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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.
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.
Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine
Belonozhkin V.V., Teslya D.N.
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.
Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade
Matveev V.N., Melnikov S.A., Popov G.M., Zubanov V.M., Kudryashov I.A., Shcherban A.I.
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.
Formation of a method of choosing rational values of ultralow power turbine parameters in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
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.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev 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.
Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading
Badamshin I.K.
Off-line long-life unservice close gas organic fuel-powered turbine
Arbekov A.N.
3D investigation of heat exchange and hydrodynamics of high pressure turbine nozzle block platforms with different cooling schemes
Gorelov Y.G., Ananyev V.V., Zolotuhina D.A.
Improvement of gas turbine engines due to isothermal expansion in the turbine
Muraeva M.A., Gorjunov I.M.
Design of the gas turbine engine rotor wheel with ceramic blades
Sapronov D.V., Reznik S.V.
Project of 30 000 h.p. power gas turbine
Zrelov V.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.
Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate
Kocherova E.E.
Mathematical models for evaluating the energy efficiency of ultralow power turbine drives
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Validation of CFD-models of gas turbine engine uncooled turbines
Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.
Application of thermoplastic hardening for restoration of fatigue durability of gas turbine disks
Vishnyakov M.A.
Design of bimetallic impeller for gas turbine
Magerramova L.A.
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.
Series of diagnostic indicators of gearbox teeth wear in aircraft gas turbine engines
Sundukov A.Y., Shakhmatov Y.V.
Development of methods of designing modern gas turbines
Inozemtsev A.A., Khairulin V.T., Tikhonov A.S., Samokhvalov N.Y.
Development of a virtual prototype of gasturbine engine at the stage of conceptual thermogasdynamic designusing the CAE-system «ASTRA»
Tkachenko A.Y., Krupenich I.N.
Problem of multistage compressor optimization while designing perspective gas turbine engines
Shabliy L.S.
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.
Simulation of aircraft multistage axial turbine working processes taking into account over-shroud leakage flows and blading inflows
Baturin O.V., Popov G.M., Kolmakova D.A.
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.
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.
About the thermal protection of the oil cavities for designing gas turbine engines
Tryanov A.Y., Grishanov O.A., Vinogradov A.S.
Wearability, wearproof and heat-shielding coverings for details of the gas path of the turbine, the compressor and the chamber of combustion of gas turbine engine
Barvinok V.A., Shitarev I.L., Bogdanovich V.I., Dokukina I.A., Karasev V.M.
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.
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.
Calculation of flow characteristics of liquid fuel supplied through pressure jet atomizers of small-sized gas turbine engines
Gurakov N.I., Zubrilin I.A., Hernandez Morales M., Yakushkin D.V., Didenko A.A., Matveev S.G., Komisar Y.V.
Method for optimizing mass and size characteristics of a high-pressure turbine disk
Siluyanova M.V., Grunin A.N., Alendar A.D., Kandaurov S.K.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
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.
Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber
Matveev S.G.
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.
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.
Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor
Posadov V.V., Remizov A.E.
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.
Possibility of using a bi-directional impulse turbine in a thermo-acoustic engine
Dovgjallo A.I., Shimanov A.A.
Problems of ultralow power turbine design in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Thermoplastic strengsening of blades aircraft gas turbine engines
Krotinov N.B.
Working conditions analysis of rotor supports bearings in aviation gas turbine engines and energetic units structure
Zrelov V.A., Makarchuk V.V., Prodanov M.E., Sudarev A.A.
MR vibration dampers development to reduce vibration and noise in gas turbine locomotive and their equivalent vibration tests
Ermakov A.I., Lazutkin G.V., Parovay F.V., Troynikov A.A.
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.
Aerodynamic improvement of GTE compressors by space profiling of blade vanes
Gerasimenko V.P., Shelkovsky M.Y.
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.
Development of turbopump unit design for hydrogen liquid-propellant rocket engines without generators developed at the design bureau of chemical automation
Dmitrenko A.I., Ivanov A.V., Rachuk V.S.
Optimization characteristics of rotor-support system from NK-14ST free power turbine with consider statics and dynamics propertys
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.
Criteria of discrete phase control of blade working condition and their feasibility in systems of turbine driven set automatic control
Danilin A.I., Tchernyavsky A.Z.
Thermal state of a groind-use gas turbine engine stator
Grechishnikov O.V., Balakin A.Y., Roslyakov A.D.
Mathematical model of turbofan engine weight estimation taking into account the engine configuration and size
Avdeev S.V.
Algorithm for predicting the vibrational state of a turbine rotor using machine learning
Bolotov M.A., Pechenin V.A., Pechenina E.J., Ruzanov N.V.
Gas turbine engine rotor bearings electrical current damage on the base of NK-family engines for electrical generator drive
Nazdrachev S.V.
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.
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.
Analysis of schemes of correction of dynamic characteristics of acoustic probes for measuring pressure pulsations in a gas turbine engine
Gimadiev A.G., Bystrov N.D., Dyagileva E.S.
Assessment of gas turbine engine airfoil surface microstructure
Nosov N.V., Abramov A.D., Kosulin S.I.
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.
Computer-aided design of aircraft gas turbine engines and selection of materials for their main parts
Akhmedzyanov D.A., Kishalov A.E., Markina K.V.
Experimental research of heat exchange in a plane channel using the regular thermal regime mrthod with different Biot numbers
Kolesova E.G., Veretennikov S.V., Zhornik M.N.
Installation for strengthening local thermoplastic turbulent disc
Krutsilo V.G., Nikishov O.V.
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.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
Defects of shrouded blade platforms of high-temperature gas turbines
Belousov A.I., Nazdrachyov S.V.
Vortex effect and intensification of heat and mass transfer in cell energy technology
Piralishvily S.A., Veretennikov S.V.
Compulsory ignition of fuel-air mixture in small-sized gas turbine engine combustion chambers
1 1., 1 1., 1 1.
Features of designing gas turbine of complex cycle GT24
1 1.
Estimation the factors, make the greatest influence on reliability parametres of a GTD disk with a glance sudden failures
Belousov A.I., Gritsin A.V.
Problems of making auxiliary gas turbine engines with gas bearing rotors
Ponomaryov B.A., Gavrilov V.V.
Estimation of parameters of a pulse detonation engine (РDЕ)
Anakin A.T., Tsybizov Y.I.
Сalculation of characteristics of atomization of liquid supplied at an angle to the flow direction and justification of adjusting the angle of the nozzle inclination relative to the gas flow
Teslya D.N., Mityaev S.V., Drobyshev P.A.
Formation of film cooling on the turbine blade back and pressure side in the case of using V-shaped dimples
Lebedev V.V., Lebedev O.V., Remizov A.E.
Determination of a rational combination of the radial turbine basic parameters with an allowance for strength, technological and other constraints
Baturin O.V., Shabliy L.S.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades
Sazonov M.B., Solovatskaya L.V.
Micro gas turbine engine imitation model
Kuznetsov A.V., Makaryants G.M.
Development of an exhaust air turbine engine
Yeliseev Y.S., Fedorchenco D.G., Tsibizov Y.I., Tyulkin D.D., Tkachenko A.Y.
Conversion of gas turbine engine oil system
Boev A.A., Grishanov O.A.
Simulation of aerodynamic structure of the flow in the combustion chamber of a small-size gas turbine engine with the help of CAE–systems
Matveev S.G., Orlov M.Y., Abrashkin V.Y., Zubrilin I.A., Matveev S.S.
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.
Research of gas turbine engine operation in dust-filled atmosphere
Abdullin B.R., Akmaletdinov R.G., Goumerov K.S., Nigmatullin R.R.
Combined calculation of gas generators of small GTE in package ANSYS CFX
Matveev S.G., Orlov M.Y., Matveev S.S., Zinkovskii V.S., Krivtsov A.V.
A technique to estimate efficiency of turbine underplatform friction dampers
Nikhamkin M.S., Sazhenkov N.A.
Dependence of required turbine inlet temperature at cruise mode of long-term flight on bypass ratio
Rybakov V.N.
Discrete phase converters moving elements rotating units power units
Danilin A.I., Grechishnikov V.M.
Effect of cavity width on performance of pre-swirl systems
Didenko R.A., Karelin D.V., Ievlev D.G., Lebedev V.V., Belousova E.V.
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