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Vol 22, No 1 (2023)

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.

(Rus)

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

About investigations the orientation dependence of single-crystal turbine blade exploitation properties

Tikhomirova E.A., Givushkin A.A., Sidokhin E.F.

(Rus)

Vol 18, No 1 (2019)

Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades

Sazonov M.B., Solovatskaya L.V.

(Rus)

Vol 13, No 4 (2014)

Structural and acoustic anisotropy of turbocompressor blade material

Tarasenko Y.P., Krivina L.A., Motova E.A., Nikitina N.Y.

(Rus)

Vol 10, No 1 (2011)

Technique of operational monitoring of blade operational life exhaustion on turbounits

Danilin A.I., Grechishnikov V.M.

(Rus)

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

The Laue back-reflection method for determination orientation and subgrains disorientation of blade manufacture single-crystal pieces

Tikhomirova E.A., Sidokhin E.F.

(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 13, No 4 (2014)

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.

(Rus)

Vol 10, No 1 (2011)

Discrete-phase movement transducers for the determination of turbine blade vibration parameters

Danilin A.I., Grechishnikov V.M.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

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

Karpov A.V.

(Rus)

Vol 15, No 3 (2016)

Analysis of information characteristics of a dynamic displacement doppler transducer signal

Danilin A.I., Gretskov A.A.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Doppler method for measuring fluctuations of elements rotationg parts power

Danilin A.I., Gretskov A.A.

(Rus)

Vol 8, No 1 (2009)

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.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

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 15, No 3 (2016)

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.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

A technique to estimate efficiency of turbine underplatform friction dampers

Nikhamkin M.S., Sazhenkov N.A.

(Rus)

Vol 7, No 3 (2008): Special Issue

The devices for the diagnosis and control of turbine blades deformative condition during operation

Danilin A.I., Chernyavskiy A.G., Kapustin A.S.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

Methodology of optimization of parameter of matching the combustion chamber and turbine joint operation

Grigoriev A.V., Golubchikov P.P., Ilushin M.Y., Rudakov O.A., Solovieva A.V.

(Rus)

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

Analysis of the possibility of using topology optimization in the design of uncooled turbine rotor blades

Vasilyev B.E., Magerramova L.A.

(Rus)

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

Nondestructive testing of the working compressor blades of the aviation engine

Nikitina N.E., Motova E.A., Tarasenko Y.P.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

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.

(Rus)

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

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.

(Rus)

Vol 14, No 3 (2014)

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.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

Research of the fan blades flutter on the stalling airflow mode

Khorikov A.A., Danilkin S.Y.

(Rus)

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

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.

(Rus)

Vol 13, No 2 (2014)

Discrete phase converters moving elements rotating units power units

Danilin A.I., Grechishnikov V.M.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Automated system for measuring geometric parameters of turbine blades in production conditions

Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

The possibility of ultrasonic testing of compressor blades after exploitation and repair

Motova E.A., Nikitina N.Y.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Perfection of methods of conducting resonance tests of rotor blades being part of the engine

Khorikov A.A., Danilkin S.Y., Redkin D.A.

(Rus)

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

Operational testing of thermoplastic reinforced blades

Krutsilo V.G., Krotinov N.B.

(Rus)

1 - 30 of 30 Items

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