• 설비공학논문집
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• 제19권9호
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• pp.669-678
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• 2007

In this study, the ventilation characteristics is investigated numerically of the longitudinal ventilation method in the curved long road tunnel. Numerical work has been conducted for the jet fan location by utilizing the commercial finite-volume code, FLUENT. Configuration of the tunnel is three-lane, 1600 m long, $120m^2$ in area, 3000 m curvature radius. The velocity profile, distribution of mono-dioxide carbon and flow rate of air are examined in the tunnel. Through the analysis, it is found that the difference of ventilation flow rate Is a little by the jet fan location, but tunnel outlet setup (CASEIII) of jet fans is the most efficient concerned with CO concentration.

• 터널과지하공간
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• 제12권2호
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• pp.92-98
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• 2002

본 연구에서는 제트팬이 설치된 터널에서 화재발생시 연기의 거동을 해석하기 위하여 축소실험을 실시하였다. Froude 상사를 사용하여 1/20로 축소된 모형터널에서 실험을 실시하였으며 가연물질로는 휘발유를 사용하였다. 지름이 6.6∼ 12.5 cm의 화원을 사용하였으며 발열량은 7.714∼4.77 kW이다. 2.5 kW이하의 화재시 팬을 가동함으로 인하여 역기류가 팬 상류 약 40cm 이상 감소하였으며 팬 하류에서는 효과적으로 연기를 제어하였다. 팬 상류에서는 팬을 가동하지 않은 경우에 비해 연층은 하강하고 온도는 감소하였으나 터널 하부에서는 온도가 증가하였다.

• 한국방재안전학회논문집
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• 제12권2호
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• pp.47-56
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• 2019

주차장 화재 시 다량의 연기 발생으로 소방대원이 화점에 진입하기 곤란한 문제점을 극복하고자 최근 주차장 환기 목적으로 설치된 급 배기팬과 유인팬(Jet fan)을 이용하여 연기를 배출하는 방법을 이용하고 있다. 본 연구에서는 급배기팬만 동작하는 조건과 유인팬이 함께 동작하는 2가지 조건에서 연기층의 유동변화를 CCTV를 이용하여 관찰하였으며, 또한 hot smoke test가 주차장 환기 성능평가 방법으로서의 적정성을 평가하기 위해 플럼 주위의 온도를 Alpert eq.과 비교 분석하였다. 그 결과 jet fan을 동시에 동작시키는 경우 연기층이 교란될 수 있음을 확인할 수 있었으며, 그로인하여 초기 피난 장애 우려가 있을 것을 것으로 분석되었다. 다만, jet fan이 추가로 작동됨에 따라 배기성능은 향상되는 것을 관찰용 CCTV로 확인할 수 있었으며, 이는 진압전술을 펴는데 도움이 될 것으로 판단된다. 플럼 주변의 온도를 측정하여 Alpert eq과 비교한 결과 Plume 중심축에서 약 $2^{\circ}C$ 낮고 연기가 배출되는 방향으로 8 m에서는 $9.0^{\circ}C$ 높은 것으로 분석되었다. Plume 주변의 온도 측정 결과는 AS 4391-1999의 예상 최대 온도보다 낮았고 실험으로 인한 예상 온도 위험을 초과하지 않았다. 이 결과와 같이 고온 연기 시험의 진행으로 인한 온도 위험성이 예측 가능하기 때문에 관련 기준이 없는 주차장의 연기 제어 성능 평가를 위한 일반적인 평가 방법 중 하나로 활용 가능할 것이다.

• 한국추진공학회지
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• 제21권6호
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• pp.83-90
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• 2017

복합형 로터항공기의 터보샤프트 엔진에 대한 성능해석을 수행하였다. 복합형 로터항공기의 개념으로 팁제트 방식과 덕티드팬 방식의 형태를 이용하였다. 터보샤프트엔진에 대한 성능해석은 Gasturb 12 소프트웨어를 이용하여 수행하였다. 팁제트 방식의 항공기는 주어진 임무조건에서 최대출력 약 1,600 hp 대가 요구되며, 덕티드팬은 설계점에서 약 1,000 hp 대의 출력이 요구된다. 이것은 팁제트의 경우 제자리비행 시 부가적인 보조압축기 구동이 필요하며, 동력장치에 높은 출력을 요구하고 있기 때문인 것으로 파악된다. 또한 연료소모량의 경우 팁제트 방식이 덕티드팬에 비해 약 2.8배정도 소모되어 연료 효율 측면에서 덕티드팬 방식의 항공기가 보다 우수한 특성이 있음을 알 수 있다.

• 한국전산유체공학회지
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• 제11권4호
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• pp.20-25
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• 2006

In the present study, flow characteristics inside a road tunnel are simulated for the ventilation flows due to jet fan system and flows induces by the traffic. Traffic ventilation is numerically simulated by multiple reference frame. From the results of steady state simulation of tunnel ventilation, it is found that the proper ventilation is achieved by the designed jet fan system along with ventilating flow induced by the traffic. A transient simulation is also performed for the case of vehicle fire in the tunnel reversing the direction of rotation of some fans. The results suggest that the heat and smoke can be controlled by the proper changing of fan operation mode. The present results can be used to design proper ventilation system and effective smoke control system as well.

• 천문학회보
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• 제45권1호
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• pp.45.1-45.1
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• 2020

Light bridges (LBs) are relatively bright structures that divide sunspot umbrae into two or more parts. Chromospheric LBs are known to be associated with various activities including fan-shaped jet-like ejections and brightenings. Although magnetic reconnection is frequently suggested to be responsible for such activities, not many studies presented firm evidence to support the scenario. We carry out magnetic field measurements and imaging spectroscopy of a LB where fan-shaped jet-like ejections occur with co-spatial brightenings at their footpoints. We study their fine photospheric structures and magnetic field changes using TiO images, Near-InfraRed Imaging Spectropolarimeter data, and Hα data taken by the 1.6 m Goode Solar Telescope. As a result, we detect magnetic flux emergence in the LB that is of opposite polarity to that of the sunspot. The new flux cancels with the pre-existing flux at a rate of 5.6×1018 Mx hr-1. Both recurrent jet-like ejections and their footpoint brightenings are initiated at the vicinity of the magnetic cancellation, and show apparent horizontal extension along the LB at a projected speed of 4.3 km s-1 to form the fan-shaped appearance. Based on these observations, we suggest that the fan-shaped ejections may have resulted due to slipping reconnection between the new flux emerging in the LB and the ambient sunspot field.

• 한국유체기계학회 논문집
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• 제8권5호
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• pp.29-34
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• 2005

In this study, the effect of flow settling means on the performance of fan tester were numerically investigated by using a computational fluid dynamics (CFD). The airflow rate was calculated from the pressure differential across a flow nozzle in the measuring plane and the flow settling means were generally installed in the chamber of the fan tester to provide proper airflow patterns ahead of the measuring plane. The predicted nozzle differential pressures with uniform inlet velocities were compared with the values of the ANSI/AMCA 210-99 to verify the performance of the commercial CFD code CFX 5.6. The influence of flow settling means on the measurement of airflow rate in a fan tester were discussed with various porosities and inlet jet velocities. The results obtained show that the proper band of porosities exist to meet the AMCA standard in a specified inlet jet velocity.

• 한국유체기계학회 논문집
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• 제9권4호
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• pp.43-48
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• 2006

In this study, the effect of flow settling means on the performance of fan tester were numerically investigated by using a computational fluid dynamics(CFD). The airflow rate was calculated from the pressure differential across a flow nozzle in the measuring plane and the flow settling means were generally installed in the chamber of the fan tester to provide proper airflow patterns ahead of the measuring plane. The predicted nozzle differential pressures with uniform inlet velocities were compared with the values of the ANSI/AMCA 210-99 to verify the performance of the commercial CFD code CFX 5.6. The influence of flow settling means on the measurement of airflow rate in a fan tester were discussed with various porosities and inlet jet velocities. The results obtained show that the proper band of porosities exist to meet the AMCA standard in a specified inlet jet velocity.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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• pp.439-443
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• 2002

In this study, three-dimensional incompressible viscous flow analysis and optimization using response surface method are presented for the design of a jet fan. Steady, incompressible, three-dimensional Reynolds averaged Wavier-Stokes equations are used as governing equations, and standard k-$\epsilon$ turbulence model is chosen as a turbulence model. Governing equations are discretized using finite volume method. Sweep angles and maximum thickness of blade are used as design variables for the shape optimization of the impeller in response surface method. The experimental points which are needed to construct response surface are obtained from the D-optimal design and Full Factorial design and relations between design variables and response surface are examined.

• 대한기계학회논문집B
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• 제30권8호
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• pp.715-721
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• 2006

In the present work, nozzle shape of a jet fan is optimized numerically using three-dimensional Reynolds-averaged Navier-Stokes analysis. Standard $k-{\epsilon}$ model is used as a turbulence closure. Response surface method is employed as an optimization technique. The objective function is defined as maximum throw distance. Three geometric variables, i.e., length and angle of nozzle, and interval between two nozzles, are selected as design variables. As the main result of the optimization, the throw distance has been improved effectively.