• Title/Summary/Keyword: Air-cycle refrigeration

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An Experimental Study of the 2-stage Gifford-McMahon Cryorefrigerator (2단 Gifford-McMahon 극저온냉동기의 특성실험)

  • Park, S.J.;Koh, D.Y.;Yoo, C.J.;Kim, E.J.;Choi, H.O.
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.5 no.3
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    • pp.198-206
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    • 1993
  • Experimental results of two stage Gifford-McMahon cryorefrigerator are described. In-prototype experiments, drive mechanism is Scotch Yoke type driven by stepping motor, copper meshes and lead balls are used for regenerator's materials in the first stage and the second stage, respectively. To find optimal conditions of the cryopump, no load temperature and refrigeration capacity according to the variation of cycle frequency and operating pressure are measured, and the cool down and load characteristics at particular cycle frequencies are presented. In general, as the cycle frequency is lowered, no load temperature is dropped but refrigeration capacity is diminished. As the representative result, in a case that the cycle frequency is 70rpm and steady state pressure is 14 atm, no load temperature of second stage is lowered to 10.5K in 55 minuters, and in this situation the refrigeration capacity of the first stage is 42W at 80K, that of the second stage is 11 W at 20K.

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A Study on the Comparison of Design Conditions between Booster Ejector and Air Ejector in the Steam-Jet Water-Vapour Refrigeration Cycle (증기분사냉동계의 부우스터 이젝터와 에어 이젝터의 설계조건비교에 관한 연구)

  • Lee, Chang-Sik
    • The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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    • v.7 no.2
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    • pp.73-79
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    • 1978
  • This paper presents the experimental study on the design conditions of pressure between booster ejector and air ejector in the steam-jet water-vapour refrigeration system. In this experiment, the motive steam of booster ejector and ai. ejector was dry saturated from 6 ata to 8 ata and flash chamber pressure were about $10\∼540mmHg$ higher than mixing section in booster ejector. The investigation of air on the pressure of booster ejector was performed by changing the condenser pressure. The experimental results show that flash chamber vacuum and condenser pressure of steam-jet refrigeration cycle increased in accordance with the increase of motive steam Pressure. Among the several nozzle sires tested, No.4 nozzle were best in term of evaporator vacuum under the constant operating conditions of air ejector in condenser.

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Experimental Study of a High Efficiency Transport Refrigeration Container under Cooling and Defrosting Conditions (고효율 냉동 컨테이너의 냉각 및 제상 실험)

  • Mun, Je-Cheol;Ardiyansyah, Ardiyansyah;Choi, Kwang-Il;Oh, Jong-Taek
    • Proceedings of the SAREK Conference
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    • 2008.06a
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    • pp.277-281
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    • 2008
  • This paper presents the development of a high efficiency transport refrigeration system for sliced-raw fish transportation. The refrigeration system is equipped with heat storage for reverse cycle-hot gas defrost (the stored heat is used during defrost cycle of the system). System performance and container operating conditions are analyzed during experimental investigation on a $3,225{\times}1,740{\times}1,640\;mm$ full-scale refrigerated container under cooling and defrosting conditions. The prototype system indicates better performance in terms of shorter cooling-down time, shorter defrost time and smaller fluctuations of refrigerated container's temperature.

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Oplimum Design Conditions for a Basic Refrigeration Cycle (냉동사이클의 최적 설계조건)

  • Cho, Sung-Whan
    • The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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    • v.15 no.4
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    • pp.356-361
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    • 1986
  • An optimum design condition for a basic refrigeration cycle is defined as the condition which minimizes the total cost of heat exchanges (condenser and evaporator) and compressor for the refrigeration effect. Thermodynamic properties of ammonia (R717) are approximated by rational functions in order to obtain the optimum condition for a basic refrigeration cycle. Optimum condition depends on the heat capacity rates (mass flow rate times specific heat) of cooling water and brine used in condenser and evaporator. The difference between the cooling water temperature and condensation temperature at the optimum condition increases as the heat capacity rates and the coat of heat exchangers relative to the cost of compressor increase. Numerical examples of optimum conditions are obtained when the condensation temperature is $30^{\circ}C$ and the evaporator temperature is $-10^{\circ}C$.

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Performance Characteristics of OTEC(Ocean Thermal Energy Conversion) Power Cycle with Vapor-Liquid Ejector (증기-액 이젝터를 적용한 해양온도차발전 시스템의 성능 특성)

  • Yoon, Jung-In;Son, Chang-Hyo;Kim, Hyeon-Uk;Ha, Soo-Jung;Lee, Ho-Saeng;Kim, Hyun-Ju
    • Journal of Power System Engineering
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    • v.18 no.5
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    • pp.88-93
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    • 2014
  • In this paper, the performance analysis of condensation and evaporation capacity, turbine work and efficiency of the OTEC power system using vapor-liquid Ejector is presented to offer the basic design data for the operating parameters of the system. The working fluid used in this system is $CO_2$. The operating parameters considered in this study include the vapor quality at heat exchanger outlet, pressure ratio of ejector and inlet pressure of low turbine, mass flow ratio of separator at condenser outlet. The main results were summarized as follows. The efficiency of the OTEC power cycle has an enormous effect on the mass flow ratio of separator at condenser outlet. With a thorough grasp of these effects, it is possible to design the OTEC power cycle proposed in this study.

Design of Membership Ranges for Robust Control of Variable Speed Drive Refrigeration Cycle Based on Fuzzy Logic (가변속 냉동사이클의 강인제어를 위한 퍼지로직의 멤버십함수 범위 설계)

  • Jeong, Seok-Kwon
    • Journal of Power System Engineering
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    • v.22 no.1
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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.

Simulation of the effects of a non-adiabatic capillary tube on refrigeration cycle (비단열 모세관의 영향을 고려한 냉동 사이클 시뮬레이션)

  • Park, Sang-Goo;Son, Ki-Dong;Jeong, Ji-Hawn;Kim, Lyun-Su
    • Proceedings of the SAREK Conference
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    • 2008.06a
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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.

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Comparison of Performance in CO2 Cooling System with an Ejector for Various Operating Conditions (다양한 운전조건에서 이젝터를 적용한 CO2 냉동기의 성능비교)

  • Kang, Byun;Cho, Hong-Hyun
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.23 no.7
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    • pp.505-512
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    • 2011
  • Recently, many researchers have analyzed the performance of the transcritical $CO_2$ refrigeration cycle in order to identify opportunities to improve the system energy efficiency. The reduction of the expansion process losses is one of the key issues to improve the efficiency of the transcritical $CO_2$ refrigeration cycle. In this study, the analytical study on the performance characteristics of $CO_2$ cycle with an ejector carried out with a variation of outdoor temperature, gascooler inlet air velocity, evaporator inlet air velocity, and evaporator inlet air temperature. As a result, the system performance could be improved over 85% by using an ejector for various operating condition because of the reduction of compressor work. Moreover, the cooling capacity increased about 18% for variable outdoor condition. Therefore, the high performance of an ejector system could be maintained for wide operating conditions and system reliability could be improved compared to that of a basic system.

Performance Evaluation of $CO_2$ Air-Conditioning System (이산화탄소를 사용하는 냉동 시스템의 성능 평가 (I))

  • 신지영
    • Journal of Advanced Marine Engineering and Technology
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    • v.24 no.2
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    • pp.24-30
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    • 2000
  • The high-pressure natural refrigerant $CO_2$ is now being evaluated for use in the motor vehicle air-conditioning systems and for several types of unitary equipment. In this study thermodynamic properties of $CO_2$ is compared to those of R-22 and R-134a and the performance characteristics of $CO_2$ refrigeration cycle is analyzed. The results show that the optimum discharge pressure for the cycle performance exists. New design concept for the $CO_2$ refrigeration system should be developed due to the high-operating pressure of itself.

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