• Title/Summary/Keyword: vacuum pump

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Hyunmin GVT's Cryopump Story (현민 지브이티(GVT) 크라이오 펌프 이야기)

  • Lee, Dong Ju
    • Vacuum Magazine
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    • v.2 no.3
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    • pp.23-29
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    • 2015
  • Cryopump(cryogenic pump), with integrating cryogenic skills into vacuum technology, is the most popular high vacuum pump system, which is widely used at the commercial vacuum industries with TMP. Hyunmin GVT, Inc. is the domestic unique professional manufacturer of the cryopump systems. About ten years ago, while GVT succeeded in domestically producing cryopump systems, this high technology initiated from US became localized completely. But the process of the home production was not easy. It was possible through many trials and errors and after efforts and sacrifices of our engineers. Now many users and customers have the benefit of the advantage and excellence of the domestic cryopump systems. Especially, these days GVT is conducting researches and developments regarding low vibration cryopump and large-sized CWPs and Cryo-TMPs.

Consideration on the performance test procedure of a turbomolecular pump and a compound molecular pump (터보분자펌프 및 복합분자펌프의 성능시험절차에 대한 고찰)

  • 인상렬;박미영
    • Journal of the Korean Vacuum Society
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    • v.10 no.3
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    • pp.303-311
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    • 2001
  • The pumping speed and the maximum compression ratio as well as the critical backing pressure as main parameters representing normal and limiting performance of a turbomolecular pump and a compound molecular pump were measured basing on a draft KS of the acceptance test procedure. Characteristics of the molecular pumps of two different kinds were compared and some points for improving regulations of the test procedure were proposed.

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Digital Linear Control System for a Magnetic Bearing System of a High Vacuum Turbomolecular Pump (고진공 터보 분자펌프용 자기베어링 시스템의 디지털 선형 제어시스템)

  • Ro, Seung-Kook;Kyung, Jin-Ho;Park, Jong-Kweon;Nam, Woo-Ho;Koh, Deug-Yong
    • Journal of the Korean Vacuum Society
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    • v.19 no.4
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    • pp.256-264
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    • 2010
  • In this paper, a digital controller of magnetic bearing system for a high vacuum turbomolecular pump (TMP) is designed and examined. For stabilizing and providing damping in magnetic bearing, the digital PID controller is applied for each 5 control axes, and the inter-axis cross feedback controller is also applied to suppress low frequency vibration caused by gyroscopic moment of the rotor at high speed of rotation. The fabricated rotor-shaft has its first flexible natural frequency lower than maximum speed, about 614Hz, so the two lead filters are applied to increase damping of flexible mode. Notch filters with rotating frequency were selected to reduce vibration of the pump housing caused by unbalance load. The implemented controllers are verified by examination of frequency response and rotating test up to 40,000 rpm, which is higher than critical speed of backward flexible mode.

Mass flow rate of Knudsen pump According to Membrane Type for Micro Propulsion Applications (초소형 추진장치에 적용을 위한 누센펌프의 멤브레인 종류에 따른 질유량 특성)

  • Kim, Hye-Hwan;Huh, Hwan-Il
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.11a
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    • pp.36-40
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    • 2008
  • Minimization of nozzle induces many flow losses in micro-propulsion system. In this study, we studied about thermal transpiration based new conceptual micro propulsion system to overcome these losses. Thermal transpiration device(Knudsen pump) having no moving parts can self-pump the gaseous propellant by temperature gradient only (cold to hot). We designed, fabricated the knudsen pump and analyzed pressure gradient efficiency of membrane according to Knudsen number under vacuum condition. In this paper, we compared mass flow rate of Knudsen pump by using different membrane type ; Polyimide and Hangi, Korean traditional paper.

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Vacuum Test of Cavity with Liquid Nitrogen

  • Choi, Suk;Park, Gunn-Tae;Kim, Heetae
    • Applied Science and Convergence Technology
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    • v.24 no.5
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    • pp.132-135
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    • 2015
  • Schematic of RAON vacuum system is introduced. Vacuum test for superconducting cavity with liquid nitrogen is performed. Schematic plan for RAON vacuum system is introduced and vacuum control system for superconducting cavity test is constructed. Vacuum pressure of cavity is shown as a function of pumping time. The temperature of cavity is shown as a function of cooling time. Outgassing species from cavity is also detected. Detailed experimental procedure is presented to test the cavity vacuum with liquid nitrogen.

Performance Estimation and Test of Protype Pulse Tube Cryopump (맥동관형 크라이오펌프 시제품 성능예측과 평가)

  • In, Sang Ryul;Kang, Sang Paek
    • Journal of the Korean Vacuum Society
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    • v.22 no.2
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    • pp.45-54
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    • 2013
  • The cryopump of the pulse tube type has been developed successfully, and manufacturing of a prototype pump is finished under leading of Woosung Vacuum. The target pumping speed of the prototype pump is above 3,600 L/s for nitrogen with the intake port of 14 inches I.D (16 inches O.D). For designing optimally the pump structure including the charcoal array, thermal shield, and baffle, the pumping speed was simulated for various configurations through Monte Carlo method. Pumping performances of the protype cryopump manufactured on the basis of optimal design were conformed experimentally with a standard test system and procedures. The measured $N_2$ pumping speed of the prototype cryopump was 4,600 L/s which agreed well with simulated one and exceeded the target value.

Characteristic Study of Micro-Nozzle Performance and Thermal Transpiration Based Self Pumping in Vacuum Conditions

  • Jung, Sung-Chul;Huh, Hwan-Il
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.03a
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    • pp.866-870
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    • 2008
  • In this study, we designed cold gas propulsion system with minimum 0.25 mm nozzle and micro-thrust measurement system to analyze flow characteristic of micro propulsion system in ambient and vacuum condition. Argon and Nitrogen are used for propellant and the result of experiments is compared with CFD analysis and theory. But there is a point where reduced scale versions of conventional propulsion systems will no longer be practical. Therefore, a fundamentally different approach to propulsion systems was taken. That is thermal transpiration based micro propulsion system. It has no moving parts such as lubricants, pressurizing system and can pump the gaseous propellant by temperature gradient only(cold to hot). We are advancing basic research of propulsion system based on thermal transpiration in vacuum conditions and had tried experiment process and theoretical access in advance. To characterize membrane of Knudsen pump, we select Polyimide material that has low thermal conductivity(0.29 W/mK) and can stand high temperature($300^{\circ}C$) for long time. And we fabricated hole diameter 1, 0.5, 0.2, 0.1 mm using precision manufacturing. Experimental results show that pressure gradient efficiency of Knudsen pump is increased to maximum 82% according to Knudsen number and thick membranes are more effective than thin membranes in transition flow regime.

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