• Title/Summary/Keyword: rotating mesh

검색결과 83건 처리시간 0.026초

2축 스크류 니더의 설계에서 스크류 로터 팁의 각도가 믹싱성능에 미치는 영향 (Influence of Screw Rotors Tip Angle on Mixing Performance for One Novel Twin-screw Kneader)

  • Wei, Jing;Chen, Dabing;Zhou, Dongming;Zhang, Aiqiang;Yang, Yuliang
    • 폴리머
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    • 제39권3호
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    • pp.441-452
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    • 2015
  • Twin-screw kneader is an efficient polymer processing equipment. In this paper, the mixing performance of one novel intermeshing counter-rotating twin-screw kneader with different tip angles of the male rotor is simulated using the mesh superimposition technique (MST). Statistical analysis is carried out for the flow field using particle tracking technique, and distributive mixing performance is evaluated using the residence time distribution and segregation scale, while the dispersive mixing performance is estimated using the parameters such as shear rate, stretching rate and mixing index. The results show that the best distributive mixing performance is achieved when the tip angle is 0o, while the optimal dispersive mixing performance is obtained when the tip angle is 20o. The results in this paper provide a data basis for the selection of parameters and optimization of the performance for the screw rotors.

원자력 발전소용 순환수 펌프의 성능해석 (THE PERFORMANCE ANALYSIS OF A CWP PUMP FOR A NUCLEAR POWER PLANT)

  • 이명수;한병윤;황도연;유성수;박형구
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2009년 춘계학술대회논문집
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    • pp.232-238
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    • 2009
  • The objective of this study is to investigate the suitable design for a domestic CWP pump, which is used in cooling-water intakes for the unit 3 and 4 of Yeonggwang nuclear power plant. All the simulations are performed, using CFD method with a commercial code STAR-CCM+ version 3.02. After modeling a present design of the pump, the flow around the rotating blade was calculated by using quasi-static method and sliding mesh method with the almost same condition as an actual state. Based on fundamental simulations with various depth of sea water, the reference pressure for the boundary condition of the present study was decided. To verify the reliability of the calculation results, the suction flow rate of the data was compared with that of the experimental data. As a result of this comparison, it is confirmed that two results are fairly consistent. For the improvement of the suction flow rate, computational analysis was done by changing a flow channel and blade shapes. It is shown that the suction flow rate of the new pump was improved.

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롤타입 마스크를 이용한 연속 포토리소그래피 기술과 그 응용 (Continuous Photolithography by Roll-Type Mask and Applications)

  • 곽문규
    • 대한기계학회논문집B
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    • 제36권10호
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    • pp.1011-1017
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    • 2012
  • 본 논문에서는 롤타입 마스크를 사용한 마이크로/나노 구조 제작용 광학 리소그래피 방법을 소개한다. 이 생산 방법은 다양한 목표 해상도에 따라 위상지연 리소그래피방법과 포토리소그래피로 나뉜다. 사용되는 빛의 파장대보다 작은 해상도를 갖는 패턴을 제작하기 위해서 실린더 형태의 위상지연 마스크를 활용한 근거리 노광 방식을 사용한다. 또한 필름 형태의 금속 마스크를 써서 포토리소그래피를 연속방식으로 수행하였는데 이 방식은 실린더 마스크의 회전수를 조절함으로써 노광 결과 패턴의 주기를 실시간으로 조절할 수 있다. 이 기술의 응용으로 금속 그물패턴으로 만들어진 100 $mm^2$ 넓이의 투명전극을 제작하였다.

틸트로터 항공기의 탑재장비 상세 지지구조 형상을 고려한 전산진동해석 및 평가 (Computational Vibration Analysis and Evaluation of a Tilt-Rotor Aircraft Considering Equipment Supporting Structures)

  • 김유성;김동만;양건명;이정진;김동현
    • 한국항공운항학회지
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    • 제15권4호
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    • pp.24-32
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    • 2007
  • In this study, computational structural vibration analyses of a smart unmanned aerial vehicle (SUAV) with tilt-rotors due to dynamic hub loads have been conducted considering detailed supporting structures of installed equipments. Three-dimensional dynamic finite element model has been constructed for different fuel conditions and tilting angles corresponding to helicopter, transition and airplane flight modes. Practical computational procedure for modal transient response analysis is successfully established. Also, dynamic loads generated by rotating blades and wakes in the transient and forward flight conditions are calculated by unsteady computational fluid dynamics technique with sliding mesh concept. As the results of present study, transient structural displacements and accelerations of the vibration sensitive equipments are presented in detail. In addition, vibration characteristics of structures and installed equipments of which safe operation is normally limited by the vibration environment specifications are physically investigated for different flight conditions.

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수치해석을 이용한 FPSO용 사류펌프 성능해석 연구 (A Numerical Study on the Performance Analysis of the Mixed Flow Pump for FPSO)

  • 강경원;김영훈;김영주;우남섭;권재기;윤명오
    • 한국유체기계학회 논문집
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    • 제14권5호
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    • pp.12-17
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    • 2011
  • The seawater lift pump system is responsible for maintaining the open canal level to provide the suction flow of circulating water pump at the set point. The objective of this paper is to design a 2-stage mixed flow pump (for seawater lifting) by inverse design method and to evaluate the overall performance and the local flow fields of the pump by using a commercial CFD code. Rotating speed of the impeller is 1,750 rpm with the flow rate of 2,700 $m^3$/h. Finite volume method with structured mesh and realized k-${\varepsilon}$ turbulent model is used to guaranty more accurate prediction of turbulent flow in the pump impeller. The numerical results such as static head, brake horse power and efficiency of the mixed flow pump are compared with the design data. The simulated results are good agreement with the design data less 3% error.

2단 사류펌프의 임펠러 성능향상 방안 연구 (STUDY ON THE HYDRAULIC DESIGN OF 2 STAGE MIXED FLOW PUMP)

  • 김영주;우남섭;권재기;정소걸;박의섭;배상은;박수한
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.556-560
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    • 2011
  • The seawater lift pump system is responsible for maintaining the open canal level to provide the suction flow of circulating water pump at the set point. The objective of this paper is to design a 2-stage mixed flow pump(for seawater lifting) by inverse design and to evaluate the overall performance and the local flow fields of the pump by using a commercial CFD code. Rotating speed of the impeller is 1,750 rpm with the flow rate of 2,700 $m^3/h$. Finite volume method with structured mesh and Realizable ${\kappa}-{\varepsilon}$ turbulent model is used to guaranty more accurate prediction of turbulent flow in the pump impeller. The numerical results such as static head brake horse power and efficiency of the mixed flow pump are compared with the reference data. Also, the periodic condition calculation method for the mixed flow pump was carried out in order to investigate the pump performance characteristics with the modification of impeller geometry.

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원자력 발전소용 순환수 펌프의 성능해석 (THE PERFORMANCE ANALYSIS OF A CIRCULATING WATER PUMP FOR A NUCLEAR POWER PLANT)

  • 이명수;한병윤;황도연;유성수;박형구
    • 한국전산유체공학회지
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    • 제14권3호
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    • pp.69-75
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    • 2009
  • The objective of this study is to investigate the suitable design for a domestic Circulating water pump(CWP), which is used in cooling-water intakes for the unit 3 and 4 of Yeonggwang nuclear power plant. All the simulations are performed, using CFD method with a commercial code STAR-CCM+ version 3.02. After modeling a present design of the pump, the flow around the rotating blade was calculated by using quasi-static method and sliding mesh method with the almost same condition as an actual state. Based on fundamental simulations with various depth of sea water, the reference pressure for the boundary condition of the present study was decided. To verify the reliability of the calculation results, the suction flow rate of the data was compared with that of the experimental data. As a result of this comparison, it is confirmed that two results are fairly consistent. For the improvement of the suction flow rate, computational analysis was done by changing a flow channel and blade shapes. It is shown that the suction flow rate of the new pump was improved.

진공청소기 흡입효율 개선을 위한 모터 주위의 유동해석 (Performance Improvement of a Vacuum Cleaner by CFD Analysis around Motor)

  • 박진우;기민철;박형구
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.522-525
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    • 2008
  • A vacuum cleaner is the widely used home equipment. However, it has a trouble with too much power consumption. Most losses occur at the centrifugal fan. To remedy this trouble the investigation of motor, which is the main component of vacuum cleaner, is required. The flow characteristics around the high-speed rotating centrifugal fan which is influenced by the very low inlet pressure is quite different from a commonly used fan. Hence it is quite difficult to analyze the flow by the experimental means or by the numerical simulation. In this research, it is aimed to improve the air-suction performance of a vacuum cleaner through the flow analysis around a motor. The efficiency of the centrifugal fan is affected by blade shape, blade number, blade pitch, etc. The influence of the shape of impeller on the flow is investigated in this study. The flow around the centrifugal fan is simulated by applying the moving mesh. To verify the validity of the computation results, the air flow rate and the pressure field to the cleaner is compared with the experimental data. All simulations are performed by using commercial code SC/Tetra. The calculated results show good agreement with the experimental ones and it is believed to be promising to use computational simulation in the improvement of the vacuum cleaner performance.

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정지비행 로터 블레이드에 부착된 탭의 공기역학적 효과 (AERODYNAMIC EFFECTS OF THE TAB ON A HOVERING ROTOR BLADE)

  • 강희정;김도형;김승호
    • 한국전산유체공학회지
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    • 제18권3호
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    • pp.60-66
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    • 2013
  • Numerical simulation was performed for the rotor blade with fixed tab in hover using an unstructured mesh Navier-Stokes flow solver. The inflow and outflow boundary conditions using 1D momentum and 3D sink theory were applied to reduce computational time. Calculations were performed at several operating conditions of varying collective pitch angle and fixed tab length. The aerodynamic effect of fixed tab length was investigated for hovering efficiency, pitching moment and flapping moment of the rotor blade. The results show that it affects linearly increasing on the pitching moment of the rotor blade but does not affect on the flapping moment. The required power is less than 45kw for ground rotating test in hover. Numerical simulations also show that the vortex generate not only from the tip of the rotor blade but also from the fixed tab on the rotor blade.

중형 컨테이너선의 연료절감형 비틀림 타 개발 (Development of Twisted Rudder to Reduce Fuel Oil Consumption for Medium Size Container Ship)

  • 전호환;차경정;이인원;최정은
    • 대한조선학회논문집
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    • 제55권2호
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    • pp.169-177
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    • 2018
  • Twisted rudder, twisted rudder with bulb, and twisted rudder with bulb and fin have been developed computationally for 3,000 TEU container ship through parametric study. The objective function is to minimize delivered power in model scale. Design variables are twisted angle, rudder bulb diameter and fin angle. The governing equation is Reynolds averaged Navier-Stokes equations in an unsteady turbulent flow and the Reynolds stress model applied for the turbulent closure. A double body model is used for the treatment of free-surface. The calculation was carried out in towing and self-propulsion conditions at design speed. The sliding mesh technique was employed to simulate the flow around the propeller. Form factor is obtained from the towing computation. Self-propulsion point is obtained from the self-propelled computations at two propeller rotating speeds. The delivered power due to the designed twisted rudder, twisted rudder with bulb, and twisted rudder with bulb and fin are reduced by 1.1%, 1.6%, and 2.0%, respectively.