• 제목/요약/키워드: Spiral Groove

검색결과 41건 처리시간 0.019초

나선 홈 펌프 실의 누설 및 로터다이내믹 해석 (Leakage and Rotordynamic Analysis of Spiral-Grooved Pump Seal Based on Three-Control-Volume Theory)

  • 하태웅;이안성
    • 한국유체기계학회 논문집
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    • 제6권1호
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    • pp.14-22
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    • 2003
  • In this paper the leakage prediction md rotordynamic analysis of an annular seal with a smooth rotor and spiral-grooved stator is performed. For the development of a theoretical model, the three-control-volume analysis of the circumferentially-grooved seal is expanded by considering pressure reduction due to the pumping effect of spiral groove and pressurized flow through the spiral groove. Validation on the present analysis is achieved by comparisons with available experimental data. For the leakage prediction the present analysis generally shows a reasonable agreement with experimental results. Rotordynamic coefficients for rotor speed with spiral angles show same trend, but the magnitudes of rotordynamic coefficients yield differences between analysis and experimental results.

나선 홈 펌프 시일의 특성 해석 (Characteristic Analysis of Spiral-Grooved Pump Seal)

  • 하태웅;이안성
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문집
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    • pp.799-804
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    • 2002
  • In this paper the leakage prediction and rotordynamic analysis of an annular seal with a smooth rotor and spiral-grooved stator are performed. For developing a theoretical model, the three-control-volume analysis of the circumferentially-grooved seal is expanded by considering pressure reduction due to the pumping effect of spiral groove and pressure flow through the spiral groove. Results by the present analysis are compared with available experimental data. For leakage the analysis results generally show a reasonable agreement to the experimental results. For rotordynamic coefficients the analysis results show the same trend as the experimental results for rotor speed with spiral angles, but their magnitudes show somewhat large deviations.

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내부 원형 그루브를 갖는 저속 드라이 가스 시일의 윤활 성능해석 (Lubrication Performance Analysis of A Low-Speed Dry Gas Seal having An Inner Circular Groove)

  • 이안성;김준호
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 2004년도 학술대회지
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    • pp.201-208
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    • 2004
  • In this study a general Galerkin FE lubrication analysis method was utilized to analyze the complex lubrication performance of a spiral groove seal having an additional inner circular groove, which was designed for a chemical process mixer operating at a low speed of the maximum 500 rpm. Equilibrium seal clearance analyses under varying outer pressure revealed that the seal maintains a certain levitation seal clearance under the outer pressure of more than about 1.5 bar, regardless of a rotating speed. Also, under the normal outer pressure of 11 bar, the axial stiffness of the seal was predicted to have a high value of more than 7.0e+07 N/m, regardless of a rotating speed and thereby, the seal is expected to maintain a stable thickness of lubrication film under a certain external excitation acting.

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나선 홈 펌프 시일의 특성 해석 (Characteristic Analysis of Spiral-Grooved Pump Seal)

  • Ha, Tae-Woong;Lee, An-Sung
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문초록집
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    • pp.379.1-379
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    • 2002
  • In this paper the leakage prediction and rotordynamic analysis of an annular seal with a smooth rotor and spiral-grooved stator are performed. For developing a theoretical model, the three-control-volume analysis of the circumferentially-grooved seal is expanded by considering pressure reduction due to the pumping effect of spiral groove and pressure flow through the spiral groove. Validation to the present analysis is achieved by comparisons with available experimental data. (omitted)

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다양한 곡률을 가진 공기 동압 베어링의 축방향 부하특성 해석 (Analysis of Axial Load Characteristics of Air-Dynamic Bearings of Various Curvatures)

  • 최우천;신용호;최정환
    • 한국정밀공학회지
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    • 제17권3호
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    • pp.129-135
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    • 2000
  • Air-dynamic bearings are increasingly used in supporting small high-speed rotating bodies. This study investigates the effects of design parameters on the axial stiffness of spiral-grooved air bearings of various curvatures. Design parameters are fundamental clearance, groove depth, and bearing number. The pressure distribution at the clearance between the stator and rotor of the bearing is obtained by solving the Reynolds equation, and the supporting load and the axial linear stiffness are calculated from the pressure distribution. It is found that a larger curvature increases the axial linear stiffness more and that there exist an optimal groove depth for the linear stiffness of the air bearing. It is also found that the linear stiffness has a linear relationship with the bearing number.

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내부 원형 그루브를 갖는 저속 드라이 가스 시일의 윤활 성능해석 및 실험 (Lubrication Performance Analysis and Experiment of a Low-Speed Dry Gas Seal having an Inner Circular Groove)

  • 이안성;김준호
    • Tribology and Lubricants
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    • 제21권2호
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    • pp.53-62
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    • 2005
  • In this study a general Galerkin FE lubrication analysis method was utilized to analyze the complex lubrication performance of a spiral groove seal having an additional inner circular groove, which was designed for a chemical process mixer operating at a low speed of the maximum 500 rpm. Equilibrium seal clearance analyses under varying outer pressure revealed that the seal maintains a certain levitation seal clearance under the outer pressure of more than about 1.5 bar, regardless of a rotating speed. Also, under the normal outer pressure of 11 bar, the axial stiffness of the seal was predicted to have a high value of more than 7.0 e + 07 N/m, regardless of a rotating speed and thereby, the seal is expected to maintain a stable thickness of lubrication film under a certain external excitation acting. A seal levitation test rig was designed and constructed. Experimental results at 500 rpm agreed well with analytical predictions and the applied lubrication analysis method was verified.

고속비행체용 스파이럴 그루브 드라이 가스 시일의 윤활 성능해석 (Lubrication Performance Analysis of a Spiral Groove Dry Gas Seal for a High-Speed Flying Object)

  • 이안성;김준호
    • Tribology and Lubricants
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    • 제21권1호
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    • pp.8-15
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    • 2005
  • In this study a general Galerkin FE lubrication analysis method is utilized to analyze the complex lubrication performance of a spiral groove seal, which is being designed and developed for a high-speed flying object application operating at a high-speed of over 50,000 rpm. As at the equilibrium seal clearance the axial stiffness of the seal is predicted to have almost such a constant high value of $1.04\times10^8\;N/m$ regardless of a rotating speed, the seal is expected to maintain a stable thickness of lubrication film under a certain external excitation acting. Also, as even at an ultra high-speed of 80,000 rpm the axial damping of the seal is shown to have a rotatively high value of 5,775 N-s/m, the dynamic stability of the seal system at the axial degree of freedom is assured well enough.

나선홈을 갖는 반구형 공기 베어링의 반경 방향 성능 측정 (Radial Performances of Spiral-Grooved Spherical Air Bearings)

  • 박근형;최정환;최우천;김권희;우기명;김승곤
    • 한국정밀공학회지
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    • 제16권2호통권95호
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    • pp.23-30
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    • 1999
  • This paper investigates the radial performance of self-acting spiral-grooved air bearing, used to support small high-speed rotating bodies. Repeatable runout, nonrepeatable runout, stiffness and supporting load are selected as the performance. The clearance between rotor and stator, the stator groove depth, and the rotating speed are chosen as three main parameters affecting the performances. Force application and displacement measurement are done in a noncontact manner, in order not to disturb operation: electromagnetic force is applied to the rotor and gap sensors are used to measure the displacement of the rotor. Experimental results show that repeatable runout decreases as speed, groove depth and clearance decrease. Nonrepeatable runout decreases as clearance decreases, and it has a minimum value at $5.5{\mu}m$ of grove depth and a maximum value at speed of 18.000rpm. Stiffness increases as speed increases and clearance decreases, and has a maximum value around $5.5{\mu}m$ of groove depth. The relationship between force and displacement is linear for small displacement, but becomes nonlinear for large displacement. Supporting load is linearly proportional to the stiffness, and it is a maximum value around $4.75{\mu}m$ of clearance.

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마모 실 홈 형상이 펌프 성능에 미치는 영향에 관한 실험적 연구 (An experimental study on influence of wearing seal groove shape to performance of the pump)

  • 김준호
    • Journal of Advanced Marine Engineering and Technology
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    • 제38권3호
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    • pp.285-291
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    • 2014
  • 본 논문은 펌프에서 비접촉식 실로 사용되는 홈 실 적용에 의한 누설 손실을 줄임으로서 고성능 원심펌프의 효율 향상에 관한 것이다. 경사 및 평형 홈 로터와 스테이터의 조합을 포함한 홈 실 형상의 다양한 조합을 실험적으로 연구하였다. 그리고 관련해서 수력성능 및 축추력의 크기를 10가지 케이스에 대하여 측정하고 계산하였다. 그 결과로부터 로터와 스테이터 양쪽 모두에 나선 홈 실(나선 각 : $0.98^{\circ}$)을 가지는 타입이 가장 효과적임을 알 수 있었다. 이 경우 설계 유량($340m^3/h$)에서 기존 설계보다 양정과 효율은 각각 2.1%와 2.3% 향상 되었고 축추력은 10% 감소 되었다.

Recent Research and Development on Aerosol Cyclones-Review

  • Lee, K.W.;Kim, H.T.
    • Journal of Korean Society for Atmospheric Environment
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    • 제16권E호
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    • pp.59-68
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    • 2000
  • In this paper Various aerosol cyclones that are developed recently form Kwangju Institute of Science and Technology(KJIST) for increasing collection efficiency or for decreasing pressure drop are reviewed. For the first time, new sets of experimental data are reported on the particle collection efficiency of cyclones with modified surface bodies namely, spiral guide body, circumferential groove body, and vertical groove body. Multi-cylinder cyclones by adding one or two additional cylindrical walls into the conventional cyclone are also described. Ad an attempt to increase the collection efficiency of small particles, electrocyclone using an externally applied electric field was designed and operated. In addition, factors affecting the cyclone performance were studied including flowrate, body and outlet sizes, cyclone dust outlet, and gas property.

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