http://chineseinput.net/에서 pinyin(병음)방식으로 중국어를 변환할 수 있습니다.
변환된 중국어를 복사하여 사용하시면 됩니다.
항공전자기기용 냉각시스템의 대체냉매 적용에 관한 실험적 연구
강훈(Hoon Kang),정종호(Jongho Jung),정민우(Minwoo Jung),지용남(Yongnam Chi),유용선(Yongseon Yoo),최희주(Heeju Choi),변영만(Youngman Byeon),김영진(Youngjin Kim),오광윤(Kwangyoon Oh),김용찬(Yongchan Kim) 대한기계학회 2013 大韓機械學會論文集B Vol.37 No.5
항공전자기기의 정상적인 동작을 위해서는 내부에서 발생되는 열부하를 적절히 처리해야 하기 때문에 냉각시스템의 장착이 요구된다. 본 연구에서는 항공용 냉각시스템으로의 대체냉매 적용 가능성을 분석하기 위하여 증기압축 사이클 방식의 밀폐 공기순환 냉각시스템을 설계·제작하였다. 대체냉매로 가장 유력한 R236fa를 냉각시스템에 적용하여 냉매 충전량, 팽창밸브 개도, 그리고 압축기 운전회전수 변화에 따른 성능특성을 실험적으로 고찰하였다. 또한, 실험결과를 기존 냉매인 R124의 실험결과와 비교·평가를 수행하여, R236fa가 대체냉매로서 적용 가능함을 확인하였다. 최종적으로 R236fa를 적용한 냉각시스템의 효율 향상을 위한 설계 개선안을 제시하였다. A cooling system is adopted to control the thermal load from the avionic equipments in an aircraft for stable operation. In this study, an avionic cooling system was designed and manufactured by adopting a vapor compression cycle with a closed-loop air-circulation system to investigate the operating characteristics of an alternative refrigerant. The performance characteristics of a cooling system adopting R236fa as an alternative refrigerant were experimentally determined by varying the refrigerant charging amount, expansion valve opening, and compressor rotation speed. The experimental results were analyzed and compared with those of a cooling system adopting R124 as a refrigerant. The possibility of the adoption of R236fa as an alternative refrigerant was verified, and design solutions were suggested to improve the system efficiency.
항공기 외장형 정찰 장비용 냉각 시스템의 성능 특성에 관한 실험적 연구
정대윤,이행복,Jung, Daeyoon,Lee, Hang Bok 한국군사과학기술학회 2013 한국군사과학기술학회지 Vol.16 No.1
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.