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  • 學位論文

高速射出油壓伺服系統設計之探討

The Investigation of Hydraulic Servo System Design for High-Speed Injection Molding

指導教授 : 陳夏宗
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摘要


射出成型產品的日趨輕薄短小,使得工業界對射出機在薄殼射出的能力要求愈來愈高,而要使薄殼順利成型,高射速是必要且必然的發展方向之一。 本論文針對高射速射出機的射出油壓伺服系統之架構與設計技術進行探討,本研究主要使用一比例伺服閥於所架設的油壓系統中,控制油壓缸的前進速度;同時加裝一蓄壓器來提供足夠的油壓流量並維持系統的穩定;再於油壓缸末端加入負載,使其模擬射出成型時螺桿遇到的熔膠阻力。藉著這些元件的組合控制,並透過由LabVIEW 軟體撰寫的人機介面監控裝置,來研究、瞭解影響油壓缸前進速度的原因,做為發展高速射出機的設計參考。 本研究並以HyPneu 軟體來模擬驗證實驗的結果並做比較,以確保系統設計的正確性。並由實驗結果來驗證比例伺服閥於射出單元高速前進時的動作特性,基本上模擬能夠大致反應實驗之結果。

關鍵字

伺服閥 射出成型 蓄壓器

並列摘要


3C thin-wall products require to be molded by a high-speed injection molding machines. In this study, we the structure and design of hydraulic proportional-servo valve system in a high-speed injection molding is investigated. The proportional-servo valve was used to build hydraulic platform system. The system can actuate hydraulic forward speed and provide enough flow rate to keep up system stable under the aid of accumulation with and without loading. The human interface was also developed using LabVIEW. HyPneu simulation software used to simulate the system function and compare with experimental data. According to experimental data, we know that the reaction characteristic of proportional-servo valve that used in injection unit will influence the high-speed injection characteristic. Simulation shows well coincidence with measurement.

並列關鍵字

injection molding servo valve accumulator

參考文獻


[3]D. A. Pease, ”Basic Fluid Power “, Prentic-Hall,1967.
[4]E. C. Fitch, JR., ”Fluid Power and Control System”, Mcgraw-Hill, 1966.
[7]J. Watton, ”The Effect of Drain Orifice Damping on Performance Characteristics of a Servo valve Flapper Nozzle Stage ”, Trans. ASME. J. Dyn. Syst., Means. Control,1987,Vol.107,pp.19-23.
[15] LabVIEW Advanced Course Manual, National Instruments,1996
參考文獻

被引用紀錄


陳柏祺(2003)。超高速伺服油壓系統與元件響應時間之研究〔碩士論文,中原大學〕。華藝線上圖書館。https://doi.org/10.6840/cycu200300575
余啟揚(2002)。高速射出油壓伺服系統調控響應 特性之探討〔碩士論文,中原大學〕。華藝線上圖書館。https://doi.org/10.6840/cycu200200542
楊霆遠(2015)。壓縮空氣推動液壓馬達之油路設計及控制方法〔碩士論文,國立清華大學〕。華藝線上圖書館。https://www.airitilibrary.com/Article/Detail?DocID=U0016-0312201510245133

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