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New methods for identifying diagnostic indicators of the technical condition of aircraft gas turbine engine reduction gearboxes
Sundukov A.Y., Shakhmatov Y.V.
Standardization of diagnostic indicators of gearbox teeth wear in aircraft gas-turbine engines
Sunduckov A.Y., Shakhmatov Y.V.
Calculation of lubricant flow in the slide bearing of the aviation engine reducer
Siluyanova M.V., Fertikov A.О.
Carbothermal synthesis of fine-dispersed tantalum monocarbide powder
Simonenko Y.P., Ignatov N.A., Yezhov Y.S., Sevastyanov V.G., Meshalkin V.P., Kuznetsov N.T.
Refining methods of vibration diagnostics of wear of turbo-prop engine differential speed reduction unit gear teeth
Avramenko A.A., Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.
Vibration resistance problem for a space vehicle with single-degree-of-freedom powered gyroscopes
Filippov Y.I., Peresypkin K.V.
Formulas of reducing engine environmental performance and combustion characteristics to standard atmospheric conditions
Grigoriev A.V., Kosmatov A.A., Rudakov O.A., Solovieva A.V.
PDM implementation efficiency in mechanical industry
1 1., 1 1., 1 1.
A new mathematical tool for modelling the processes in fuel sprays
Sazhin S.S., Sobolev V.A., Shchepakina E.A.
Identification and procedure of reducing periodic noise of internal combustion car engines using the active compensation method
Vasilyev A.V., Andreyev S.S., Butsayev I.V., Pimkin V.V.
Construction of detailed kinetic mechanisms of forming for five ring PAH and their reduction for use in modern CAE systems
Matveev S.G., Chechet I.V.
Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor
Shipov M.G., Steklova A.A., Davydov A.A.
Assessing reduction gear mass in the problem of optimizing parameters of the working process of a turboprop engine at the initial design stage
Grigoryev V.A., Zagrebelnyi A.O., Prokaev A.S., Kuznetsov S.P.
Using signals from the gas-turbine engine shaft speed sensor in the diagnosis of the technical condition of its reduction gearbox
Avramenko A.A., Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.
Numerical solution of a production planning problem in case of dynamic labor input reduction
Pavlov O.V., Ryasnaya T.N.
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.
Analysis of the effect of technological parameters of rolling on the optimization of rolling milladjustment programs
Tlustenko S.F.
1 - 17 of 17 Items

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