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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.
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.
Morphological characteristics of the intermetallic phase of heat resisting nickel alloys
Kirikov S.V., Perevezentsev V.N., Tarasenko Y.P.
Post-operation state and extension of service life of compressor blades of the gas-turbine power plant GTE-45-3
Tarasenko Y.P., Berdnik O.B., Tsareva I.N.
Discrete phase converters moving elements rotating units power units
Danilin A.I., Grechishnikov V.M.
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.
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.
Analysis of information characteristics of a dynamic displacement doppler transducer signal
Danilin A.I., Gretskov A.A.
Thermoplastic strengsening of blades aircraft gas turbine engines
Krotinov N.B.
Operational testing of thermoplastic reinforced blades
Krutsilo V.G., Krotinov N.B.
The devices for the diagnosis and control of turbine blades deformative condition during operation
Danilin A.I., Chernyavskiy A.G., Kapustin A.S.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
Research of the postoperational condition of the restored compressor shovels of GTD gas-transfer of the units which have fulfilled the appointed resource
Tarasenko Y.P., Tsareva I.N., Krivina L.A.
Laser powder weld reconditioning of gas turbine engine blades
Korsmik R.S., Turichin G.A., Klimova-Korsmik O.G., Zemlyakov E.V., Babkin K.D.
Doppler method for measuring fluctuations of elements rotationg parts power
Danilin A.I., Gretskov A.A.
Research of the mechanism of shock-inertial deposition of dispersed particles from a gas flow
Usmanova R.R., Zhernakov V.S.
Methods of the blade release at casings containment capability
Baluev B.A.
Blading of radial-axial turbine wheel using Bezier curve
Baturin O.V.
Research of the fan blades flutter on the stalling airflow mode
Khorikov A.A., Danilkin S.Y.
Analysis of the possibility of using topology optimization in the design of uncooled turbine rotor blades
Vasilyev B.E., Magerramova L.A.
A technique to estimate efficiency of turbine underplatform friction dampers
Nikhamkin M.S., Sazhenkov N.A.
Technique of operational monitoring of blade operational life exhaustion on turbounits
Danilin A.I., Grechishnikov V.M.
About investigations the orientation dependence of single-crystal turbine blade exploitation properties
Tikhomirova E.A., Givushkin A.A., Sidokhin E.F.
The possibility of ultrasonic testing of compressor blades after exploitation and repair
Motova E.A., Nikitina N.Y.
Experimental studies of prototype models of bimetallic blisks of a high-temperature turbine with cooled blades for advanced gas turbine engines
Magerramova L.A., Stadnikov A.N.
Technological features of formation of the multifunctional nanostructured coverings of nitride of the titan for compressor shovels aviation GTD
Tarasenko Y.P., Tsareva I.N., Kocherov E.P., Vyazovskaya L.M.
Discrete-phase movement transducers for the determination of turbine blade vibration parameters
Danilin A.I., Grechishnikov V.M.
The Laue back-reflection method for determination orientation and subgrains disorientation of blade manufacture single-crystal pieces
Tikhomirova E.A., Sidokhin E.F.
Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades
Sazonov M.B., Solovatskaya L.V.
Peculiarities of applying Darcy’s law in research and development of hybrid engine blades for an advanced aerospace plane
Baigaliev B.E., Tumakov A.G., Tumakov E.A.
Nondestructive testing of the working compressor blades of the aviation engine
Nikitina N.E., Motova E.A., Tarasenko Y.P.
Research and rationing admissible nick on working blades of the compressor for engine NK-12 example
1 1., 1 1., 1 1., 1 1.
Comparative analysis of facilities for the implementation of thermoplastic hardening blades of gas turbine engines and pumping units
Karpov A.V.
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.
Perfection of methods of conducting resonance tests of rotor blades being part of the engine
Khorikov A.A., Danilkin S.Y., Redkin D.A.
Optimization of casing on mass with ensuring requirements for deduction of the ragged blade
Krundaeva A.N., Gabov D.V., Maralev A.Y.
Structure and mehanpichesky properties of the shovel 1 steps of the rotor of turbine GTE-45-3 after the long operating time and regeneration
1 1., 1 1., 1 1.
Development of technology extension resource ХН65ВМТЮ alloy turbine blades
Berdnik O.B., Tsareva I.N., Razov E.N.
Assessment of gas turbine engine airfoil surface microstructure
Nosov N.V., Abramov A.D., Kosulin S.I.
Structural and acoustic anisotropy of turbocompressor blade material
Tarasenko Y.P., Krivina L.A., Motova E.A., Nikitina N.Y.
Research of a heat-resistant intermetallic underlayer for the heat-shielding coating of gas turbine engine turbine blades
Tarasenko Y.P., Tsareva I.N., Berdnik O.B., Fel Y.A., Krivina L.A.
Probabilistic estimate of compressor blades durability to foreign object damage
1 1., 1 1.
1 - 42 of 42 Items

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