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Vol 7, No 1 (2008)

Product life cycle in the aspect of postulates of logistics and labour object theory

Sosnina T.N.

(Rus)

Vol 23, No 2 (2024)

The relevance of introducing a requirements management system in the production process of the aircraft engine construction industry

Malinovskiy I.M., Starodumov A.V., Myagkov K.A., Yusipov B.K.

(Rus)

Vol 17, No 1 (2018)

Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate

Kocherova E.E.

(Rus)

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

Education organization in common information sphere given about product

Prodanov M.Y.

(Rus)

Vol 14, No 4 (2015)

Estimation of residual stress influence on the low-cycle fatigue of threaded parts

Zlobin A.S.

(Rus)

Vol 11, No 4 (2012)

Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation

Shuplyak Y.P., Sorokoletov V.I.

(Rus)

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

Questions of HCF for materials and details modern GTE

Petukhov A.N.

(Rus)

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

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.

(Rus)

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

Ways of increasing the reliability and service life of bearing assemblies of modern gas-turbine engines and gears

Petrov N.I., Lavrentyev Y.L.

(Rus)

Vol 14, No 3 (2014)

Ontology description languages for high-tech fields of applied engineering

Burakova E.E., Borgest N.M., Korovin M.D.

(Rus)

Vol 8, No 2 (2009)

Process of autoreengineering of entreprise common information space

Ivashchenko A.V.

(Rus)

Vol 17, No 4 (2018)

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.

(Rus)

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

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.

(Rus)

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

The interactive system for collecting data of technical condition of aircraft components

Blagorazumov A.K., Kirpichev I.G.

(Rus)

Vol 17, No 3 (2018)

Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading

Badamshin I.K.

(Rus)

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

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.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

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.

(Rus)

Vol 7, No 1 (2008)

Procedure rules of press forging business process development and coordination

Khaimovitch I.N., Khaimovitch A.I.

(Rus)

Vol 17, No 2 (2018)

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.

(Rus)

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

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.

(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 18, No 3 (2019)

Design of experiments for verification of computational life prediction methods

Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.

(Rus)

Vol 17, No 1 (2018)

Relation between characyeristics of low-cycle and high-cycle fatigue of threaded parts and residual stresses

Zlobin A.S.

(Rus)

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

Conception of cycle life additivity and its application for determining the resource of aero engine disks

Tumanov N.V., Lavrentyeva M.A.

(Rus)

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

Development and investigation of electropump of increased service life with ball bearings

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

(Rus)

Vol 18, No 3 (2019)

Life of gas turbine engine components under corrosive exposure

Pivovarova M.V., Gladkiy I.L.

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

Laws of life dispersion and statistical estimation of life distribution boundaries as applied to aviation engine LPC disks

Kutyrev V.V., Teplova S.V.

(Rus)

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

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.

(Rus)

Vol 16, No 2 (2017)

Criterion assessment of the possibility to prolong the service life limit of the helicopter tail drive shaft

Mashoshin O.F., Semenikhin R.L.

(Rus)

Vol 11, No 4 (2012)

Life testing of pipeline elements

Boltenkova O.M., Davydov O.Y., Yegorov V.G.

(Rus)

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

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.

(Rus)

1 - 32 of 32 Items

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