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TEMPERATURE BOUNDARY EFFECT OF THE LARGE HEAT PUMP CYCLE ON THE CHARACTERISTICS OF THE TURBOCOMPRESSOR.

Author(s) : SAREVSKI M.

Summary

AN ANALYSIS HAS BEEN MADE OF THE INDUSTRIAL WATER COOLING SYSTEMS WHICH CAN BE USED AS A HEAT SOURCE. FOR THIS ANALYSIS, THE RANGE OF THE TEMPERATURE BOUNDARIES OF THE R12 HEAT PUMP CYCLES ARE CONSIDERED. RESULTS ARE GIVEN OF THE LOSSES IN THE IMPELLER AND DIFFUSER, THEIR INTERACTIONS, EXPECTED EFFICIENCY AND EXPECTED GAS DYNAMIC CHARACTERISTICS. THE CRITERIA ARE DEFINED FOR THE OPTIMAL DESIGN OF THE ONE-STAGE CENTRIFUGAL COMPRESSORS.

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Pages: 1986-1

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Details

  • Original title: TEMPERATURE BOUNDARY EFFECT OF THE LARGE HEAT PUMP CYCLE ON THE CHARACTERISTICS OF THE TURBOCOMPRESSOR.
  • Record ID : 1987-2378
  • Languages: English
  • Source: Progress in the design and construction of refrigeration systems.
  • Publication date: 1986/08/05
  • Document available for consultation in the library of the IIR headquarters only.

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