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Modelling width of the spectral component of a gas-turbine engine gearbox output shaft speed
Sundukov A.E., Shakhmatov E.V.
Model of the turboprop engine reduction gear tooth harmonic spectral component
Sundukov A.E., Shakhmatov E.V.
New methods for identifying diagnostic indicators of the technical condition of aircraft gas turbine engine reduction gearboxes
Sundukov A.Y., Shakhmatov Y.V.
Series of diagnostic indicators of gearbox teeth wear in aircraft gas turbine engines
Sundukov A.Y., Shakhmatov Y.V.
Increasing the sensitivity and expanding the functionality of bipolar analysis of rotary machine vibrations
Sundukov A.E., Shakhmatov Y.V.
Simulation model of oscillations of the “sun gear – satellites” pair of turboprop engine planetary reduction gearbox in the presence of defects of tooth flanks
Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.
Calculation of lubricant flow in the slide bearing of the aviation engine reducer
Siluyanova M.V., Fertikov A.О.
Diagnostic methods and tools for condition-based maintenance of aircraft drives
Golovanov V.V., Vasilenko V.G., Zemskov A.A., Panov S.S., Emelianova A.A.
Diagnostic indicators of tooth flank wear based on the analysis of tooth spectral component parameters
Sunduckov A.E.
1 - 9 of 9 Items

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