원문정보
초록
영어
Cooling by gas helium circulation can be used for various HTS (high temperature superconductor) magnets operating at 20~40 K, and a cryogenic blower is an essential device for circulating gas helium in the cooling system. The performance of the cryogenic blower is determined by various design parameters such as the impeller diameter, the blade number, the vane angle, the volute cross-sectional area, and the rotating speed. The trailing edge angle and the height of impeller vane are also key design factors in determining the blower performance. This study describes the design, fabrication and performance evaluation of cryogenic blower to produce a flow rate of 30 g/s at 5 bar, 35 K gas helium. The impeller shape is designed using a specific speed/specific diameter diagram and CFD analysis. After the fabrication of the cryogenic blower, a test equipment is also developed using a GM cryocooler. The measured flow rates and the pressure differences are compared with the design values at various rotating speeds and the results show a good agreement. Isentropic efficiency is also evaluated using the measured pressures and temperatures.
목차
1. 서론
2. 극저온 블로워 설계
2.1. 운전 조건과 임펠러 설계 조건
2.2. 비속도-비직경 관계에 의한 기초 설계
2.3. 극저온 블로워 임펠러 상세 형상 설계
2.4. 극저온 블로워의 유동 해석
2.5. 구동부 축 설계 및 전도 열침입
3. 극저온 블로워의 구성 및 제작
4. 극저온 블로워의 성능 평가
4.1. 극저온 블로워 성능 평가 장치
4.2. 극저온 블로워 성능 평가 결과
5. 결론
ACKNOWLEDGMENT
REFERENCES
