• 에너지공학
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• 제15권4호
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• pp.284-290
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• 2006

냉 난방 수요에서 일어나는 환경오염의 최소화와 화석연료 소비를 감소시키기 위해서 에너지 회수를 개선시키는 것은 필수적이다. 이러한 점에서 흡수식 열펌프기술은 에너지 절약을 위해서 많은 가능성을 가지고 있다. 흡수식 열펌프는 에너지를 주입하지 않고 폐열의 이용을 높일 수 있는 방법이다. 본 연구에서는 에너지 회수를 위한 재흡수 열펌프 연군를 메탄올-글리세린을 이용하여 수행하였다. 이 물질의 열역학 데이터를 이용하여 재흡수 열펌프의 이론적 열효율 값을 각 기관의 조업 조건에 따라서 계산하였다. $70{\sim}80^{\circ}C$의 산업 폐열 온도를 가지고 $40{\sim}50^{\circ}C$ 승온 시킬 때 열효율 값 0.4 이상을 얻을 수 있었다.

• Journal of Advanced Marine Engineering and Technology
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• 제39권9호
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• pp.881-889
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• 2015

해양온도차발전은 해양의 표층수와 심층수의 온도차를 이용하여 발전하는 유기랭킨사이클이다. 작동유체와 사이클 구성은 유기랭킨사이클의 열역학적 효율에 큰 영향을 미치는 요소이다. 본 연구에서는 작동유체와 사이클에 따른 해양온도차발전시스템의 성능분석을 수행하였다. 고전적인 단순 랭킨사이클과 단순 랭킨사이클의 대안으로 제시되고 있는 개방형 및 통합형 재생 랭킨사이클 그리고 칼리나 사이클이 본 연구에서 고려되었으며, 작동유체로는 9종의 단일냉매와 3종의 혼합냉매를 본 연구에 적용하였다. 사이클의 성능분석에는 핀치포인트온도차를 일정하게 유지하는 핀치포인트분석이 적용되었다. 성능분석결과를 살펴보면, 단순 랭킨사이클과 개방형 및 통합형 재생 랭킨사이클의 경우 RE245fa2를 작동유체로 사용하며, 칼리나 사이클의 경우 $NH_3/H_2O$의 질량비가 0.9:0.1일 때 열역학적 효율이 가장 높았다. 한편, 개방형 및 통합형 재생 랭킨사이클과 칼리나 사이클을 해양온도차발전시스템에 적용할 경우 단순 랭킨사이클과 비교하여 각각 약 2.0 %, 1.0%, 10.0%의 효율 향상을 기대할 수 있었다.

• 대한기계학회논문집B
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• 제36권3호
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• pp.293-299
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• 2012

대형 선박의 추진용 디젤엔진에서 버려지는 배기가스의 열을 회수하기 위한 랭킨사이클이 적용된 발전시스템에 대하여 R245fa 및 water 의 작동유체들에 따른 열역학적 효율 특성을 분석하였다. 그 이론적인 계산 결과로, 고정된 질량유량의 R245fa 에 대하여 터빈입구의 압력이 증가할수록 사이클, 시스템, 및 전체적 효율이 증가하였고, 사이클에 의해 발생되는 순동력도 증가하는 특성을 보였다. 반면, water 의 경우에는 R245fa 에 비하여 더 낮은 질량유량 및 터빈입구 압력의 비율에서 최대의 시스템 효율을 보였다. 또한 water 에 대하여 최적화된 사이클의 순출력, 시스템 효율, 및 전체적 효율의 값들은 R245fa 의 경우보다 더 크게 나타났다.

• 한국태양에너지학회 논문집
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• 제27권3호
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• pp.37-44
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• 2007

For the past few years, the concern for clean energy has been greatly increased. Ocean Thermal Energy Conversion(OTEC) power plants are studied as a viable option for the supply of clean energy. In this paper, the thermodynamic performance of OTEC cycle was examined. Computer simulation programs were developed under the same condition and various working fluids for closed Rankine cycle, regeneration cycle, Kalina cycle, open cycle and hybrid cycle. The results show that the regeneration cycle using R125 showed a 0.17 to 1.56% increase in energy efficiency, and simple Rankine cycle can generate electricity when the difference in warm and cold sea water inlet temperatures are greater than $15^{\circ}C$. Also, the cycle efficiency of OTEC power plant using the condenser effluent from nuclear power plant instead of the surface water increased about 2%.

• 한국태양에너지학회 논문집
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• 제30권3호
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• pp.124-130
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• 2010

Ocean Thermal Energy Conversion(OTEC) power plants have been examined as a viable option for supplying clean energy. This paper evaluated the thermodynamic performance of the OTEC Power system for the production of electric power and desalinated water. The results show that newly developed fluids such as R32, R125, R143a, and R410A that do not cause stratospheric ozone layer depletion perform as well as R22 and ammonia. Overall cycle efficiency of open cycle is the lowest value of 3.01% because about 10% of the gross power is used for pumping out non-condensable gas. Also, the hybrid cycle is an attempt to combine the best features and avoid the worst features of the open and closed cycles. The overall cycle efficiency of hybrid cycle is 3.44% and the amount of desalinated water is 0.0619 kg/s.

• 한국추진공학회지
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• 제3권2호
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• pp.48-55
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• 1999

50㎾급 터보제너레이터 가스터빈 엔진에 리쿠퍼레이터가 부착되는 경우 성능 변화를 조사하였다. 리쿠퍼레이터는 군사 및 소형 자동차용 엔진에 경제적 연비와 배기가스 저감의 목적으로 많이 적용되어 왔다. 열역학적 관점에서 볼 때 재생사이클은 압축비 10이하 및 비교적 낮은 터빈 입구온도에서 사이클의 효율 상승에 기여하는 바가 큰 것으로 나타난다. 1축단순사이클 터보제너레이터 가스터빈 엔진에 리쿠퍼레이터를 부착하는 경우 리쿠퍼레이터 효율 $\varepsilon$ = 0.5에서 엔진의 효율은 상대적으로 약 30% 증가하는 것으로 나타났고 이때 열교환기내의 압력 손실은 5.2%로 설계하였다. 용이한 제작, 구조적 견고성, 최소의 누출 둥의 장점으로 튜브형의 열교환 시스템이 본 가스터빈 엔진에 적합한 것으로 판단되었다.

• 한국수소및신에너지학회논문집
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• 제26권6호
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• pp.590-599
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• 2015

In this paper a performance analysis is carried out based on the first and second laws of thermodynamics for heat exchanger in organic Rankine cycle (ORC) for the recovery of low-temperature finite thermal energy source. In the analysis, effects of the selection of working fluid and pinch temperature difference are investigated on the performance of the heat exchanger including the effectiveness of the heat exchanger, exergy destruction, second-law efficiency, number of transfer unit (NTU), and pinch point. The temperature distribution are shown depending on the working fluids and the pinch temperature difference. The results show that the performance of the heat exchanger depends on the pinch temperature difference sensitively. As the pinch temperature increases, the exergy destruction in the evaporator increases but the effectiveness, second law efficiency and NTU decreases.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2008년도 춘계학술대회 논문집
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• pp.169-173
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• 2008

Stirling engine is a promising heat engine with a high efficiency, muti-fuel capability, low emission, quiet operation, very low maintenance and long life. As one of the promising applications, solar power system based on the Stirling dish, providing net solar-to-electric conversion efficiencies reaching 30%, can operate as stand-alone units in remote locations or can be linked together in groups to provide utility-scale power. This paper introduced a new Scroll-type Stirling engine, being developed for solar power, superior to conventional Stirling engines. The Scroll-type Stirling engine is characterized as traits of continuous and wholly separated compression and expansion; one-way flow system; direct cooling and heating the fluid in the working spaces through the extensive inner surfaces of scroll wraps. All theses traits contribute to achieving thermodynamic cycle closer to the ideal Stirling cycle (exactly speaking, Ericsson cycle).

• International Journal of Aeronautical and Space Sciences
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• 제18권4호
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• pp.651-661
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• 2017

A truss-braced wing (TBW) aircraft has recently received increasing attention due to higher aerodynamic efficiency compared to conventional cantilever wing aircraft. For conceptual TBW aircraft design, we developed a propulsion-and-airframe integrated design environment by replacing a semi-empirical turbofan engine model with a thermodynamic cycle-based one built upon the numerical propulsion system simulation (NPSS). The constructed NPSS model benefitted TBW aircraft design study, as it could handle engine installation effects influencing engine fuel efficiency. The NPSS model also contributed to broadening TBW aircraft design space, for it provided turbofan engine design variables involving a technology factor reflecting progress in propulsion technology. To effectively consolidate the NPSS propulsion model with the TBW airframe model, we devised a rapid, approximate substitute of the NPSS model by reduced-order modeling (ROM) to resolve difficulties in model integration. In addition, we formed an artificial neural network (ANN) that associates engine component attributes evaluated by object-oriented weight analysis of turbine engine (WATE++) with engine design variables to determine engine weight and size, both of which bring together the propulsion and airframe system models. Through propulsion-andairframe design space exploration, we optimized TBW aircraft design for fuel saving and revealed that a simple engine model neglecting engine installation effects may overestimate TBW aircraft performance.

• Advances in Energy Research
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• 제4권1호
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• pp.29-45
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• 2016

There has been a growing interest in the recent time for the development of solar power tower plants, which are mainly used for utility scale power generation. Combined heat and power (CHP) is an efficient and clean approach to generate electric power and useful thermal energy from a single heat source. The waste heat from the topping Brayton cycle is utilized in the bottoming HRSG cycle for driving steam turbine and also to produce process steam so that efficiency of the cycle is increased. A thermal storage system is likely to add greater reliability to such plants, providing power even during non-peak sunshine hours. This paper presents a conceptual configuration of a solar power tower combined heat and power plant with a topping air Brayton cycle. A simple downstream Rankine cycle with a heat recovery steam generator (HRSG) and a process heater have been considered for integration with the solar Brayton cycle. The conventional GT combustion chamber is replaced with a solar receiver. The combined cycle has been analyzed using energy as well as exergy methods for a range of pressure ratio across the GT block. From the thermodynamic analysis, it is found that such an integrated system would give a maximum total power (2.37 MW) at a much lower pressure ratio (5) with an overall efficiency exceeding 27%. The solar receiver and heliostats are the main components responsible for exergy destruction. However, exergetic performance of the components is found to improve at higher pressure ratio of the GT block.