• 제목/요약/키워드: Brayton Cycle

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Performance analysis of S-CO2 recompression Brayton cycle based on turbomachinery detailed design

  • Zhang, Yuandong;Peng, Minjun;Xia, Genglei;Wang, Ge;Zhou, Cheng
    • Nuclear Engineering and Technology
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    • 제52권9호
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    • pp.2107-2118
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    • 2020
  • The nuclear reactor coupled with supercritical carbon dioxide (S-CO2) Brayton cycle has good prospects in generation IV reactors. Turbomachineries (turbine and compressor) are important work equipment in circulatory system, whose performances are critical to the efficiency of the energy conversion system. However, the sharp variations of S-CO2 thermophysical properties make turbomachinery performances more complex than that of traditional working fluids. Meanwhile, almost no systematic analysis has considered the effects of turbomachinery efficiency under different conditions. In this paper, an in-house code was developed to realize the geometric design and performance prediction of S-CO2 turbomachinery, and was coupled with systematic code for Brayton cycle characteristics analysis. The models and methodology adopted in calculation code were validated by experimental data. The effects of recompressed fraction, pressure and temperature on S-CO2 recompression Brayton cycle were studied based on detailed design of turbomachinery. The results demonstrate that the recompressed fraction affects the turbomachinery characteristic by changing the mass flow and effects the system performance eventually. By contrast, the turbomachinery efficiency is insensitive to variation in pressure and temperature due to almost constant mass flow. In addition, the S-CO2 thermophysical properties and the position of minimum temperature difference are significant influential factors of cyclic performance.

초전도 전력 케이블 냉각 시스템 적용을 위한 극저온 터보 팽창기 설계 및 해석 (Design and Analysis of Cryogenic Turbo Expander for HTS Power Cable Refrigeration System)

  • 이창형;김동민;양형석;김석호
    • 한국기계가공학회지
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    • 제14권3호
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    • pp.141-148
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    • 2015
  • The cryogenic cooling system should maintain the HTS power cable below 77 K. As the length of HTS power cables has increased, there have been many efforts to develop large capacity cryocoolers. Brayton, Joule-Thomson, and Claude refrigerators were considered for the large capacity cryocooler. Among the various cryocoolers, the Brayton refrigerator is the most competitive in terms of the HTS power cable. At present, it is thought that a 10-kW class refrigerator will be able to be used as a unit cooling system for the commercialization of HTS power cables in the near future. The Brayton refrigerator is composed of recuperative heat exchangers, a compressor, and a cryogenic turbo expander. Among the various components, the cryogenic turbo expander is the part that decreases the temperature, and it is the most significant component that is closely related with overall system efficiency. It rotates at high speed using high-pressure helium or neon gas at cryogenic temperatures. This paper describes the design of a 300-W class Brayton refrigeration cycle and the cryogenic turbo expander as a downscale model for the practical 10-kW class cycle. Flow and structural analyses are performed on the rotating impeller and nozzle to verify the efficiency and the design performance.

HTS 케이블 냉각용 역브레이튼 사이클 극저온 냉동기 설계에 관한 연구 (Design of Reverse Brayton Cycle Cryocooler System for HTS Cable Cooling)

  • 박재홍;권용하;김영수;박성출
    • 한국초전도ㆍ저온공학회논문지
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    • 제5권2호
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    • pp.58-65
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    • 2003
  • The high temperature superconductivity(HTS) cable must be cooled below the nitrogen liquefaction temperature to applicate the cable in power generation and transmi-ssion system under the superconducting state. To obtain superconducting state. a reliable cryocooler system is required. Structural and thermal design have been performed to design cryocooler system operated with reverse Brayton cycle using gas neon as refrigerant. This cryocooler system consists of compressor. recuperator. coldbox. control valves and has 1 kW cooling capacity. Heat loss calculation was conducted for the given cryocooler system by considering the conduction and radiation through the multi-layer insulation(MLI) and high vacuum. The results can be summarized as: conduction heat loss is 7 W in valves and access port and radiation heat loss is 18 W through the surface of cryocooler. The full design specifications were discussed and the results were applied to construct in house HTS cable cooling system.

초임계 이산화탄소 이중 브레이튼 사이클 개발 연구 (Research on the Development of the Supercritical CO2 Dual Brayton Cycle)

  • 백영진;나선익;조준현;신형기;이길봉
    • 대한기계학회논문집B
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    • 제40권10호
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    • pp.673-679
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    • 2016
  • 초임계 이산화탄소 사이클은 소형화 및 효율 향상에 대한 잠재력 때문에 최근 관심이 증가하고 있으며, 원자력, 태양열(CSP) 및 화력 발전 분야에서 활발히 연구되고 있다. 이와 관련하여, 본 논문에서는 한국에너지기술연구원(KIER)의 초임계 이산화탄소 동력 사이클 연구 내용과 현황을 소개하였다. 1 단계 연구에서는 단순 초임계 브레이튼 사이클 실험 루프를 제작 및 시운전 하였으며, 현재 진행중인 2 단계 연구에서는 두개의 터빈과 두개의 재생기를 갖는 초임계 이중(dual) 브레이튼 사이클을 설계 및 제작하고 있다. 최적 설계를 위한 초임계 이중 브레이튼 사이클 모델링 및 시뮬레이션 결과, 본 연구에서 고려한 조건하에서, 사이클의 순출력을 극대화시키는 설계 변수가 존재함을 확인하였다.

2 kW급 브레이튼 냉동기용 열역학 사이클 및 극저온 터보 팽창기 설계 (Design of Thermodynamic Cycle and Cryogenic Turbo Expander for 2 kW Class Brayton Refrigerator)

  • 이진우;이창형;양형석;김석호
    • KEPCO Journal on Electric Power and Energy
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    • 제2권2호
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    • pp.299-305
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    • 2016
  • 초전도 전력 케이블의 상용화 노력에 따라 점차 장선화 되면서, 단위 냉각 시스템당 냉각용량이 큰 대용량 냉동기의 필요성이 증가하고 있다. 국내에서는 극저온 냉동기에 대한 기술 부족으로 인해 현재 극저온 냉동기는 해외 선진사로부터 고가의 비용으로 수입되고 있다. 초전도 전력 케이블의 상용화를 위해서는 대용량 브레이튼 냉동기의 국내 개발이 시급하다. 대용량 브레이튼 냉동기의 구성은 복열식 열교환기, 압축기, 극저온 터보 팽창기로 구성되어 있으며, 냉동기 효율과 가장 직접적인 연관이 있는 것은 극저온 터보 팽창기이다. 극저온 터보 팽창기는 극저온에서 고속으로 회전하면서 고압의 헬륨 혹은 네온 가스를 팽창시켜 온도를 낮추는 역할을 한다. 본 논문에서는 역브레이튼 냉동 사이클을 설계하고, 이에 적합한 극저온 터보 팽창기를 설계하였다.

Recent trends of supercritical CO2 Brayton cycle: Bibliometric analysis and research review

  • Yu, Aofang;Su, Wen;Lin, Xinxing;Zhou, Naijun
    • Nuclear Engineering and Technology
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    • 제53권3호
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    • pp.699-714
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    • 2021
  • Supercritical CO2 (S-CO2) Brayton cycle has been applied to various heat sources in recent decades, owing to the characteristics of compact structure and high efficiency. Understanding the research development in this emerging research field is crucial for future study. Thus, a bibliometric approach is employed to analyze the scientific publications of S-CO2 cycle field from 2000 to 2019. In Scopus database, there were totally 724 publications from 1378 authors and 543 institutes, which were distributed over 55 countries. Based on the software-BibExcel, these publications were analyzed from various aspects, such as major research areas, affiliations and keyword occurrence frequency. Furthermore, parameters such as citations, hot articles were also employed to evaluate the research output of productive countries, institutes and authors. The analysis showed that each paper has been cited 13.39 times averagely. United States was identified as the leading country in S-CO2 research followed by China and South Korea. Based on the contents of publications, existing researches on S-CO2 are briefly reviewed from the five aspects, namely application, cycle configurations and modeling, CO2-based mixtures, system components, and experiments. Future development is suggested to accelerate the commercialization of S-CO2 power system.

브레이튼과 펄스 데토네이션 복합 엔진 사이클의 열역학적 성능 해석 (Thermodynamic Analysis of Hybrid Engine Cycle of Brayton and Pulse Detonation Engine)

  • 김건홍;구자예
    • 한국항공운항학회지
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    • 제15권1호
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    • pp.1-10
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    • 2007
  • When detonation is occurred, the working fluid is compressed itself, though there are no other devices that compress the fluid. As a result, an engine which uses detonation for a combustion process doesn't need moving parts so that the engine can be lighter than other engines ever exist, and such an engine is often referred to as a pulse detonation engine. Since using detonation has higher performance than using deflagration, many studies have been attempting to control and analyze the engines using detonation as combustion. The purpose of this study is to analyze the hybrid cycle which is consisted of Brayton and Pulse Detonation Engine cycle. At first, we set the theoretical basis of detonation analysis, and after that we consider two hybrid cycles; a turbojet hybrid cycle and a turbofan hybrid cycle. The more energy released, the higher detonation Mach number the detonation wave has. In general, a cycle which has a detonation process has higher performances but thermal efficiency of hybrid turbofan engine.

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Real operation of 2 kW class reverse-Brayton refrigeration system with using scroll compressor package

  • Kim, Hyobong;Yeom, Hankil;Choo, Sangyoon;Kim, Jongwoo;Park, Jiho;In, Sehwan;Hong, Yong-Ju;Park, Seong-Je;Ko, Junseok
    • 한국초전도ㆍ저온공학회논문지
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    • 제22권4호
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    • pp.40-44
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    • 2020
  • This paper describes the real operation of 2 kW class reverse-Brayton refrigeration system with neon as a working fluid. The refrigeration cycle is designed with operating pressure of 0.5 and 1.0 MPa at low and high pressure side, respectively. Compressor package consists of several helium scroll compressors witch are originally used for driving GM cryocooler. Three segments of plate heat exchanger are adopted to cover the wide temperature range and the refrigeration power is produced by turbo expander. The developed refrigeration system is successfully operated at its target temperature of 77 K. In experiments, all parameters such as pressure, temperature, mass flow rate and valve opening are measured to investigate characteristics during cool-down process and normal state. The difference between design and real operation is discussed with measured experimental data. At normal state of 77 K operation, the developed reverse-Brayton refrigeration system shows 1.83 kW at 68.2 K of cold-end temperature.

熱交換 過程 을 考慮한 브레이튼 사이클 의 最大出力條件 (The maximum power condition of the Brayton cycle with heat exchange processes)

  • 정평석;차진걸;노승탁
    • 대한기계학회논문집
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    • 제9권6호
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    • pp.795-800
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    • 1985
  • 본 연구에서는 위의 내용을 한 단계 더 발전시켜 유한열용량 유동 사이에서 작동하는 브레이튼 사이클의 운전조건에 따른 출력변화와 취대출력 조건을 규명하였으 며, 이것은 단순히 이론적용 대상의 확장이라는 의미와 함께, 앞에서의 카노 사이클의 이상적인 사이클인 반면 브레이튼 사이클이라는 점에서 공학적 의의가 있으며, 특히 원자력 등을 열원으로 하는, 열교환기가 있는 가스 터어빈 사이클의 설계나 운전조건 의 결정 등에는 직접 적용될 수도 있을 것이다.

ASSESSMENT OF GAS COOLED FAST REACTOR WITH INDIRECT SUPERCRITICAL $CO_2$ CYCLE

  • Hejzlar, P.;Dostal, V.;Driscoll, M.J.;Dumaz, P.;Poullennec, G.;Alpy, N.
    • Nuclear Engineering and Technology
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    • 제38권2호
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    • pp.109-118
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    • 2006
  • Various indirect power cycle options for a helium cooled gas cooled fast reactor (GFR) with particular focus on a supercritical $CO_2(SCO_2)$ indirect cycle are investigated as an alternative to a helium cooled direct cycle GFR. The balance of plant (BOP) options include helium-nitrogen Brayton cycle, supercritical water Rankine cycle, and $SCO_2$ recompression Brayton power cycle in three versions: (1) basic design with turbine inlet temperature of $550^{\circ}C$, (2) advanced design with turbine inlet temperature of $650^{\circ}C$ and (3) advanced design with the same turbine inlet temperature and reduced compressor inlet temperature. The indirect $SCO_2$ recompression cycle is found attractive since in addition to easier BOP maintenance it allows significant reduction of core outlet temperature, making design of the primary system easier while achieving very attractive efficiencies comparable to or slightly lower than, the efficiency of the reference GFR direct cycle design. In addition, the indirect cycle arrangement allows significant reduction of the GFR &proximate-containment& and the BOP for the $SCO_2$ cycle is very compact. Both these factors will lead to reduced capital cost.