• DocumentCode
    2771074
  • Title

    Vibrational diagnostics and prediction of technical state of aviation turbine coolers

  • Author

    Losiev, Boris M.

  • Author_Institution
    Military Dept., Moscow Aviation Inst., Russia
  • fYear
    1995
  • fDate
    18-21 Jul 1995
  • Firstpage
    42461
  • Lastpage
    42468
  • Abstract
    Transfer of aviation aggregates to exploitation according to their technical state anticipates exploitation until reaching the limit of their service life. For turbine coolers (TC) with bearings, usual signs of technical state (TS) considered are: concentration of metallic particles in lubrication oil, axial and radial gaps, vibrations, etc. This report considers bands of vibrational spectrum, which are maximally varied depending upon object´s operating age. Presented is a formal method of forming of vibration sign space. It is based on computer search of vibrational spectrum bands of several objects of one type (and with the same operating age as well). In such a way a “teaching process” was performed for spectral bands, which have maximal variation depending upon the object´s operating age. Results were extended to general objects´ population
  • Keywords
    aerospace propulsion; aircraft; aircraft testing; cooling; gas turbines; life testing; vibration measurement; aviation turbine coolers; operating age; service life; teaching process; vibration sign space; vibrational diagnostics; vibrational spectrum; Aggregates; Education; Lubricating oils; Petroleum; Prediction methods; Shafts; Signal analysis; State estimation; Testing; Turbines;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 1995. ICIASF '95 Record., International Congress on
  • Conference_Location
    Wright-Patterson AFB, OH
  • Print_ISBN
    0-7803-2088-3
  • Type

    conf

  • DOI
    10.1109/ICIASF.1995.519110
  • Filename
    519110