• 한국수소및신에너지학회논문집
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• 제29권5호
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• pp.490-496
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• 2018

Recently, the power and refrigeration cogeneration based on Kalina cycle has attracted much attention for more efficient utilization of low-grade energy. This study presents a thermodynamic performance analysis of a cogeneration cycle of power and absorption refrigeration based on Kalina cycle. The cycle combines Kalina cycle (KCS-11) and absorption cycles by adding a condenser and an evaporator between turbine and absorber. The effects of ammonia mass fraction and separation pressure were investigated on the system performance of the system. Results showed that the energy utilization of the system could be greatly improved compared to the basic Kalina cycle.

• 융복합기술연구소 논문집
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• 제1권2호
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• pp.29-32
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• 2011

In this paper, we will introduce the overview of new project dealing how to increase of refrigeration cycle COP using nano-fluids, CuO, TiO2, Al2O3, that are used on similar previous studies. Recently many studies were performed to show the effect of nano-fluids at refrigeration cycle. But, the reason was not cleared yet. In general, the flow phenomena at the evaporator were guessed to be mixed with the partial pool boiling condition and the flow boiling condition from the previous results not published yet. So, we hope that the COP increase of refrigeration cycle will be verified and showed through this project.

• 한국수소및신에너지학회논문집
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• 제29권4호
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• pp.357-362
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• 2018

In this study, computer simulation and optimization works have been performed for a refrigeration cycle using ammonia as a refrigerant and also how much power was saved when the liquefied natural gas cold heat is replaced for the refrigeration cycle. PRO/II with PROVISION release 10.0 from Schneider electric company was used, and Peng-Robinson equation of the state model was selected for the modeling of the refrigeration cycle and LNG cold heat utilization process.

• 설비공학논문집
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• 제4권4호
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• pp.277-288
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• 1992

Numerical simulations are made of the refrigeration cycle in a domestic refrigerator/freezer. The main purpose of the present study is to predict the steady-state cycle performance with various specifications of cycle components and cabinet under the continuous running conditions. The detailed mathematical models are constructed for both the cycle components and cabinet, which are strongly coupled with each other. The simultaneous equations are solved by simple iteration method, and the results obtained are examined to assess the effect of the cycle components and cabinet modification on the system performance.

• 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.

• 한국군사과학기술학회지
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• 제16권1호
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• pp.74-80
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• 2013

In this paper, we have proposed a vapor cycle refrigeration system as a cooling system to provide cooling air to the aircraft external reconnaissance stores. In the proposed vapor cycle system, receiver which prevents refrigerant from subcooling was eliminated and thermal expansion valve was replaced with electronic expansion valve. The vapor cycle refrigeration system is aimed to provide cooling air to the reconnaissance stores which is added to the aircraft in the form of external store. The wide temperature range of ambient air from the flight conditions can decrease the cooling performance and can make the refrigeration system unstable in low ambient temperature. Performance characteristics of the vapor cycle refrigeration system has been experimented under air conditions which is derived from the flight envelope. From the experiments, the vapor cycle refrigeration system has been proved to provide enough cooling air to the reconnaissance equipment and to be stable under all the flight conditions.

• 한국산학기술학회논문지
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• 제12권2호
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• pp.1013-1019
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• 2011

본 논문에서는 천연가스를 액화시키기 위해서 프로판, 에틸렌 및 메탄 냉매를 이용한 다단 캐스케이드 냉동사이클에 대한 전산모사를 PRO/II with PROVISION 8.3에 내장되어 있는 Peng-Robinson 상태방정식을 활용하여 수행하였다. 천연가스의 조성은 한국가스공사로부터 제공받은 것을 적용하였으며, 유량은 연간 500만톤으로 가정하였다. 프로판 냉매의 공급온도는 $-40^{\circ}C$로, 에틸렌 냉매의 공급온도는 $-95^{\circ}C$로 메탄 냉매의 공급온도는 $-155^{\circ}C$로 각각 정하였으며, 천연가스와 각각의 냉매의 최소 접근온도는 $3^{\circ}C$로 정하였다. 다단 냉동을 위한 프로판 냉동 사이클은 3단 냉동을 가정하였으며, 에틸렌 냉동 사이클은 2단 냉동을 그리고 메탄 냉동 사이클은 3단 냉동을 가정하였다. 메탄 냉매에 의해서 $-152^{\circ}C$까지 냉각된 천연가스는 줄-톰슨 팽창에 의해서 $-162^{\circ}C$까지 냉각되어 액화가 일어나도록 하였다. 결론적으로 캐스케이드 냉동 사이클과 줄-톰슨 팽창을 통한 천연가스의 액화율은 몰 비로 91.71%이며, 액화천연가스 1.0 kg/hr당 0.433 kW의 압축 일이 필요함을 알 수 있었다.

• 동력기계공학회지
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• 제22권1호
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• pp.18-24
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• 2018

This paper focuses on systematic design about the membership ranges of the main design factors such as control error, control error rate, and sampling time for the fuzzy logic control of the variable speed drive refrigeration cycle. The upper and the lowest limit of the membership ranges are set up from the data of static characteristics obtained by experiments. Three kinds of membership ranges on the control error and the control error rate are tested by experiments. Especially, an effect of sampling time on control performance is also investigated in the same way. Experimental data showed the control error rate and the sampling time strongly effected on the control performance of the refrigeration cycle with a variable speed drive.

• 설비공학논문집
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• 제24권9호
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• pp.671-678
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• 2012

The objective of this study is to analyze theoretically the performance of an open air-cycle refrigeration system in which environmental concerns increase. The pressure ratio of the external compressor and efficiencies of the components that compose of the system are selected as important parameters. As the pressure ratio of the external compressor increases, the pressure ratio of the ACM compressor is determined high, the refrigerating temperature and capacity increase, the COP decreases, and the total entropy production rate increases. The effect of heat exchanger effectiveness and turbine efficiency on the performance are greater than that of the ACM compressor efficiency. Also the performance of the air-cycle refrigeration system with two heat exchangers has been enhanced like high COP and low total entropy production rate, compared to the system with one heat exchanger.

• 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).