• 제목/요약/키워드: Vane

검색결과 785건 처리시간 0.028초

지지격자 혼합날개에 의한 $5{\times}$ 5 봉다발에서 유동 패턴 (A Study of Flow Pattern in $5{\times}5$ Rod Bundle by the Spacer Grid Mixing Vane)

  • 추연준;장석규;김복득;문상기;송철화
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2873-2878
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    • 2007
  • The mixing vanes attached to the spacer grid of rod bundles are used to improve the heat transfer in heat exchanger devices by controlling the characteristics of the flow structures and turbulence. In this study, velocity patterns induced by two types of mixing vane(split and swirl vane) are measured by the PIV technique to better understand how to effect on the cross and secondary vortex flow patterns in $5{\times}$ rod bundle simulating the fuel assembly of the nuclear reactor. A successful measurement of the lateral velocity patterns was conducted using a specially designed beam sheet generator and experimental loop at KAERI. As the result, we found that for the cross flow between subchannels, the split vane is more effective than the swirl vane, while for the secondary vortex flow in each subchannel, the swirl vane's one is larger and longer than split vane's one.

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선박용 강제통풍 팬의 기어식 베인댐퍼 성능평가 (Development of Gear-Type Vane Dampers to Replace Link-Type Vane Dampers in Marine FD Fans)

  • 허남수;장성철;이경준
    • 한국산업융합학회 논문집
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    • 제19권4호
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    • pp.216-222
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    • 2016
  • Thus, this study aimed to develop a gear-type vane damper in order to replace the link-type vane damper. To achieve this goal, the torque generated in a gear-type vane damper was analyzed, and a structural analysis was conducted. In addition, the fluid flow was analyzed according to the changes in the vane's angle, and experimental tests such as a dry-heat test and cold test were conducted considering the operating conditions of the vessels. Moreover, an appropriate actuator was selected for the developed gear-type vane damper, and studies on the reduction in the backlash due to the facing-pressure adjustment length and flow rate and leakage test due to the vane's angle were conducted.

Vane Pump의 유동 특성에 대한 수치 해석 (Numerical Analysis on Flow Characteristics of a Vane Pump)

  • 이상혁;진봉용;허남건
    • 한국유체기계학회 논문집
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    • 제10권1호
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    • pp.34-40
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    • 2007
  • In this study, the characteristic of a vane pump of automotive power steering system is numerically analyzed. The vane pump changes the energy level of operation fluid by converting mechanical input power to hydraulic output. To simulate this mechanism, moving mesh technique is adopted. As a result, the flow rate and pressure are obtained by numerical analysis. The flow rate agrees well with the experimental data. Moreover, the variation and oscillation of the pressure around the rotating vane are observed. As a result of flow characteristics, The difference of pressure between both side of vane tip causes the back flow into the rotor. As the rotational velocity increases, the flow rate at the outlet and the pressure in the vane tip rises with higher amplitude of oscillation. In order to reducing the oscillation, the design of devices for decreasing the cross-area of the outlet part and returning the flow from the outlet to the inlet is required.

Variable Geometry Mixed Flow Turbine for Turbochargers: An Experimental Study

  • Rajoo, Srithar;Martinez-Botas, Ricardo
    • International Journal of Fluid Machinery and Systems
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    • 제1권1호
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    • pp.155-168
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    • 2008
  • This paper investigates a variable geometry (VG) mixed flow turbine with a novel, purposely designed pivoting nozzle vane ring. The nozzle vane ring was matched to the 3-dimensional aspect of the mixed flow rotor leading edge with lean stacking. It was found that for a nozzle vane ring in a volute, the vane surface pressure is highly affected by the flow in the volute rather than the adjacent vane surface interactions, especially at closer nozzle positions. The performance of the VG mixed flow turbine has been evaluated experimentally in steady and unsteady flow conditions. The VG mixed flow turbine shows higher peak efficiency and swallowing capacity at various vane angle settings compared to an equivalent nozzleless turbine. Comparison with an equivalent straight vane arrangement shows a higher swallowing capacity but similar efficiencies. The VG turbine unsteady performance was found to deviate substantially from the quasi-steady assumption compared to a nozzleless turbine. This is more evident in the higher vane angle settings (smaller nozzle passage), where there are high possibility of choking during a pulse cycle. The presented steady and unsteady results are expected to be beneficial in the design of variable geometry turbochargers, especially the ones with a mixed flow turbine.

대형 트럭 코너베인 주위의 공력특성에 관한 3차원 수치해석 (Three-Dimensional Numerical Study on the Aerodynamic Characteristics around Corner Vane in Heavy-Duty Truck)

  • 김민호;정우인
    • 한국자동차공학회논문집
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    • 제8권3호
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    • pp.181-189
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    • 2000
  • The aerodynamic characteristics of large transport vehicle has become more and more important in recent vehicle design to improve driving performance in high speed cruising and raise the product valve with regard to a comfortable driving condition. Hence, detailed knowledge of the flow field around truck coner vane is essential to improve fuel efficiency and reduce the dirt contamination on vehicle body surface. In this study, three-dimensional flow characteristics around corner vane attached to truck cabin were computed for the steady, incompressible, and high speed viscous flow, adopting the RNG k-$\varepsilon$ turbulence model. In order to investigate the influence of configuration and structure of corner vane, computations were carried out for four cases at a high Reynolds number, Re=4.1$\times$106 (based on the cabin height). The global flow patterns, drag coefficient and the distributions such as velocity magnitude, turbulent kinetic energy around the corner vane, were examined. As a result of this study, we could identify the flow characteristics around corner vane for the variation of corner vane length and width. Also, suggest the improved structure to reduce the dirt contamination in cabin side.

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로켓노즐에 장착된 제트베인 표면의 열전달 특성 (Heat Transfer on a Jet Vane Surface Installed in a Rocket Nozzle)

  • 유만선;조형희;황기영;배주찬
    • 한국추진공학회지
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    • 제9권1호
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    • pp.9-16
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    • 2005
  • 제트베인은 로켓추진기관의 발사초기 자세제어와 조정 안정성의 확보를 위해 로켓노즐 출구부에 장착되어지며, 발사 수초 후까지 연소가스와의 접촉으로 인해 구동부를 가열시키고, 그 자체도 화학적 혹은 기계적으로 삭마된다. 본 연구는 제트베인의 열해석을 위한 기초연구로서 균일 초음속 유동장내에 위치한 단일 제트베인으로의 열전달 특성 해석을 수행하여 보았다. 경계층 적분법과 유한차분법의 연립해석이 이루어 졌으며, 벽근방에서 도출된 경계조건을 바탕으로 베인 내부의 비정상 열전도 해석도 수행되었다.

Vane 방법을 이용한 고추장의 항복응력 측정 (Yield Stress of Kochujang with Vane Method)

  • 장윤혁;유병승
    • 한국식품과학회지
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    • 제32권4호
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    • pp.974-978
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    • 2000
  • 다섯 종류의 시판 고추장에 대한 항복응력은 vane 방법에 의해 controlled shear-rate 조건에서 측정되었다. Vane 항복응력은 전단속도와 전단응력 데이터의 외삽법(extrapolation)에 의해 결정된 Casson 항복응력 보다 높은 수치를 보여주었다. 고추장의 구조가 손상되지 않은 시료와 이미 손상된 시료에 대해 vane 방법에 의해 정적항복응력$({\sigma}_s)$과 동적항복음력$({\sigma}_d)$이 각각 측정되었으며 큰 수치 차이로부터 고추장에 대한 구조파괴 정도를 결정하는 데 있어 vane 방법이 적합함을 알 수 있었다. ${\sigma}_{ov}({\sigma}_{s},\;{\sigma}_{d})$${\sigma}_{oc}$ 수치 사이에는 좋은 상관관계를 보여주고 있으며 ${\sigma}_{d}$ 수치는 외삽법에 의해 얻어진 ${\sigma}_{oc}$ 수치와 잘 일치함을 나타냈다. ${\sigma}_{s}$${\sigma}_{d}$의 비율로부터 얻어진 무차원 yield number$(N{\sigma}_{o})$는 고추장의 일시적 구조 존재여부를 결정하는데 사용될 수 있다. $N{\sigma}_{o}$로부터 계산된 fator ${\varepsilon}$의 수치$({\varepsilon}=0.100-0.169)$로부터 고추장은 강한 결착구조를 형성하고 있는 분산식품임을 알 수 있었다.

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Application and optimal design of the bionic guide vane to improve the safety serve performances of the reactor coolant pump

  • Liu, Haoran;Wang, Xiaofang;Lu, Yeming;Yan, Yongqi;Zhao, Wei;Wu, Xiaocui;Zhang, Zhigang
    • Nuclear Engineering and Technology
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    • 제54권7호
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    • pp.2491-2509
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    • 2022
  • As an important device in the nuclear island, the nuclear coolant pump can continuously provide power for medium circulation. The vane is one of the stationary parts in the nuclear coolant pump, which is installed between the impeller and the casing. The shape of the vane plays a significant role in the pump's overall performance and stability which are the important indicators during the safety serve process. Hence, the bionic concept is firstly applied into the design process of the vane to improve the performance of the nuclear coolant pump. Taking the scaled high-performance hydraulic model (on a scale of 1:2.5) of the coolant pump as the reference, a united bionic design approach is proposed for the unique structure of the guide vane of the nuclear coolant pump. Then, a new optimization design platform is established to output the optimal bionic vane. Finally, the comparative results and the corresponding mechanism are analyzed. The conclusions can be gotten as: (1) four parameters are introduced to configure the shape of the bionic blade, the significance of each parameter is herein demonstrated; (2) the optimal bionic vane is successfully obtained by the optimization design platform, the efficiency performance and the head performance of which can be improved by 1.6% and 1.27% respectively; (3) when compared to the original vane, the optimized bionic vane can improve the inner flow characteristics, namely, it can reduce the flow loss and decrease the pressure pulsation amplitude; (4) through the mechanism analysis, it can be found out that the bionic structure can induce the spanwise velocity and the vortices, which can reduce drag and suppress the boundary layer separation.

입구 안내익 영향으로 인한 원심 압축기 불안정성 연구 (Experimental Study on the Effect of Inlet Guide Vane of Instabilities of a Centrifugal Compressor)

  • 임병준;차봉준
    • 한국유체기계학회 논문집
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    • 제7권3호
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    • pp.23-31
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    • 2004
  • An experimental study on the performance and instability development characteristics of a centrifugal compressor equipped with an adjustable inlet guide vane has been performed with varying guide vane angles. The test was conducted at the design speed of 20,800 rpm for 6 guide vane angles : $-30^{\circ},\;-20^{\circ},\;10^{\circ},\;0^{\circ},\;10^{\circ},\;20^{\circ},\;30^{\circ}$. Unsteady pressures were measured using high-frequency pressure transducers at the inducer to investigate the instability phenomena such as rotating stall and surge inside the compressor. From the unsteady measurements, it is found that the transient process from rotating stall to surge was mainly affected by inlet guide vane angles. The results of the present study can be applied to the instability control of the centrifugal compressors using a adjustable inlet guide vane.

보일러 압입통풍기용 인버터 적용기술 (The Application of Variable Frequency Drive for Forced Draft Fan)

  • 임익헌;김봉석;류호선;이주현;황영하
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2006년도 추계학술대회 논문집 전기기기 및 에너지변환시스템부문
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    • pp.185-187
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    • 2006
  • 본 논문에서는 평택화력 제2호기 FDF(Forced Draft Fan : 압입송풍기, 이하 FDF) 출구의 공기량제어를 Vane Control 시스템으로 구성되어 있는 것을 구동 유도전동기에 가변속 제어시스템(이하 VFD: Variable Frequency Drive)으로 교체하여 발생한 실험결과를 보여준다. VFD는 Vane을 전개(全開)하고 전동기 속도를 변경시켜 연소에 필요한 노내 공기량을 제어하는 방식이다. VFD 운전은 정속도 Vane 개도 운전에 비해 Throttle Loss를 최소화해서 에너지 절감효과는 크지만 간단한 Vane 제어기에 비해 복잡한 전력전자제어시스템이 어우러진 기기로 신뢰도는 떨어지는 것이 사실이다. 따라서 고도의 신뢰성이 요구되는 전력생산 보일러에서 후비보호책으로 VFD 고장 시에 Vane제어 모드로 절환은 필연적으로 필요한 설비이다. VFD에서 Vane으로 절환 시에 일어나는 과도상태를 최소화하기 위해서는 보일러 연소제어 알고리즘의 최적화가 필요하다. 본 논문에서는 구현된 제어알고리즘을 정리한 것이다.

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