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
Link To Document :
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