Abstract We consider a method for diagnostics of the engine flow passage technical status of a maneuverable aircraft operating in a wide range of altitudes and speeds; the behavior of measured parameter deviations from throttle characteristics and calculated characteristics of the flow passage units from their initial values is used for diagnostics. We present the methods for determining these deviations as well as flight conditions and engine operation modes at which diagnostics is made possible.
Choice of flight conditions and modes of engine operation for its diagnostics
Russian Aeronautics (Iz VUZ) ; 52 , 4 ; 419-425
2009-12-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Choice of flight conditions and modes of engine operation for its diagnostics
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