• DocumentCode
    2903638
  • Title

    Fault diagnostics on jet engine starting

  • Author

    Liu, H.Z. ; Wang, H.M. ; Ni, X.Q.

  • Author_Institution
    Beijing Univ. of Aeronaut. & Astronaut., China
  • fYear
    1991
  • fDate
    27-31 Oct 1991
  • Firstpage
    392
  • Lastpage
    396
  • Abstract
    To investigate jet engine starting, a series of engine parameters must be evaluated. The measurements of rotor speed, fuel flow rate, fuel combustion, and gas temperature must be taken in real time. A dynamic measurement system was used to evaluate the starting performance, and to diagnose faults during starting. The dynamic measurement system contained a photoelectric system and a fast thermocouple used to detect and inspect the fault symptoms during starting. As a result, the starting operation quality to be assessed can be determined and improved. The experiment was completed on a sea-level test bench for a small single spool jet engine
  • Keywords
    aerospace engines; aerospace testing; combustion; fault location; flames; photodetectors; starting; combustion; dynamic measurement; fault diagnosis; flame signal; fuel combustion; fuel flow rate; gas temperature; ignition; jet engine starting; photoelectric system; real time; rotor speed; sea-level test bench; single spool jet engine; thermocouple; Aerodynamics; Combustion; Extraterrestrial measurements; Fires; Frequency; Fuels; Ignition; Jet engines; Phototransistors; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 1991. ICIASF '91 Record., International Congress on
  • Conference_Location
    Rockville, MD
  • Type

    conf

  • DOI
    10.1109/ICIASF.1991.186262
  • Filename
    186262