• 제목/요약/키워드: Molecular pump

검색결과 108건 처리시간 0.034초

터보형 드래그펌프의 배기특성에 관한 실험적 연구 (An Expreimental Study on the Pumping Performance of Various Turbo-Type Drag Pumps)

  • 황영규;허중식;최욱진;권명근
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집B
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    • pp.555-560
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    • 2000
  • An experimental study on pumping characteristics of various turbo-type drag pumps is purformed. The inlet pressures are measured for various outlet pressures of the test pump. The maximum compression ratios for nitrogen are 100,000(Disk-type drag pump+ turbo molecular pump), 10000(Helical-type drag pump+turbo molecular pump), 850 (Helical-type drag pump), 100(disk-type drag pump).

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터보 분자 펌프(Turbomolecular pump)내의 자유 분자 유동에 관한 수치 해석적 연구 (A Numerical Study of a Free Molecular Flow in the Turbomolecular Pump)

  • 황영규;허중식
    • 설비공학논문집
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    • 제8권2호
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    • pp.219-229
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    • 1996
  • In the free molecular flow range, the pumping performance of a turbomolecular pump has been predicted by calculation of the transmission probability employing the integral method and the test particle Monte-Carlo method. The velocities of molecules incident upon a moving blade are given by the random numbers, which are sampled from the Maxwell molecular velocity distribution function. The present results agree quantitatively with the previous known numerical results. For a multi-stage pump, the velocity profile of molecules between two blade rows is not Maxwell distribution. In this case, the Monte-Carlo method is employed to calculate the overall transmission probability for the entire set of blade rows. When the results of the approximate method combining the single stage solutions are compared with those of the Monte-Carlo method for the pump having six rows at C=0.6, the approximate method overestimates as much as 36% in the maximum compression ratio and 19% in the maximum pumping speed than does the Mote-Carlo method.

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우주환경모사기용 진공배기시스템 교체

  • 이상훈;진성호;조혁진;서희준;문귀원
    • 한국진공학회:학술대회논문집
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    • 한국진공학회 2011년도 제41회 하계 정기 학술대회 초록집
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    • pp.102-102
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    • 2011
  • 인공위성이 임무를 수행하는 우주환경은 지상 환경과 달리 고진공 및 극저온의 극한환경으로 지상에서는 제대로 작동하는 것으로 관찰되더라도 우주환경에서는 예상하지 못한 기능장애를 일으켜 위성의 성능에 치명적인 영향을 미치기도 한다. 이에 10-5 torr 이하의 고진공과 -180$^{\circ}C$ 이하의 극저온 환경을지상에서 모사하여 위성체의 안정성 및 신뢰성을 시험한다. 시험에는 열진공챔버라고 불리는 우주환경모사기가 사용이 되며, 기본적으로 챔버 내부 진공형성이 중요하다. 우주환경의 모사를 위해 먼저 저진공펌프로 10-2 Torr 의 저진공을 형성한 후 Turbo-molecular pump 및 Cryopump를 이용하여 10-5 Torr 이하의 고진공을 형성하게 된다. 본 논문에서는 기존 우주환경모사기에 부착된 oil type rotary pump 및 구형 turbo-molecular pump의 교체 과정을 기술한다. 특히, 저진공펌프의 경우는 챔버 내부로의 oil 역류로 인한 오염 문제를 방지하기 위하여 dry type의 펌프가 설치되었다.

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분자 드래그 회전자 형상에 따른 복합분자펌프의 배기성능에 관한 실험적 연구

  • 황영규;권명근
    • 한국반도체및디스플레이장비학회:학술대회논문집
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    • 한국반도체및디스플레이장비학회 2006년도 춘계학술대회
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    • pp.202-205
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    • 2006
  • Recently, high vacuum pumps are widely used in the semi-conduction and liquid-crystal display ( LCD ) process. The composite-type high vacuum pumps are widely used in the various processes. In this study, the pumping performance of composite-type molecular pumps has been investigated experimentally. The experimented pumps are a compound molecular pump ( CMP ) and hybrid molecular pump ( HMP ). The CMP consists with helical-type drag pump, at lower part, and with turbomolecular pump ( TMP ), at upper part. The HMP consists with disk-type drag pump, at lower part, and with TMP, at upper part. The experiments are performed in the outlet pressure of $0.2\;{\sim}\;533\;Pa$. We have measured the ultimate pressure, compression ratio, and pumping speed

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Analysis of Two-Dimensional Flow Fields in the Multi-Stage Turbomolecular Pump Using the DSMC Method

  • Heo, Joong-Sik;Hwang, Young-Kyu
    • International Journal of Air-Conditioning and Refrigeration
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    • 제9권2호
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    • pp.8-18
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    • 2001
  • The direct simulation Monte Carlo Method is applied to investigate the two-dimensional flow fields of a turbomolecular pump(TMP) in both molecular and transition flow regions. The pumping characteristics of the TMP are investigated for a wide range of the Knudsen number. The maximum of compression ratio and of pumping speed strongly depend on the Knudsen number in transition region, while they weakly depend on the Knudsen number in free molecular flow region. The present numerical results show good agreement with the previously known experimental data. Finally. the results of the single blade row in both molecular and transition regions are used to predict the overall performance of a TMP, which has three kinds of blade with 24-rows.

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

  • 인상렬;박미영
    • 한국진공학회지
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    • 제10권3호
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    • pp.303-311
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    • 2001
  • 터보분자펌프와 복합분자펌프의 배기성능을 나타내는 가장 중요한 항목인 배기속도 및 최대압축비와 함께 극한성능을 나타내는 임계배압을 현재 마련되어 있는 KS규격(안)을 준용하여 측정했다. 두 펌프의 성능이 어떤 점에서 차이가 나는지 비교하고 성능평가 절차에 대해 몇 가지 개선점을 제시했다.

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헬리컬형 분자 드래그 펌프의 유동특성에 관한 연구 (A Study on the Pumping Performance of a Helical-type Molecular Drag Pump)

  • 김도행;권명근;황영규
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회B
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    • pp.2723-2728
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    • 2008
  • The present study is numerically and experimentally performed to reveal the pumping characteristics of a helical-type molecular drag pump (HTDP) in the molecular transition flow region. In the experimental study, the pressures are measured simultaneously at the 5 positions along the helical channel of rotor under various conditions of outlet pressure and throughputs, and nitrogen is used as test gas. The outlet pressure is in the range of 26-533 Pa. As results, the local pressure changes are checked corresponding to the various outlet pressure and throughput of HTDP. In the numerical study, Navier-Stokes equations with slip boundary conditions are employed (Re< 1000, Kn< 0.1). The local pressure distribution and the pumping speed are calculated. The numerical results are compared with the experimental results. The numerically computed value agrees with the experimental data within an error of approximately 5%.

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DSMC법을 이용한 터보분자펌프 다단 익렬의 2차원 유동장 해석 (Analysis of two-dimensional flow fields in the multi-stage turbomolecular pump using the DSMC method)

  • 황영규;허중식;박종윤
    • 설비공학논문집
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    • 제12권1호
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    • pp.83-94
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    • 2000
  • The performance of a turbomolecular pump(TMP) in both molecular and transition flow regions is predicted by the numerical solutions of the Boltzmann equation obtained by the direct simulation Monte Carlo method. The compression characteristics of the TMP are investigated for a wide range of the Knudsen number( Kn ). The maximum compression ratios strongly depend on Kn in transition region, while do they weakly on Kn in free molecular flow region. The present numerical results of the single blade row in both molecular and transition regions are used to predict the overall performance of a TMP, which has three kinds of blade with 24-rows.

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원판형 분자 드래그펌프 회전자에 대한 압력 측정 (The Measurement of Vacuum Pressure for the Rotors of Disk-type Molecular drag Pumps)

  • 권명근;김도행;황영규
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2725-2730
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    • 2007
  • Turbo-type molecular drag pumps ( MDPs ) are used in the liquid crystal display ( LCD ), semiconductor and other thin film industries. Siegbahn ( disk-type ) molecular drag pumps are used as high-pressure stages in the hybrid-type turbomolecular pumps, where they can operate in the viscous, the transition and the free molecular flow regime. In this study is performed to investigate the pumping characteristics of three-stage disk-type molecular drag pump ( DTDP ) in the molecular transition flow region. The experiments are measured using five vacuum pressure gauges in the positions for rotors of DTDP. The test is performed with nitrogen gas ( $N_2$ ).

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