Series of diagnostic indicators of gearbox teeth wear in aircraft gas turbine engines
Sundukov A.Y., Shakhmatov Y.V.
Method of constructing diagnostic models of aircraft hydraulic systems in an analytic form
Kovalev M.A., Borodkin G.V., Khablo I.I.
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.
The method of providing heat traceability of wireless devices at the stage of project
Uvaysov S.U., Yurkov N.K.
Mathematical model of the inline sensor based on matrix photodetector
Kornilin D.V.
Numerical study of possibility of reliable diagnostics of gas turbine engine by gasdynamic parameters using a linear mathematical model
Gerasimov A.B., Sundukov M.Y.
Vibrodiagnostics of turboprop engine gearbox wear
Sundukov A.Y., Sundukov Y.V., Plotnikov S.M.
The device for the determination of blades oscillation parameters based on nonlinear approximation of primary transducers signals
Danilin A.I., Chernyavskiy A.Z., Danilin S.A.
Measurament of characteristics and spectral structure of laser plasma
Timchenko P.E., Marinin V.L.
Complex failure analysis of aero engine compressor blades
Sachin V.M., Tumanov N.V., Lavrentyeva M.A., Cherkasova S.A.
Identifying the causes of excessive vibration in gas turbine engines in the course of their rig tests
Sundukov A.Y., Sundukov Y.V., Plotnikov S.M.
Building a diagnosis face gas dynamic seals
Falaleev S.V., Vinogradov I.S., Midyukin V.V.
Tooling system of express assessment of explosive military equipment objects after hitling effects
1 1., 1 1.
Imitation models of aircraft hydraulic units with account for typical faults
Gareyev A.M., Popelnyuk I.A., Stadnik D.M.
Investigation of the vibration behavior of a gas turbine engine in icing conditions
Danilkin S.Y., Teleshev V.A.
Discrete phase converters moving elements rotating units power units
Danilin A.I., Grechishnikov V.M.
Laser vibrating method of gluing shells defects detecting
1 1., 1 1., 1 1., 1 1., 1 1.
Analysis of the accuracy of autonomous navigation of the space robot in the diagnosis of the technical condition of an orbital object
Golyakov A.D., Fominov I.V., Korolev S.Y.
Perfection of methods of conducting resonance tests of rotor blades being part of the engine
Khorikov A.A., Danilkin S.Y., Redkin D.A.
Research of textural features for the diagnostics of nephrological diseases using ultrasound images
Gaidel A.V., Larionova S.N., Khramov A.G.
The devices for the diagnosis and control of turbine blades deformative condition during operation
Danilin A.I., Chernyavskiy A.G., Kapustin A.S.
Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor
Posadov V.V., Remizov A.E.
Thermal medical software hardware-based thermal imager COX CX - 320U
Davydov I.E., Agafonov A.N.
Diagnostics of computer modules of the Superjet-100 aircraft using the method of boundary scan
Grechishnyikov V.M., Kuritsky A.A., Manuilov I.Y.
Current state of the theory and practice of circuit wiring control and testing of the avionics of rocket fairings of middle-class launch vehicles
Koptev A.N., Gulyaev A.A.
Calculating the dynamic error in measurement of electrohydromechanical system parameters, taking into account the operating speed of sensors
Gareyev A.M., Gimadiev A.G., Stadnik D.M., Popelnyuk I.A.
Development of the criteria of analyzing the stress-strain state of gas turbine engine parts in the elastoplastic range
Bukaty A.S., Bukaty S.A.
Parameters transducers of the blade’s dynamic movements of turbounits based on nonlinear approximation of primary signals
Chernyavskiy A.Z., Danilin A.I., Danilin S.A.
Applied problems in the theory of diagnostic process for aircraft flight-navigation complexes
Koptev A.N., Kirillov A.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.
Using the theory of dynamic analogies for modelling automated manufacturing systems
Gareyev A.M., Koptev A.N., Gareyev T.M.
Control of the aircraft hydraulic system technical conditions on the basis of monitoring viscidity values and purity level of fluid power
Kovalev M.A., Borodkin G.V.
Flight-navigation complex diagnostics at the aircraft manufacture stage
Koptev A.N., Kirillov A.V.
1 - 33 of 33 Items

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