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EXPERIMENTAL INVESTIGATION ON R134A AIRBORNE VAPOR-COMPRESSION REFRIGERATION SYSTEM

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【作者】 李运祥潘泉刘娟

【Author】 Li Yunxiang 1 , Pan Quan 1 , Liu Juan 2 ( 1.Collage of Automation , Northwest Polytechnical University , Xi′an , 710072 , P.R.China ; 2.College of Aerospace Engineering , Nanjing University of Aeronautics and Astronautics , Nanjing , 210016 , P.R.China )

【机构】 Collage of Automation,Northwest Polytechnical UniversityCollege of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics

【摘要】 The airborne high power electrical equipments have been widely used in modern aircrafts , which consequently causes the dramatic increase of heating load up to dozens of kilowatts.Accordingly , vapor-compression refrigeration system ( VCRS ) with lower engine bleed air and larger refrigeration capacity has been paid much attention in recent years.Therefore , based on the analysis of the characteristics of VCRS , an experiment system of VCRS using R134ais set up to simulate operation performances.The influences of different parameters including evaporation pressure , condensing pressure , refrigerant mass flow rate and compressor rotation speed are also investigated.The impacts of different parameters on the system performance are various.This work can help to establish the specific control law under different work conditions.

【Abstract】 The airborne high power electrical equipments have been widely used in modern aircrafts , which consequently causes the dramatic increase of heating load up to dozens of kilowatts.Accordingly , vapor-compression refrigeration system ( VCRS ) with lower engine bleed air and larger refrigeration capacity has been paid much attention in recent years.Therefore , based on the analysis of the characteristics of VCRS , an experiment system of VCRS using R134ais set up to simulate operation performances.The influences of different parameters including evaporation pressure , condensing pressure , refrigerant mass flow rate and compressor rotation speed are also investigated.The impacts of different parameters on the system performance are various.This work can help to establish the specific control law under different work conditions.

  • 【文献出处】 Transactions of Nanjing University of Aeronautics & Astronautics ,南京航空航天大学学报(英文版) , 编辑部邮箱 ,2013年01期
  • 【分类号】TB657
  • 【下载频次】39
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