載達2035 mN,振動頻率為535 Hz,振幅為93 μm。500 mN徑向負載下的氣渦輪筒匣可以透過氣壓振動器的輔助,在頻率341 Hz的軸向振動下有效提升切削率達2.5倍。
zh_TW
dc.description.abstractThe ultrasonic assisted drilling has been verified to be able to significantly improve the cutting efficiency of high hard materials. High-frequency vibrations can be easily realized by electric power. But there are some security concerns such as electrical leakage in humid environment for application of dental handpiece. The aim of this thesis is to develop a pneumatic axial vibrator integrated with the existing air turbine cartridge. High pressure air is applied as the power source to create high frequency axial vibration.
Because of less power consumption, the self-excited vibration is chosen as the working principle of the developed pneumatic vibrator, and its excitation source draws on the cavity resonance phenomenon. The pressure relief and recovery mechanism is designed to continuously convert the gas pressure into the kinetic energy of vibration. Firstly through the theoretical analysis, the working principle and the influential parameters of the pneumatic vibrator are studied and evaluated. According to its derived embodiment design, the CFD simulation is carried out to comprehend and optimize the relationship between the design parameters and the vibration performance. Based on the optimized result, the prototypes are precisely developed. The developed prototypes are experimentally tested to verify the influence of load on their performance - vibration amplitude and frequency. Finally through the integration testing of the pneumatic vibrator and the air turbine cartridge, the ultrasonic assisted drilling performance is also confirmed.
The experimental results demonstrate that the cavity resonance effect is feasible to drive the pneumatic vibrator. Without axial load, the pneumatic vibrator can create an amplitude of 91 μm at the frequency of 674 Hz for the air pressure of 5.5 bar; and it can withstand a maximum load of 2035 mN by supplying an air pressure of 4 bar and achieve an amplitude of 93 μm at the frequency of 535Hz. The air turbine cartridge under a radial load of 500 mN can be assisted by the pneumatic vibrator to effectively enhance its cutting rate by 2.5 times that without axial vibration at the frequency of 341 Hz.
en
dc.description.provenanceMade available in DSpace on 2021-06-07T23:51:17Z (GMT). No. of bitstreams: 1
ntu-102-R00522617-1.pdf: 13035545 bytes, checksum: f928fc4a51fe96dcf801d4dafc99a19e (MD5)
Previous issue date: 2013
en
dc.description.tableofcontents口試委員會審定書 i
誌謝 ii
中文摘要 iii
Abstract iv
目錄 v
圖目錄 vii
符號表 ix
第一章 緒論 1
1.1 研究背景與動機 1
1.2 文獻回顧 3
1.2.1 超音波輔助鑽削 3
1.2.2 牙醫用微型氣渦輪筒匣 4
1.2.3 氣壓振動器 4
1.3 研究目標與章節內容摘要 10
第二章 空腔共振式氣壓振動器之原理與理論分析 11
2.1 空腔共振式氣壓振動器系統組成 11
2.2 自激式振動 12
2.2.1 原理 12
2.2.2 理論分析 15
2.3 空腔共振現象 23
2.3.1 Hartmann笛的運作原理 24
2.3.2 Hartmann笛的理論分析 27
2.4 壓力釋放與回復機制 30
2.4.1 原理 30
2.4.2 理論分析 36
第三章 空腔共振式氣壓振動器之實體設計 39
3.1 振動器整體架構 39
3.2 空腔共振激發源 42
3.3 排氣閥常關機制 43
3.4 流場模擬分析 46
3.4.1 自激式振動 46
3.4.2 壓力釋放與回復機制 51
3.5 微型氣渦輪筒匣整合空腔共振式氣壓振動器 56
第四章 微型氣渦輪筒匣整合空腔共振式氣壓振動器之性能量測 58
4.1 軸向振動頻率與振幅量測 58
4.2 軸向承載力量測 69
4.3 切削能力量測 72
第五章 結論與未來展望 74
參考文獻 76
附錄A 霍爾效應感測器(3503) 79
附錄B 荷重元(LVS-2kA) 81
附錄C 訊號放大器(DPM-712B) 82
附錄D 資料擷取卡(NI-6008) 84
dc.language.isozh-TW
dc.subject壓力釋放與回復機制zh_TW
dc.subject超音波輔助鑽削zh_TW
dc.subject微型氣渦輪筒匣zh_TW
dc.subject氣壓振動器zh_TW
dc.subject自激式振動zh_TW
dc.subject空腔共振現象zh_TW
dc.subjectSelf-excited vibrationen
dc.subjectPressure relief and recovery mechanismen
dc.subjectCavity resonanceen
dc.subjectUltrasonic assisted drillingen
dc.subjectMiniature air turbine cartridgeen
dc.subjectPneumatic vibratoren
dc.title空腔共振式氣壓振動器之設計開發與性能研究zh_TW
dc.titleDesign and Research of Cavity Resonant Type of Pneumatic Vibratoren
dc.typeThesis
dc.date.schoolyear102-1
dc.description.degree碩士
dc.contributor.oralexamcommittee蔡得民,陳美勇
dc.subject.keyword超音波輔助鑽削,微型氣渦輪筒匣,氣壓振動器,自激式振動,空腔共振現象,壓力釋放與回復機制,zh_TW
dc.subject.keywordUltrasonic assisted drilling,Miniature air turbine cartridge,Pneumatic vibrator,Self-excited vibration,Cavity resonance,Pressure relief and recovery mechanism,en
dc.relation.page86
dc.rights.note未授權
dc.date.accepted2014-01-21
dc.contributor.author-college工學院zh_TW
dc.contributor.author-dept機械工程學研究所zh_TW
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