Effect of a Turbo-Expander for Regeneration in the Expansion Process

팽창과정에서의 터보엑스펜더 영향에 관한 연구

  • 조종현 (경상대학교 항공우주공학과) ;
  • 조봉수 (경상대학교 항공우주공학과) ;
  • 김재실 (창원대학교 기계공학과) ;
  • 조수용 (경상대학교 기계항공공학부)
  • Published : 2006.08.23

Abstract

A turbo-expander is developed for the regeneration in the expansion process. The turbo-expander operates in the partial admission and supersonic flow, and an axial-type single stage turbine is applied to the turbo-expander. Its outer diameter is 82mm and the operating gas is R134a. A 15kW reciprocating compressor is applied in this experiment and the turbo-expander is installed in the expansion process instead of the commonly using expansion valve. Two supersonic nozzles are applied for the expansion process. The high speed of R 134a after passing the supersonic nozzles gives the impulse force to the turbo-expander and some powers are generated on this process. A generator is installed at the end of the turbo-expander shaft. The generating output power from the turbo-expander is controlled by the power controller. Pressures and temperatures are measured on the lines for the performance investigation. More than 600W/(kg/sec) are generated in this experiment.

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