• 에너지공학
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• 제24권4호
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• pp.124-129
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• 2015

$Al_2O_3$ 나노입자의 농도별로 전동식 압축기의 회전속도(rpm)의 변화에 따른 자동차용 증기압축 냉동사이클의 COP를 실험적으로 평가하고 나노입자를 적용하지 않은 기준 사이클의 COP와 비교하였다. 이를 위해 실제 하이브리드 자동차에서 쓰는 사이클 부품들을 이용하고 항온항습 챔버를 이용하지 않는 방식으로 장치를 설계 및 제작하였다. 별도의 전동식 인버터 압축기의 제어장치를 활용하여 1000rpm부터 500rpm 간격으로 4000rpm까지와 $Al_2O_3$ 나노입자를 질량비 기준으로 농도 0.05%, 0.1%, 0.2%와 0.5%의 범위에 대하여 실험을 수행하였다. 이를 통해 기준 사이클과 비교하면 기준 사이클의 일반적인 운전조건인 약 3000rpm에서 $Al_2O_3$ 나노유체를 적용하는 사이클의 COP는 질량 농도비 0.05%에서는 15.4% 정도, 농도비 0.1%, 0.2% 및 0.5%에서는 각각 9.4%, 13% 및 9.6%가 증가함을 알 수 있었다.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2006년도 동계학술발표대회 논문집
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• pp.87-87
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• 2006

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2008년도 하계학술발표대회 논문집
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• pp.255-262
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• 2008

The simulation of refrigeration cycle is important since the experimental approach is too costly and time-consuming. The present simulation focuses on the effect of capillary tube-suction line heat exchangers (CT-SLHX), which are widely used in small vapor compression refrigeration systems. The simulation of steady states is based on fundamental conservation equations of mass and energy. These equations are solved simultaneously through iterative process. The non-adiabatic capillary tube model is based on homogeneous two-phase model. This model is used to understand the refrigerant flow behavior inside the non-adiabatic capillary tubes. The simulation results show that both of the location and length of heat exchange section influence the coefficient of performance (COP). These results can be used in either design calculation of capillary tube length for refrigeration cycle or effect of suction line heat exchanging on refrigeration cycle.

• 대한기계학회논문집B
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• 제34권9호
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• pp.809-816
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• 2010

환경제어시스템은 항공전자장비로부터의 열부하를 제거하기 위한 목적으로 설치되어지며, 본 환경제어시스템은 제어변수의 변화에 따라 다양한 운전특성을 나타낸다. 본 연구에서는 냉매 R-124를 작동유체로 하는 증기압축 사이클 방식을 적용한 환경제어시스템을 설계 및 제작하였다. 냉매충전량, 팽창밸브개도, 압축기 및 송풍기 운전회전수와 같은 제어변수의 변화에 따른 환경제어시스템의 성능 및 운전 특성 변화를 실험하였다. 각 제어변수가 시스템에 미치는 영향을 분석하였으며, 최적제어를 위한 방안을 제안하였다.

• 설비공학논문집
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• 제21권9호
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• pp.519-526
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• 2009

Environmental control system is adopted to control the thermal load from the avionic equipment in the reconnaissance pod which is mounted under a fighter aircraft, undergoing large and rapid environmental changes with the variations of flight altitude and velocity. In this study, an environmental control system was designed and built by adopting vapor compression cycle using R-124. The cooling performance characteristics of the system were measured varying operating parameters: thermal load in the pod, air mass flow rate through evaporator, condenser inlet air temperature, and air mass flow rate through condenser. The effects of the experimental parameters on the system performance were analyzed based on the experimental results. The problems on the designed system were also analyzed and the solutions were suggested to improve system efficiency and to obtain stable operation.

• 대한기계학회논문집B
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• 제35권12호
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• pp.1367-1373
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• 2011

본 연구에서는 천연냉매를 적용한 압축/흡수식 하이브리드 고온제조 히트펌프를 실험적으로 연구한 결과를 제시하였다. 압축/흡수식 히트펌프는 기존의 증기압축 히트펌프에 비해 고온영역을 포함한 넓은 생산온도범위, 높은 승온기능, 다양한 용량 제어방법 등 여러가지 장점을 가지고 있다. 제작된 하이브리드 히트펌프는 현재 실제 산업현장에 적용하기 이전의 초기 시제품 단계로 실험실에 설치하여 운전하였으며, 주요 구성부품으로는 이단압축기, 흡수기, 재생기, 과열냉각기, 용액 열교환기, 용액펌프, 기액분리기/정류기 등이다. 성능실험에서 $50^{\circ}C$의 열원을 고온 및 저온열원으로 사용한 결과 $90^{\circ}C$ 이상의 고온수 토출과 10 kW급의 난방 용량을 얻을 수 있었다. 혼합냉매의 성분비 변화에 따른 압축기/펌프 유량의 순환비 변화 및 다양한 성능변화를 실험적으로 관찰하였으며, 시스템의 효율과 용량에 있어 최적 성분비가 존재함을 확인하였다.

• 설비공학논문집
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• 제21권3호
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• pp.131-139
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• 2009

The simulation of refrigeration cycle is important since the experimental approach is costly and time-consuming. The present paper focuses on the simulation of a refrigeration cycle equipped with a capillary tube-suction line heat exchanger(SLHX), which is widely used in small vapor compression refrigeration systems. The present simulation is based on fundamental conservation equations of mass, momentum, and energy. These equations are solved through an iterative process. The non-adiabatic capillary tube model is based on homogeneous two-phase flow model. This model is used to understand the refrigerant flow behavior inside the non-adiabatic capillary tube. The simulation results show that both of the location and length of heat exchange section influence the coefficient of performance (COP).

• 한국태양에너지학회 논문집
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• 제34권3호
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• pp.42-48
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• 2014

An experimental study was performed estimating COP(Coefficient of Performance) of air-conditioning cycle with inverter scroll compressor. All experiments were done for various compressor speeds from 1000~4000 rpm and used the inverter controller called CANDy to change the compressor rpm. The air-conditioning cycle components in the apparatus were used as same with components of YF hybrid car. To estimate the COP, this study measured the temperature and pressure at inlets and outlets of compressor, condenser, and evaporator. And also measured the compressor input power using Powermeter. Through the experiments, the maximum error to estimate COP was shown about ${\pm}6.09%$ at 3500rpm. This study revealed that the condenser temperature and pressure were increased and the evaporator temperature and pressure were decreased with the increased compressor speed. And also, the COP was decreased with increased compressor speed. Those results can be used the basic and fundamental data to design the air-conditioning cycle with inverter scroll compressor.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1996년도 추계학술대회 논문집
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• pp.371-376
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• 1996

The damping force of shock absorber in an automobile is determined by the components which construct the S/A. In this study we investigate the individual effect of these components on damping force. In addition, opening of important valve doling compression and tension cycle due to up-down reciprocation movement is also researched. Thus we are to strictly control the properties and tolerance of components having important effects on tile damping force and to produce S/A of better quality.

• 한국정밀공학회지
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• 제14권10호
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• pp.44-49
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• 1997

The damping force is determined by four valves and the components which consist of the shock absorber for vehicle. In this study it is investigated the individual effects of four valves and these components on damping forces using dynamic behaviour analysis program of the shock absorber. In addition, opening of main valves are researched during compression and tension cycle due to up- down reciprocation movement of piston. We are to strictly control the properties and tolerance of componenets having important effects on the damping force. Thus we are intended to produce shock absorber of better quality.