Search

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.

(Rus)

Vol 10, No 1 (2011)

Using the energy of gas differential pressure in electromagnetic injectors for improved breathing of spark-ignition internal combustion engine cylinders

Shishkov V.A.

(Rus)

Vol 14, No 1 (2015)

Vortex cleaning of fuel tank pressurant gas

Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.

(Rus)

Vol 22, No 3 (2023)

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.

(Rus)

Vol 21, No 1 (2022)

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.

(Rus)

Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle

Grigoriev V.A., Kuznetsov S.P.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Shock wave profiles in relaxing gas with external energy source

Anchikov D.A., Galimov R.N., Zavershinskii D.I., Makaryan V.G., Molevich N.E.

(Rus)

Vol 13, No 1 (2014)

Research of the mechanism of shock-inertial deposition of dispersed particles from a gas flow

Usmanova R.R., Zhernakov V.S.

(Rus)

Vol 20, No 4 (2021)

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.

(Rus)

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.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Gas turbine engine designing on the basis of a unified gas generator

Rybakov V.N.

(Rus)

Vol 23, No 1 (2024)

Development of a mathematical model of the internal structure of a granular heat accumulator for launching a mono-fuel gas generator

Zrelov V.A., Lykin A.Y.

(Rus)

Vol 21, No 4 (2022)

Series of diagnostic indicators of gearbox teeth wear in aircraft gas turbine engines

Sundukov A.Y., Shakhmatov Y.V.

(Rus)

Vol 10, No 5 (2011)

Vortex gas wind-driven power plant for supplying compressor stations with electrical energy

Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Optimization features of the working process parameters of bypass engine on the basis of given gas generator

Rybakov V.N.

(Rus)

Fluctuations of pressure in rail gas injection of engines with spark ignition

Shishkov V.A.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

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.

(Rus)

Vol 9, No 1 (2010)

Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine

1 1., 1 1.

(Rus)

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.

(Rus)

Vol 23, No 1 (2024)

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.

(Rus)

Vol 21, No 4 (2022)

Resistance of products made of steel 20GL to sulfide stress corrosion cracking

Blazhnov N.M., Borisenkova E.A., Khardin M.V.

(Rus)

Vol 19, No 2 (2020)

Development and research of a gas stamping device for making hollow products from a pipe billet

Botashev A.Y., Bayramukov R.A., Bisilov N.U., Dzhumanazarov E.K., Malsugenov R.S.

(Rus)

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.

(Rus)

Vol 23, No 1 (2024)

Neural network controller of a gas turbine plant low emission combustor

Avgustinovich V.G., Kuznetsova T.A., Sukharev A.A.

(Rus)

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.

(Rus)

Vol 22, No 4 (2023)

Method of scanning thin surfaces in repairing gas turbine blades

Kotlyar D.I., Lomanov A.N.

(Rus)

On selection of automatic control system for crvogenic fuel gas turbine engine

Bukin V.A.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

Project of 30 000 h.p. power gas turbine

Zrelov V.A.

(Rus)

Vol 22, No 4 (2023)

JSC “ODK” experience in implementing digital twin technologies in the design of gas turbine engines

Vinogradov K.A., Nikulin A.S., Shmotin Y.N.

(Rus)

Vol 21, No 2 (2022)

Validation of the “stage – diffuser” system numerical study and its use for design modernization

Cherkasova M.G., Semakina E.Y., Chernikov V.A.

(Rus)

Comparative analysis of facilities for the implementation of thermoplastic hardening blades of gas turbine engines and pumping units

Karpov A.V.

(Rus)

Vol 11, No 2 (2012)

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.

(Rus)

Vol 21, No 2 (2022)

Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing

Parovay E.F.

(Rus)

Joint work of units and characteristics of elements gas the equipment for the engine of internal combustion with spark ignition

Shishkov V.A., Lesnih U.I.

(Rus)

Vol 16, No 4 (2017)

Application of open-source software for industrial problems of vehicle lift-off gas dynamics

Abdurashidov T.O., Osipov A.V., Korchagova V.N., Kraposhin M.V., Smirnova Y.V., Strizhak S.V.

(Rus)

Vol 11, No 2 (2012)

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.

(Rus)

Vol 19, No 4 (2020)

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.

(Rus)

Vol 18, No 3 (2019)

Life of gas turbine engine components under corrosive exposure

Pivovarova M.V., Gladkiy I.L.

(Rus)

Investigation of resonant oscillations working plates in experimental models of pneumatic valve

Zhuravliov О.A., Komarov S.Y., Makaryants G.M., Sergeev R.N., Harchikova J.V.

(Rus)

Vol 18, No 2 (2019)

Calculation of lubricant flow in the slide bearing of the aviation engine reducer

Siluyanova M.V., Fertikov A.О.

(Rus)

Vol 17, No 4 (2018)

Optimization of fuel distribution in the afterburner of a gas turbine engine

Nelyubin V.R.

(Rus)

Vol 17, No 2 (2018)

Development of a multiuser system web-interface as a tool of using mathematical packages for solving engineering tasks

Danilenko A.N., Zhdanov I.A.

(Rus)

Vol 16, No 3 (2017)

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.

(Rus)

Vol 15, No 4 (2016)

Mathematical modelling of the working process of a hot gas pressure feed system

Salich V.L.

(Rus)

Vol 10, No 6 (2011)

Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components

Titov B.A., Koltsov I.V.

(Rus)

Vol 14, No 3-1 (2015): Special Issue

Research of hydrodynamic processes in the lubrication system of gas turbine engines

Gulienko A.I., Shchurovskiy Y.M.

(Rus)

Vol 10, No 5 (2011)

Experimental study of swirled gas flow by the particle image velocimetry method

Knysh Y.A., Redkin Y.S., Dmitriev D.N.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

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.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Validation of CFD-models of gas turbine engine uncooled turbines

Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.

(Rus)

On the development of probes for measuring pressure pulsations in the gas-dynamic channel gas generator

Shorin V.P., Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A., Alexandrova T.G.

(Rus)

Mathematical modeling of processes of compression and expansion in the piston pump with a gas damper

Shcherba V.E., Pavlyuchenko E.A., Kuzhbanov A.K.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

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.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria

Tkachenko A.Y., Kuzmichev V.S.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Modelling of an ejector for turbine aeroengines for application in performance synthesis tools

Georgi J., Staudacher S., Falaleev S.V.

(Rus)

Vol 9, No 1 (2010)

Compulsory ignition of fuel-air mixture in small-sized gas turbine engine combustion chambers

1 1., 1 1., 1 1.

(Rus)

Vol 8, No 3-3 (2009): Special Issue

Cycle air heating system of gas pumping unit NEVA-25NK

1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

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.

(Rus)

Vol 8, No 2 (2009)

Analysis of temperature separation efficiency in vortex gas flows

Biryuk V.V., Kurnosov N.Y., Tarnopolsky A.V.

(Rus)

Mathematical model for calculating radial non-uniformity of the gas temperature field at the exit of small gas turbine engine combustion chambers

Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.

(Rus)

Vol 19, No 4 (2020)

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.

(Rus)

Vol 18, No 3 (2019)

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.

(Rus)

Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 18, No 2 (2019)

Theory of gas turbine engine optimal gas generator

Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.

(Rus)

Vol 17, No 4 (2018)

Оptimization of gas turbine aircraft engine control throughout the engine service life

Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.

(Rus)

Vol 17, No 2 (2018)

Development and research of a device for gas sheet stamping with a piston pressure multiplier

Botashev A.Y., Bayramukov R.A.

(Rus)

Vol 16, No 2 (2017)

Assessment of gas turbine engine airfoil surface microstructure

Nosov N.V., Abramov A.D., Kosulin S.I.

(Rus)

Vol 15, No 4 (2016)

Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor

Posadov V.V., Remizov A.E.

(Rus)

Vol 10, No 7 (2011)

Gas mass spectrometer with a non-linear ion mirror

Pijakov I.V., Rodin D.V.

(Rus)

Vol 14, No 3-1 (2015): Special Issue

Method of investigating the elastohydrodynamic contact in slide bearings with compressible and incompressible lubrication

Temis M.J.

(Rus)

Vol 10, No 5 (2011)

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.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

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.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Method of gas turbine malfunction diagnostics using hybrid intellectual systems

Antropov P.G., Dolinina O.N., Shvarts A.Y.

(Rus)

Development of techniques and calculation program heterogeneous gas measurement circuits

Gimadiyev A.G., Bystrov N.D., Ustinov A.

(Rus)

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.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

Methods of increase of wear resistance and vibroakusticheskikh of parameters of knots of the friction of space equipment

Gromakovsky D.G., Kovshov A.G., Kotcherov E.P., Makaryants M.V.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

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.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

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.

(Rus)

Vol 10, No 2 (2011)

Design of bimetallic impeller for gas turbine

Magerramova L.A.

(Rus)

Vol 9, No 1 (2010)

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.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

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.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Increasing efficiency of pressurization of the rocket tanks in the flight

1 1., 1 1.

(Rus)

Vol 8, No 1 (2009)

Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle

Shustov S.A.

(Rus)

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.

(Rus)

Vol 20, No 3 (2021)

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.

(Rus)

Vol 19, No 2 (2020)

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.

(Rus)

Vol 10, No 6 (2011)

Peculiarities of starting a spark-ignition gas fuel internal combustion engine

Shishkov V.A.

(Rus)

Surging and auto-off the helicopter engine at start-up unguided missile from launchers

Prokopiev A.L., Povetkin O.V.

(Rus)

Features of optimization of the versatile gas generator parameters and design for development of a broad power range line of the advanced gas turbine engines of different application

Sharova N.A.

(Rus)

Vol 18, No 1 (2019)

Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber

Matveev S.G.

(Rus)

Vol 17, No 4 (2018)

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.

(Rus)

Vol 17, No 2 (2018)

Improvement of friction units of power plants by aplying ceramic composite spray coatings

Siluyanova M.V., Fertikov A.O.

(Rus)

Vol 16, No 2 (2017)

Micro gas turbine engine imitation model

Kuznetsov A.V., Makaryants G.M.

(Rus)

Vol 15, No 4 (2016)

Peculiarities of computer modeling of the working process in small gas turbine engines

Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.

(Rus)

Vol 14, No 4 (2015)

Investigation of the causes of crack origination in the inner casing of NK-86 gas turbine engine combustion chamber

Kocherova Е.Е.

(Rus)

Vol 14, No 3-1 (2015): Special Issue

Early detection of vibration behaviour of aircraft engine multistage axial compressor in pre-surge states during rig testing

Khorikov A.A., Danilkin S.Y., Mazikina T.I.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Efficiency of complex cycles of gas turbine units with air bleed for the cooling of intermediate combustion chambers

Ivanov V.A.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system

Shishkov V.A.

(Rus)