• 한국음향학회지
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• 제39권6호
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• pp.515-523
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• 2020

본 연구의 목표는 냉장고 기계실 냉각용 축류팬을 대상으로 익렬 분석법과 표면 돌기 형상을 이용하여 유량과 소음 성능을 향상시키는 것이다. 먼저 기존 팬 시스템의 유동 및 소음 성능을 팬 성능 시험기와 무향실에서 실험적으로 평가하였다. 다음으로 전산유체역학과 Ffowcs-Williams and Hawkings(FW-H) 방정식을 연계한 수치해석을 이용하여 유량과 소음 성능을 예측하였으며 실험 결과와의 비교를 통해 그 유효성을 검증하였다. 검증된 수치해석기법을 기반으로 유량 성능을 향상시키기 위하여 기존 팬으로부터 추출된 익형들로 구성한 2차원 익렬의 유동 성능 분석을 수행하고 양항비를 최대화할 수 있는 피치각을 도출하였다. 최적 피치각이 적용된 축류팬의 수치해석을 실시하여 향상된 유량 성능을 확인하였다. 향상된 유량 성능을 바탕으로 추가적인 소음 성능을 개선하기 위해 표면 돌기 형상을 팬 압력면에 적용한 팬 날개를 도출하였으며 수치적으로 유동 소음의 저감을 확인하였다. 마지막으로 유량 및 소음 성능 개선 축류팬을 제작하여 검증 실험을 통해 유량 및 소음 성능이 향상됨을 확인하였다.

• 한국산학기술학회논문지
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• 제18권4호
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• pp.527-535
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• 2017

연료전지 배터리 하이브리드 UPS용 연료전지 파워 팩 내부에 설치한 연료전지의 화학반응에 의해 생성되는 열을 제거하는데 어려움이 있다. 열을 제거하지 못할 경우 연료전지의 내구성과 성능에 영향을 끼쳐 수명 단축의 원인이 된다. UPS용 연료전지 파워 팩 제작을 위하여 연료전지의 적절한 냉각 방법을 선정하고 제시하는 것이 본 연구의 목표이다. 냉각방법 선정을 위해 냉각 성능에 영향을 주는 각각의 설계 인자를 변화시키면서 연구를 수행하였다. 전산해석은 상용프로그램인 COMSOL Multiphysics로 수행하였다. 먼저 연료전지 스택의 냉각 팬의 위치를 상단과 하단에 배치했을 때 1 kW급 연료전지 스택 표면온도를 비교하였으며, 각각의 위치에 따른 냉각 팬의 회전속도를 2,500, 3,000, 3,500, 4,000 RPM으로 변경하여 적절한 냉각 팬의 속도를 결정하였다. 또한 파워 팩 외부에서 내부로 들어오는 공기의 입구인 그릴의 타공면적을 달리하여 내부로 들어오는 공기의 유량이 냉각에 미치는 영향을 비교하였다. 본 연구는 UPS용 연료전지 파워 팩 내부 연료전지의 열관리 기술개발에 효과적으로 활용될 수 있을 것으로 판단된다.

• 한국정밀공학회지
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• 제22권4호
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• pp.151-158
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• 2005

An important component of a cooling tower is an axial fan, and there happens distortion in its shape which brings significant loss of efficiency. In this paper, a surface profile measuring system for large size axial fan of cooling towers is developed. A laser sensor is used as a measuring device and aluminum profiles and stepping motors are engaged into the system as frame structure and driving devices respectively. The measuring data are compared to the design data to compute the distortion of the axial fans. Two types of errors, axial and twist errors, are used to represent the precision of axial fan distortion. Genetic algorithm is used to solve the optimization problem during computing the precision. Results are displayed three dimensionally in a solid-modeler as well as 2-D drawings to help users find it with ease.

• 한국항공운항학회지
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• 제14권1호
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• pp.15-21
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• 2006

Parametric cycle analysis of a dual-spool, mixed exhaust turbofan engine with turbine blade cooling were described to investigate the effect of turbine blade cooling on the engine performance such as specific thrust and thrust specific fuel consumption. Coolant of low pressure turbine triggers high engine performance loss and cooling effect loss in high pressure turbine. Therefore low pressure turbine coolant should be much more considered for effective design.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2008년도 추계학술대회논문집
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• pp.608-609
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• 2008

An alternator which converts mechanical rotating energy into electric energy is an important component of a vehicle. It operates in broad range from 3000 RPM to 18000 RPM. So, sufficient flow rate and low noise are needed in such broad operating range for a cooling fan of this alternator. In current study, the cooling fan of an alternator is developed through DFSS process and numerical analysis. In order to calculate flow rate and noise level, SC/Tetra and FlowNoise S/W are used respectively, for a new developed fan, compared with original model, numerical result shows 3 dBA reduction and measured value shows 4 dBA reduction.

• 한국공작기계학회논문집
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• 제12권1호
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• pp.50-57
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• 2003

In this paper, an automated design and 3-D modeling system of an axial fan and a boss for cooling towers was developed. API and parametric design Provided by a commercial solid-modeler are engaged to automate modeling process. Design data of the boss are assumed to be given by a user with design experiences while the fan from the fan design program using three-dimensional flow analysis. An algorithm avoiding the interferences between fans and a boss is developed. The design data are registered on the database not only to remove duplicate design but also to transfer the data to ERP system.

• 설비공학논문집
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• 제19권10호
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• pp.735-741
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• 2007

An axial F.R.P. fan model for cooling tower is developed. The fan is designed using the equations for one dimensional inviscid flow through the fan blade. Fan shape is swept forward with a parabolic function. Calculations of the three dimensional turbulent flow around the fan are carried out to investigate performance of the fan. Data of the total pressure rise and hydraulic efficiency can be obtained for the various setting angles. Calculated values of the total pressure rise and hydraulic efficiency at the design point are less than those of the design specification. The prototype of the F.R.P. fan is made by laminating of the fiberglass and epoxy resins on the mold of fan shape.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 학술대회
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• pp.233-238
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• 2008

An alternator which converts mechanical rotating energy into electric energy is an important component of a vehicle. It operates in broad range from 3000 RPM to 18000 RPM. So, sufficient flow rate and low noise are needed in such broad operating range for a cooling fan of this alternator. In current study, the cooling fan of an alternator is developed through DFSS process and numerical analysis. In order to calculate flow rate and noise level, SC/Tetra and Flow Noise are used respectively, for a new developed fan, compared with original model, numerical result shows 3 dBA reduction and measured value shows 4 dBA reduction.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년 추계학술대회논문집
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• pp.233-238
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• 2008

An alternator which converts mechanical rotating energy into electric energy is an important component of a vehicle. It operates in broad range from 3000 RPM to 18000 RPM. So, sufficient flow rate and low noise are needed in such broad operating range for a cooling fan of this alternator. In current study, the cooling fan of an alternator is developed through DFSS process and numerical analysis. In order to calculate flow rate and noise level, SC/Tetra and Flow Noise are used respectively, for a new developed fan, compared with original model, numerical result shows 3 dBA reduction and measured value shows 4 dBA reduction.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2003년도 춘계학술대회 논문집
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• pp.925-928
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• 2003

In this paper, a precision measuring machine for large sized axial fans of cooling towers are developed. A laser sensor is used as a measuring device and aluminum profiles and stepping motors are engaged into the system as frame structure and driving devices respectively. 3-dimensional measuring data are compared to the design data to compute the distortion of the axial fans. Two distortions such as the axis of the fan and the airfoils along the axis are introduced to define the shape precision of axial fans. Genetic algorithm is used to solve the optimization problem during computing the distortion. Results of distortion are displayed 3 dimensionally in a solid-modeler as well as 2-D drawings to help users find it with case.