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Validation of the “stage – diffuser” system numerical study and its use for design modernization
Cherkasova M.G., Semakina E.Y., Chernikov V.A.
Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine
Belonozhkin V.V., Teslya D.N.
Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
Blinov V.L., Zubkov I.S.
Features of design calculation of compressor spool flow path of a twin-shaft gas turbine engine core on the basis of 1D and 2D models of their working process
Matveev V.N., Goriachkin E.S., Popov G.M., Baturin O.V., Kudryashov I.A.
Gasdynamic and strength improvement of the axial flow turbine of a helicopter gas turbine engine
Goriachkin E.S., Popov G.M., Matveev V.N., Shcherban A.I., Kudryashov I.A., Melnikov S.A.
Special aspects of numerical simulation of a two-stage axial-flow compressor with defective blades
Blinov V.L., Zubkov I.S., Iskortsev E.Y., Belyaev O.V., Plishkin P.I.
Structure and physico-mechanical properties of heat resistant gazoplazmennyh coating NiCrCoAlY/ZrO2 for turbine blades of gas turbine engines
Tarasenko Y.P., Tsareva I.N., Berdnik O.B., Fehl Y.A.
Series of diagnostic indicators of gearbox teeth wear in aircraft gas turbine engines
Sundukov A.Y., Shakhmatov Y.V.
Investigation of the influence of broadband mechanical disturbances on the quality of recording interference patterns of GTE-wheel oscillations using a digital speckle pattern interferometer
Ivchenko A.V., Safin A.I.
Neural network controller of a gas turbine plant low emission combustor
Avgustinovich V.G., Kuznetsova T.A., Sukharev A.A.
Method of scanning thin surfaces in repairing gas turbine blades
Kotlyar D.I., Lomanov A.N.
Project of 30 000 h.p. power gas turbine
Zrelov V.A.
JSC “ODK” experience in implementing digital twin technologies in the design of gas turbine engines
Vinogradov K.A., Nikulin A.S., Shmotin Y.N.
Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing
Parovay E.F.
Development of elements and parameters of LNG fuel system with cryogenic piston pump and gas receiver for road gas turbine locomotive
Bukin V.A., Rudenko V.F.
Validation of CFD-models of gas turbine engine uncooled turbines
Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.
Design of bimetallic impeller for gas turbine
Magerramova L.A.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
Application of thermoplastic hardening for restoration of fatigue durability of gas turbine disks
Vishnyakov M.A.
Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate
Kocherova E.E.
Improvement of gas turbine engines due to isothermal expansion in the turbine
Muraeva M.A., Gorjunov I.M.
Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading
Badamshin I.K.
Design of the gas turbine engine rotor wheel with ceramic blades
Sapronov D.V., Reznik S.V.
Off-line long-life unservice close gas organic fuel-powered turbine
Arbekov A.N.
Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle
Grigoriev V.A., Kuznetsov S.P.
Gas turbine engine designing on the basis of a unified gas generator
Rybakov V.N.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Optimization features of the working process parameters of bypass engine on the basis of given gas generator
Rybakov V.N.
Problem formulation of bypass engine parameters optimization with a preselected gas generator
Kuzmichev V.S., Kulagin V.V., Tkachenko A.Y., Krupenich I.N., Rybakov V.N.
Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine
1 1., 1 1.
Evaluating the possibility of using low-temperature thermal energy in liquefied natural gas complexes
Dovgjallo A.I., Sarmin D.V., Uglanov D.A., Shimanov A.A.
Conditions of compatibility of compressor and turbine used as part of a gas generator required to ensure turbine operability
Grigoriev A.V., Ilyushin M.Y., Mitrofanov V.A., Rassokhin V.A., Rudakov O.A., Solovieva A.V.
The task of creating the bypass engines of various thrust levels using the given gas generator
Kocherov E.P., Kuzmichev V.S., Kulagin V.V., Fedorchenko D.G.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Comparative analysis of facilities for the implementation of thermoplastic hardening blades of gas turbine engines and pumping units
Karpov A.V.
Numerical simulation of gas temperature spatial distribution in a full-size gas turbine combustor and its one-burner sector
Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.
Numerical simulation of gas temperature spatial distribution in a one-burner sector of a gas turbine combustor with uncertain initial conditions of fuel atomization
Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.
The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters
Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.
Life of gas turbine engine components under corrosive exposure
Pivovarova M.V., Gladkiy I.L.
Calculation of lubricant flow in the slide bearing of the aviation engine reducer
Siluyanova M.V., Fertikov A.О.
Optimization of fuel distribution in the afterburner of a gas turbine engine
Nelyubin V.R.
Development of a multiuser system web-interface as a tool of using mathematical packages for solving engineering tasks
Danilenko A.N., Zhdanov I.A.
Constructing 3D fan blade models in CAD-system on the basis of coordinate measuring techniques
Arkhipov A.N., Ravikovich Y.A., Fedorov I.M., Kholobtsev D.P.
Research of hydrodynamic processes in the lubrication system of gas turbine engines
Gulienko A.I., Shchurovskiy Y.M.
Calculation of exciting aerodynamic load on a gas turbine engine compressor blade induced by the effect of a non-uniform gas flow
Ermakov A.I., Shklovets A.O., Fedorchenko D.G.
The defectoscopy of the fatigue cracks in the gas turbine parts by means of eddy-current method
Porter A.M., Bukatyi S.A., Leshin D.P., Vasilchuk M.V., Galickyi A.A.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
Modelling of an ejector for turbine aeroengines for application in performance synthesis tools
Georgi J., Staudacher S., Falaleev S.V.
Compulsory ignition of fuel-air mixture in small-sized gas turbine engine combustion chambers
1 1., 1 1., 1 1.
the research of the influence of the maximal stress duration in the cycle of loading upon the low-cycle fatigue and the long-term strength of the turbine shaft made of the material ЭИ 961-Ш
1 1., 1 1., 1 1.
Investigation of the characteristics of the component of vibration of gas turbine engine gearbox that causes fatigue failures of its structural elements in case of tooth flank wear
Sundukov A.E.
Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines
Kuz'michev V.S., Omar H., Tkachenko A.Y., Bobrik A.A.
Theory of gas turbine engine optimal gas generator
Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Assessment of gas turbine engine airfoil surface microstructure
Nosov N.V., Abramov A.D., Kosulin S.I.
Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor
Posadov V.V., Remizov A.E.
The concept of matching the joint operation of the combustion chamber, the compressor and the turbine
Grigoriev A.V., Golubchikov P.P., YIlushin M.Y., Rudakov O.A., Solovieva A.V.
Research of the validity of forecasting low cycle durability of gas turbine engine parts based on Manson’s equation
Porter А.M., Bukatyi S.A., Leshin D.P.
Choosing the optimal method of the centrifugal loads modeling using 2D FE models of the compressor’s disks slots
Balyaeva N.N., Guschin A.Y.
Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine
Kuzmichev V.S., Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Kulagin V.V.
Estimate of key parameters of a gas turbine engines with application of the modelling procedure of the equilibrium state of homogeneous mixture of hydrocarbon fuel combustion products
Boldyrev O.I., Gorynov I.M.
The influence of operational and technological factors on the dynamic parameters of elastic elements of elastic damping rotor supports
1 1., 1 1., 1 1.
Methodology complex of hardware-in-the-loop functional modelling of gas turbines and its systems
1 1., 1 1., 1 1., 1 1., 1 1.
Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers
Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.
Application of the vacuum casting technology in the production of small-size gas turbine engine blade machines
Faramazyan A.M., Remchukov S.S., Demidyuk I.V.
Technology of low-emission fuel combustion and conceptual structure of the combustion chamber of a gas-turbine power plant
Tsybizov Y.I., Tyulkin D.D., Vorotyntsev I.E.
Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber
Matveev S.G.
Automated construction of a fan blade model according to data of CAD profile measurements
Arkhipov A.N., Bugrjashova E.V., Ravikovich Y.A., Savin R.A., Terentjev V.V., Shevjakov A.O.
Improvement of friction units of power plants by aplying ceramic composite spray coatings
Siluyanova M.V., Fertikov A.O.
Micro gas turbine engine imitation model
Kuznetsov A.V., Makaryants G.M.
Investigation of the causes of crack origination in the inner casing of NK-86 gas turbine engine combustion chamber
Kocherova Е.Е.
Selection of optimal configuration and workflow parameters of autonomous micro gas turbine plant
Baturin O.V., Smirnova Y.D.
Studying the influence of the gas-dynamic non-stationary factors on the mathematical modelling of the gas turbine engines nonsetup work modes
Kofman V.M.
Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system
Davydov D.P.
The calculated study of fluid structure in a hub an axial aviation turbine
1 1., 1 1.
Working out the system of technical decisions for ensuring the reliability of friction units of gas-turbine engines
Gromakovsky D.G., Kovshov A.G., Ibatullin I.D.
Problems of making auxiliary gas turbine engines with gas bearing rotors
Ponomaryov B.A., Gavrilov V.V.
On the issue of research of the properties of the heat-resistant nickel single-crystal superalloys
Tikhomirova E.A., Zhivushkin A.A., Getsov L.B., Rybnikov A.I.
Application of additive technology of selective laser melting (SLM) in designing a low emission combustion chamber of a gas turbine plant
Yeliseev Y.S., Fedorchenko D.G., Golanov S.P., Tsibisov Y.I., Tyulkin D.D., Vorotyntsev I.E., Ivchenko A.V.
Development of a procedure for the synthesis of a micro gas turbine engine neural controller with account for fuel consumption constraints
Kuznetsov A.V., Makaryants G.M.
Optimization of ducted counter–rotating fan blades on the basis of solving a 3d inverse problem with the aim of improving fan gasdynamic characteristics
Mileshin V.I., Pankov S.V., Fateyev V.A., Shchipin S.K.
Evaluation of low cycle fatigue based on the use of Coffin-Manson dependence under zero-to-“soft” loading cycle
Pavlov V.F., Kirpichyov V.A., Kocherova E.E., Zlobin A.S.
Using the «virtual engine» software in automatic control system of gas turbine engine
Golberg F.D., Gurevich O.S., Petukhov A.A.
Development and analysis of screw restrictor hydraulic characteristics in the air bleed valve control unit of a gas turbine engine
Gimadiev A.G., Makaryants G.M., Blyumin K.V., Dudnichenko I.M.
Modification of the starter turbine disk for blade containment certification tests
Karimbaev K.D., Sapronov D.V.
Experience of operational development of starting characteristics of the APU combustion chamber
Chechulin A.Y.
Computer-aided system of virtual gas turbine engine testing
Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Ostapuk Y.A., Filinov E.P.
Fulfilment of initial design level of gas turbine engine using the methods of «ASTRA» CAE system
Kuzmichev V.S., Krupenich I.N., Tkachenko A.Y.
A technique to estimate efficiency of turbine underplatform friction dampers
Nikhamkin M.S., Sazhenkov N.A.
Methods and means of aircraft gas turbine engine conceptual design underlying the CAE system «ASTRA»
Kuzmichev V.S., Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Kulagin V.V.
Rotor in gas bearings dynamics experiment-calculated investigation
Temis Y.M., Temis M.Y., Egorov A.M., Gavrilov V.V., Ogorodov V.N.
Seal designing in a structure of the cooling system in gas turbine engine
Vinogradov A.S., Myatlev A.S.
Aspects of simulating stable low-cycle fatigue crack growth in the main parts of aircraft gas turbine engines
Ryabov A.A., Mokhov K.Y., Voronkov O.V., Kudryavtsev A.Y., Museev A.A.
Gas turbine engine dynamic model based on variable-memory LSTM architecture
Kuznetsov A.V., Makaryants G.M.
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.
Testing of gas turbine engine bearing oil supply through an oil-catch ring
Boev A.A., Petrukhin A.G., Mikhailov A.A.
Research of toxic substances emission during water injection into a combustion chamber
Mingazov B.G., Mukhametgaliev T.H.
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.
Research of gas turbine engine operation in dust-filled atmosphere
Abdullin B.R., Akmaletdinov R.G., Goumerov K.S., Nigmatullin R.R.
Causes of failures of rolling bearings
Zvonarev S.L., Zubko A.I.
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