• 제목/요약/키워드: Co-axial Rotor

검색결과 18건 처리시간 0.023초

선박용 송풍기의 날개 끝 간격과 정익이 성능에 미치는 영향에 대한 전산 유체 해석 (Computational and Experimental Study of Effects of Guide Vanes and Tip Clearances on Performances of Axial flow Fans)

  • 이승수;김학선;남광현;홍재익;천승현
    • 대한조선학회논문집
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    • 제41권6호
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    • pp.24-32
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    • 2004
  • The effects of guide vanes and tip clearances on the characteristics nf axial flow fans are investigated both computationally and experimentally. Performance test of fans carried out in full scale shows considerable effects of tip clearance between rotor tip and duct on the characteristics of fans. The tested results are compared with the computation based on the finite volume method to solve the Navier-Stoke equations with $textsc{k}$-$\varepsilon$ turbulence model. The comparison shows good agreements between experimental and computational results. In addition, the effects of shape of guide vanes are numerically studied. The results show that increased volume of separated region around the guide vane reduces the recovery of tangential component of kinetic energy in the wake, resulting in loss of efficiency

다단 축류 터빈에서의 초킹 영역 탈설계 성능 해석을 위한 평균반경 해석법 (Meanline Analysis Method for Performance Analysis of a Multi-stage Axial Turbine in Choking Region)

  • 김상조
    • 한국추진공학회지
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    • 제22권2호
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    • pp.20-28
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    • 2018
  • 일반적으로 다단 축류 터빈은 높은 팽창비에서 유동 가속으로 인하여 특정 단에서 초킹 현상이 발생하게 된다. 입구 유량 경계조건을 사용하는 일반적인 평균반경해석법을 사용하는 경우 유량 변화없이 팽창비만 증가하게 되는 초킹 현상을 예측하는데 한계가 있다. 본 연구에서는 이러한 문제점을 해결하기 위해 초킹 영역에서의 성능을 예측하는 알고리즘을 제안하였다. 초킹 지점 이후에는 초킹이 발생하는 노즐 혹은 로터 출구 유동이 팽창하는 특성을 반영하여 고정된 유량 조건에서 팽창비가 변할 수 있도록 알고리즘을 구성하였다. 계산된 결과를 다단 축류 터빈 전산해석 결과 및 실험결과와 비교하여 신뢰성을 확인하였다.

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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Disk형 단상 SRM의 기본 특성 해석을 위한 자화곡선 측정 (Magnetization Curves Measurement for Fundamental Characteristics Analysis of Disk-type Single Phase SRM)

  • 이충원;이종한;이은웅;오영웅
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2003년도 춘계학술대회 논문집 전기기기 및 에너지변환시스템부문
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    • pp.91-93
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    • 2003
  • Disk type Single Phase SRM(Switched Reluctance Motor) can be used axial direction magnetic flux and radial direction magnetic flux. In this paper, the flux linkage was measured according as rotor positions of disk-tyre single phase SRM, which is designed and manufactured in previous research. From the measured data, we got the magnetization curves, inductance profile and Co-energy.

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Disk형 단상 스위치드 리럭턴스 전동기의 특성 해석 (Characteristics Analysis of Disk-type Single Phase SRM)

  • 이충원;이은웅;이종한;오영웅
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2003년도 하계학술대회 논문집 B
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    • pp.988-990
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    • 2003
  • Disk type Single Phase SRM(Switched Reluctance Motor) can be used axial and radial direction magnetic flux. Therefore, the energy density per unit of volume is high and the axis can be shorter than that of any other motor. In this paper, the flux-linkage was measured according as rotor positions of disk type single phase SRM, which is designed and fabricated in previous studies. From the measured data, we got the magnetization curves, inductance profile, co-energy and torque. Also, we compared the value of the measurement with the value of analysis through 3D FEM simulation.

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STATE OF ART OF SELFBEARING MOTOR

  • Okada, Yohji;Ueno, Satoshi;Ohishi, Tetsuo
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1997년도 추계학술대회논문집; 한국과학기술회관; 6 Nov. 1997
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    • pp.20-25
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    • 1997
  • Magnetic bearings have been widely used to support rotors without any physical contact. This however, requires the control of five degrees-of-freedom and needs a separate driving motor. This paper introduces selfbearing motors which use the combination of a rotary motor and a magnetic bearing. These motors are suitable for use in high speed rotor or in special circumstances because they are small in size and can replace the contact components. The radial type one has the merit of being small in size and capable of controlling two degrees-of-freedom in x and y directions. The axial type motor controls only one degree-of-freedom in z direction. Theoretical background of the functions, of the motor and magnetic bearing will also be introduced. New research works are reviewed and the application in rotary blood pump is discussed.

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부분 유입 노즐을 적용한 초임계 이산화탄소 발전용 초고속 터보발전기 개발 연구 (Research on Development of Turbo-generator with Partial Admission Nozzle for Supercritical CO2 Power Generation)

  • 조준현;신형기;강영석;김병휘;이길봉;백영진
    • 대한기계학회논문집B
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    • 제41권4호
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    • pp.293-301
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    • 2017
  • 초임계 이산화탄소 발전사이클의 다양한 특성을 분석하기 위하여 Sub-kWe급의 소형 실험장치를 설계, 제작하였으며, 터보발전기를 개발하였다. 초임계 이산화탄소 발전용 터빈에서는 팽창비가 작고, 유량이 작기 때문에 터보발전기의 회전수가 높아지게 되고, 이에 따라 회전 부품의 선정, 터빈 공력설계, 축력 및 회전체 동역학 설계가 어려워지게 된다. 이에 터보발전기의 회전수를 줄이기 위하여 노즐의 여러 채널 중 1개의 노즐만 사용하는 부분유입 방법을 세계 최초로 초임계 이산화탄소 발전용 터보발전기에 적용하였으며, 회전체의 진동을 측정하여 부분유입 노즐을 적용함에도 회전체 안정성은 허용 범위내에 있음을 확인하였다.

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.