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Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate
Kocherova E.E.
Product life cycle in the aspect of postulates of logistics and labour object theory
Sosnina T.N.
Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading
Badamshin I.K.
New possibilities of using spin rigs to provide gas turbine engine strength reliability
Nozhnitsky Y.A., Fedina Y.A., Shadrin D.V., Servetnik A.N., Baluev B.A., Kanachkin A.V., Lepeshkin A.R., Tomashev A.A., Chernyshev S.A.
Forecasting the individual performance capabilities of the rocket engine powerplant units at the maintanance stage
Biryuk V.V., Bronshtein V.M., Presnyakova A.S., Shatilova M.Y., Dostovalova S.S.
Procedure rules of press forging business process development and coordination
Khaimovitch I.N., Khaimovitch A.I.
Biological module “BiNOM” for cubesats of the SamSat family
Zakharov V.P., Konyukhov V.N., Bakhtinov P.I., Molchkov E.V., Kornilin D.V., Konovalov S.G.
Application of the cyclic life additivity concept for the determination of service life of aero engine disks made from powder alloys
Tumanov N.V., Lavrentyeva M.A., Vorobyeva N.A., Kalashnikova A.I.
Technique of operational monitoring of blade operational life exhaustion on turbounits
Danilin A.I., Grechishnikov V.M.
Design of experiments for verification of computational life prediction methods
Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.
Relation between characyeristics of low-cycle and high-cycle fatigue of threaded parts and residual stresses
Zlobin A.S.
Conception of cycle life additivity and its application for determining the resource of aero engine disks
Tumanov N.V., Lavrentyeva M.A.
Development and investigation of electropump of increased service life with ball bearings
1 1., 1 1., 1 1., 1 1.
Life of gas turbine engine components under corrosive exposure
Pivovarova M.V., Gladkiy I.L.
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.
Laws of life dispersion and statistical estimation of life distribution boundaries as applied to aviation engine LPC disks
Kutyrev V.V., Teplova S.V.
Design and technological solutions for provision of high reliability and life time of aviation gas turbine engine disks
Nozhnitskiy Y.A., Karimbaev K.D., Potapov S.D.
Criterion assessment of the possibility to prolong the service life limit of the helicopter tail drive shaft
Mashoshin O.F., Semenikhin R.L.
Life testing of pipeline elements
Boltenkova O.M., Davydov O.Y., Yegorov V.G.
The integrated information model architecture for working out, manufacture and operation GTE together with its system of automatic control, the control and diagnostics
Kulikov G.G., Rizvanov K.A., Denisova S.S.
Education organization in common information sphere given about product
Prodanov M.Y.
Estimation of residual stress influence on the low-cycle fatigue of threaded parts
Zlobin A.S.
Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation
Shuplyak Y.P., Sorokoletov V.I.
Questions of HCF for materials and details modern GTE
Petukhov A.N.
Study of mechanisms of low cycle fatigue crack propagation in aero engine disks under operating conditions and disk residual life estimation
Tumanov N.V., Cherkasova S.A., Lavrentyeva M.A., Vorobyeva N.A.
Ways of increasing the reliability and service life of bearing assemblies of modern gas-turbine engines and gears
Petrov N.I., Lavrentyev Y.L.
Ontology description languages for high-tech fields of applied engineering
Burakova E.E., Borgest N.M., Korovin M.D.
Process of autoreengineering of entreprise common information space
Ivashchenko A.V.
Proposals for improving the efficiency and service life of the turbines of turbo-pump assemblies in liquid-propellant rocket engines by using double-sided crest-type radial labyrinth seals
Levochkin P.S., Chvanov V.K., Vasiliev V.S., Timushev S.F.
Experimental determination of thermal-fatigue life of turbine blades with various coatings made of an advanced heat resistant nickel alloy
Bychkov N.G., Nozhnitsky Y.A., Khamidullin A.S., Pershin A.V., Avrutsky V.V.
The interactive system for collecting data of technical condition of aircraft components
Blagorazumov A.K., Kirpichev I.G.
1 - 31 of 31 Items

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