液壓動力源模組致動器阻流孔壓力對液體流率之影響研究

碩士 === 中華大學 === 機械工程學系碩士班 === 97 === The accumulator (MS-28700-7, MIL-H-5606F) and the hydraulic oil (Hougto Safe1120) were discussed in the present study. The Nitrogen gas was pre-filled into the accumulator with a piston ring to separate the liquid and the gas. The tests were proceeded for differe...

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Main Author: 何國南
Other Authors: 吳泓瑜
Format: Others
Language:zh-TW
Published: 2008
Online Access:http://ndltd.ncl.edu.tw/handle/70503776861766703819
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spelling ndltd-TW-097CHPI54900022015-10-13T13:11:50Z http://ndltd.ncl.edu.tw/handle/70503776861766703819 液壓動力源模組致動器阻流孔壓力對液體流率之影響研究 何國南 碩士 中華大學 機械工程學系碩士班 97 The accumulator (MS-28700-7, MIL-H-5606F) and the hydraulic oil (Hougto Safe1120) were discussed in the present study. The Nitrogen gas was pre-filled into the accumulator with a piston ring to separate the liquid and the gas. The tests were proceeded for different liquid pressure values in the accumulator, then released the liquid for different orifice diameters and choke by the solenoid valve. The relationship between the pressure and the volume with time was obtained. The relationship between the pressure and the volume will be used to the UAV catapult system to be the reference of the basic setting condition. From the result, the pressure of the Nitrogen gas in the accumulator will affect the volume of filling liquid. The higher pressure of Nitrogen gas will lead the lower volume of filling liquid, and the few liquid output will influence the pressure drop obviously. On the contrary, the lower pressure of Nitrogen gas will lead the higher volume of filling liquid. The flow rate was influenced by orifice diameters and choke, especially for the accurate displacement about the volume change. And the accuracy will be increased by the real experiment with the deduction of error, and the surrounding effects (temperature and interface friction) should be considered. From the theoretical and the experimental results, the approximate equation on pressure and volume was obtained by curve fitting method. Therefore, the torque, the flow rate and the rotational speed of the liquid pressure motor can be determined. The flow rate and the pressure were influenced by the orifice diameters and choke obviously. When the length of the choke is longer, the pressure drop is increased. The pressure of the filling liquid (3000psi) in the accumulator was 10 times than the pre-filled pressure of Nitrogen gas (300psi). By means of the results we may derive the equation for the relationship between the pressure and the volume by the curve-fitted method. 吳泓瑜 2008 學位論文 ; thesis 77 zh-TW
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language zh-TW
format Others
sources NDLTD
description 碩士 === 中華大學 === 機械工程學系碩士班 === 97 === The accumulator (MS-28700-7, MIL-H-5606F) and the hydraulic oil (Hougto Safe1120) were discussed in the present study. The Nitrogen gas was pre-filled into the accumulator with a piston ring to separate the liquid and the gas. The tests were proceeded for different liquid pressure values in the accumulator, then released the liquid for different orifice diameters and choke by the solenoid valve. The relationship between the pressure and the volume with time was obtained. The relationship between the pressure and the volume will be used to the UAV catapult system to be the reference of the basic setting condition. From the result, the pressure of the Nitrogen gas in the accumulator will affect the volume of filling liquid. The higher pressure of Nitrogen gas will lead the lower volume of filling liquid, and the few liquid output will influence the pressure drop obviously. On the contrary, the lower pressure of Nitrogen gas will lead the higher volume of filling liquid. The flow rate was influenced by orifice diameters and choke, especially for the accurate displacement about the volume change. And the accuracy will be increased by the real experiment with the deduction of error, and the surrounding effects (temperature and interface friction) should be considered. From the theoretical and the experimental results, the approximate equation on pressure and volume was obtained by curve fitting method. Therefore, the torque, the flow rate and the rotational speed of the liquid pressure motor can be determined. The flow rate and the pressure were influenced by the orifice diameters and choke obviously. When the length of the choke is longer, the pressure drop is increased. The pressure of the filling liquid (3000psi) in the accumulator was 10 times than the pre-filled pressure of Nitrogen gas (300psi). By means of the results we may derive the equation for the relationship between the pressure and the volume by the curve-fitted method.
author2 吳泓瑜
author_facet 吳泓瑜
何國南
author 何國南
spellingShingle 何國南
液壓動力源模組致動器阻流孔壓力對液體流率之影響研究
author_sort 何國南
title 液壓動力源模組致動器阻流孔壓力對液體流率之影響研究
title_short 液壓動力源模組致動器阻流孔壓力對液體流率之影響研究
title_full 液壓動力源模組致動器阻流孔壓力對液體流率之影響研究
title_fullStr 液壓動力源模組致動器阻流孔壓力對液體流率之影響研究
title_full_unstemmed 液壓動力源模組致動器阻流孔壓力對液體流率之影響研究
title_sort 液壓動力源模組致動器阻流孔壓力對液體流率之影響研究
publishDate 2008
url http://ndltd.ncl.edu.tw/handle/70503776861766703819
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