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  • 學位論文

氣靜壓式精密單軸定位減振平台之設計開發與特性探討

Design and Development of a Uniaxial Precision Aerostatic Actuation Platform with Vibration Isolation and Research on Its Performance

指導教授 : 黃光裕
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摘要


本論文整合矩形氣靜壓軸承及平行流場式精密調壓閥開發出高精密度位移致動平台。矩形氣靜壓軸承藉由分離式概念完成節流孔實體設計,其中雙列徑向複合節流孔可提供致動器抵抗外界力矩的能力,同時減少致動過程中的摩擦力,使致動精度提昇;而軸向孔口節流孔由於擁有高負載能力之特性,因此可配合輸入氣體壓力差達成致動平台往復致動的目標。平行流場式精密調壓閥採用改變長度及流道造型之概念來調整進入致動平台的氣體壓力。性能分析探討上則透過有限元素分析及實驗找出矩形氣靜壓軸承之負載能力與間隙關係,以及平行流場式精密調壓閥之輸出壓力差與作動角度之關係。

並列摘要


The thesis presents a design of a novel aerostatic linear actuation platform and precise pressure regulator. The rectangular aerostatic bearing is divided into three parts to accomplish the radial and axial restrictor. The radial compound restrictors in double rows have sufficient stiffness to against the pitching moment. Furthermore, the frictionless aerostatic film can support the actuator to increase the actuation accuracy. Two axial orifice restrictors provide outstanding loading capacity for the actuator and realize reciprocating actuation through regulation of their differential pressure. By using the parallel-field concept, the precise pressure regulator is accomplished through variation of length and shape of the flow channel, and it can further regulate the supply pressure for the actuator. For studying and verifying the performance, the finite element analyses and the experiments are carried out to find out the relationship between the loading capacity and the air gap, and the relationship between the differential pressure and the regulating angle of the precision pressure regulator.

參考文獻


[29] 蕭宇均,“止推氣靜壓軸承之磁變形致動節流裝置之設計與開發與性能測試分析”,台灣大學碩士論文,2006。
[35] 吳佳霖,“小型氣靜壓式導引高精度電磁致動器之設計與性能分析”,台灣大學碩士論文,2007。
[2] Reynold, O., “On the Theory of Lubrication and Its Application to Mr. Beauchamp Tower’s Experiments, Including an Experimental Determination of the Viscosity of Olive Oil “, Philosophical Trans. R. Soc. London, Vol. 177, 1886, pp.157-234.
[3] Majumdar, B. C. and Singh, K. C., “Analysis of Aerostatic Thrust Bearings with Offset Load”, International Journal of Machine Tool Design & Research, Vol. 13, 1973, pp.65-76.
[4] Fourka, M., Yong, T., and Marc, B., “Prediction of the stability of air thrust bearings by numerical, analytical and experimental methods”, Wear, Vol. 198, 1996, pp.1-6.

被引用紀錄


張耿寧(2011)。氣磁浮減振平台開發與性能探討〔碩士論文,國立臺灣大學〕。華藝線上圖書館。https://doi.org/10.6342/NTU.2011.10230
丁貫中(2010)。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〔碩士論文,國立臺灣大學〕。華藝線上圖書館。https://doi.org/10.6342/NTU.2010.00523
吳翰杰(2010)。整合套杯式氣靜壓軸承之氣渦輪轉子系統之設計開發與性能探討〔碩士論文,國立臺灣大學〕。華藝線上圖書館。https://doi.org/10.6342/NTU.2010.00348
郭鈞瑋(2009)。氣磁浮軸承式牙醫手機筒匣之設計開發與性能研究〔碩士論文,國立臺灣大學〕。華藝線上圖書館。https://doi.org/10.6342/NTU.2009.02802

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