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Parametric Study on Performance of Inertance Pulse Tube Cryocooler
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  • Parametric Study on Performance of Inertance Pulse Tube Cryocooler
  • Parametric Study on Performance of Inertance Pulse Tube Cryocooler
저자명
Lee. K.H.,Rhee. J.,Kim. J.S.
간행물명
International journal of aeronautical and space sciences
권/호정보
2014년|15권 2호|pp.205-211 (7 pages)
발행정보
한국항공우주학회
파일정보
정기간행물|ENG|
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이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
서지반출

기타언어초록

The design parameters to affect the cooling capacity of a cryocooler were examined with the application of numerical modeling to optimize an inertance pulse tube cryocooler. This modeling includes the regenerator, pulse tube, inertance tube, gas reservoir, and heat exchangers. One-dimensional modeling on strings of acoustic and thermoacoustic elements was applied to compare the design parameters. The diameter and length of the pulse tube can significantly affect the cooling capacity and efficiency. The aftercooler was optimized by maintaining a certain size. The efficiency also improved as the length of inertance tube and volume of gas reservoir are increased. It was confirmed that effective design parameters are critical to the performance of an inertance pulse tube cryocooler considering the comparison of the dimensions of each part to optimize its cooling power and efficiency.