• DocumentCode
    554602
  • Title

    Effects of intercooling and recuperation on turbofan engine performance

  • Author

    Gong Hao ; Wang Zhan-xue

  • Author_Institution
    Sch. of Power & Energy, Northwestern Polytech. Univ., Xi´an, China
  • Volume
    5
  • fYear
    2011
  • fDate
    12-14 Aug. 2011
  • Firstpage
    2482
  • Lastpage
    2485
  • Abstract
    An overall performance simulation model of the intercooled recuperative aero-engine was built, and an overall performance simulation program was developed. Then, analysis of the effects of intercooling and recuperation on the thermodynamic cycle parameters and performance parameters of the turbofan engine can be carried out. The result indicates that the turbofan engine performance can be improved with the proper use of intercooling and recuperation. With the same thermodynamic cycle parameters, the thermal efficiency and the net thrust is larger, while the specific fuel consumption is lower. To gain the same performance, lower overall pressure ratio and lower bypass ratio can be chosen for the intercooled recuperative aero-engine.
  • Keywords
    aerospace engines; cooling; energy consumption; aero-engine performance; fuel consumption; intercooled recuperative aero-engine; intercooling; recuperation; thermal efficiency; thermodynamic cycle parameters; turbofan engine performance; Business process re-engineering; Educational institutions; Engines; Heating; Ice; Ocean temperature; Thermodynamics; effect; intercooling; performance; recuperation; turbofan engine;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electronic and Mechanical Engineering and Information Technology (EMEIT), 2011 International Conference on
  • Conference_Location
    Harbin, Heilongjiang, China
  • Print_ISBN
    978-1-61284-087-1
  • Type

    conf

  • DOI
    10.1109/EMEIT.2011.6023545
  • Filename
    6023545