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

Full Issue

AIRCRAFT AND SPACE ROCKET ENGINEERING
Simulation of turbulent flow in simple and complex diffuser channels
Davletshin I.S., Mingazov B.G., Yavkin V.B., Kesel B.A., Voskoboynikov D.V.
Abstract

This paper presents a comparative study of six turbulence models for calculating the diffuser channels of different configurations, and also study of influence of parameters of computational grid on calculation results. The simulations was carried out on six grids with different spacing for the near wall points and different resolutions. The performance of six different turbulence models is compared with experimental results obtained at «Aviamotor» and other published experimental results. Creation of optimal models for different stages of engineering calculations of exhaust systems is considered.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):11-15
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Repair of aircraft engine and respective conception under the condition of modern production at manufacturing plants and engine operability recovery centers
Steshenko I.G., Panov V.A.
Abstract

Problems of serial plants leading to repair as the main type of activities are investigated. Organization of production allowing cutting repair spending is presented. New types of repair are listed. A conception of repair and modernization at engine operability recovery centers is formulated.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):16-19
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Application of tailored welded blanks in aerospace and automotive industries
Khayrullin T.V., Stolbov V.I.
Abstract

Analyzed actual development in application and manufacturing tailored welded blanks for cold stamping (TWB)
parts in airspace and automotive industries. Represented basic possibilities to increase of effectiveness of implementing TWB by high-producing welding technologies and determined basic tasks of realization it.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):20-27
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Experimental methods of carbon-based structures of nanotubs materials
Motova E.A., Moskvichev A.N.
Abstract

An analytical review of the scientific publications of recent years on how to obtain nanocarbon materials. Shows perceptiveness method synthesis chemical deposition from metal-organic chemical vapor deposition for filter materials based on multiwall carbon nanotub for cleaning liquid and gaseous environments

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):33-39
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Experiment-calculated research of the influence of the shot-peening strengthening upon the low-cycle fatigue of the gas turbine parts with the stress concentrator
Porter A.M., Bukaty S.A., Leshin D.P., Bukaty A.S.
Abstract

The finite-element technique of the deflected mode of the gas turbine parts in the stress concentration zone with the residual stress after shot-peening strengthening has been developed here. The deflected mode in the interlock of the type “dovetail” after shot-peening strengthening is examined on the example of the low pressure compressor disc. Calculations and low-cycle fatigue tests of the samples and disks performed on the test stand “UIR-3” verified the effectiveness of the surface plastic deformation strengthening in the stress concentration zone.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):40-46
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Application of technology microarc oxidation (mao) aluminum and titanium alloys to improve performance parts in engines
Krishtal M.M., Ivashin P.V., Polunin A.V.
Abstract

This work substantiates the appropriateness of micro-arc oxidation technology usage for hardening of silumin with a silicon content of 6 ... 11% in the manufacture of major body parts of engines, and also the titanium alloy VT1. Results of preliminary research experiments, and study the main factors affecting the quality of the coating were described.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):47-51
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The possibility of ultrasonic testing of compressor blades after exploitation and repair
Motova E.A., Nikitina N.Y.
Abstract

The results of nondestructive testing of blades of axial compressor of gas-turbine engine of gas-pumping unit are represented. The experimental investigations were based on ultrasonic pulse-echo method. The opportunities of the nondestructive acoustical method for the studying of the steel structure during the exploitation of blades are demonstrated.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):52-56
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Research of the fan blades flutter on the stalling airflow mode
Khorikov A.A., Danilkin S.Y.
Abstract

Results of a dynamic condition experimental research of the modern three-stage blisk fan designs, designed on new calculated technologies are resulted. Features of rotor blades fluctuations are revealed at research of a flutter in stalling area. As a result of the carried out experimental research the conclusion that there are two kinds of a subsonic cascade flutter is made: without-stalling flutter to which there corresponds the wave of deformation running on rotation and a stalling flutter at which the wave of deformation runs against rotation.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):57-63
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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.
Abstract

In work results of researches of a condition of compressor shovels gas turbine engines gas-transfer the units which have fulfilled the appointed resource (~ 50 000 hours) after carrying out of repair-regenerative processing with application of ionic-plasma coverings of nitride of the titan are resulted.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):64-67
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On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Abstract

The article generalizes experience of automatic regulation systems design and development for aircraft and industrial gas turbine engines, operating with liquid hydrogen (NK-88 engine in TU-155 aircraft) or liquid natural gas (NK-89 engine in TU-155 aircraft, NK-361 engine in gas-turbine locomotive GT1-001).

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):68-77
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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.
Abstract
The report represents gas turbine locomotive LNG fuel system development results
VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):78-81
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Substantiation of the criteria for evaluation of the efficiency of the fuel supply system of the gas turbine engines
Smurova N.A.
Abstract

The article provides determinative and sub-priority criteria considered for solution of a multicriterion problem of the efficiency evaluation which characterizes implementation of a number of priority functions by the fuel flow automatic control system. These functions define switching of the automatic fuel flow in the fuel lines of the aircraft engines as well as possible fuel drain to the object drain system and its transverse centering. Presentation of the efficiency function as a function of two variables, which characterize the effect of the use of the control system regarding the determinative and one of the sub-priority indicators, permits to use a method of the stepwise evaluation of the efficiency.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):82-88
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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.
Abstract

The work studies issues to provide the guaranteed construction strength of the single-crystal rotor blades of the aviation gas turbine engines taking into account the anisotropic properties conditioned by their crystallographic orientation. Special attention is paid to research of the thermo-fatigue properties of the samples taken from the single-crystal superalloys. Influence of the thermo-cycling intervals on the durability of the samples with given orientation has been shown taking as an example ЖС36ВИ alloy.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):89-97
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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.
Abstract

The article considers a possibility of application of the versatile gas generator in designing of the gas turbine engine. Limitations of the use in the mathematical model, criteria of optimization, power range have been defined. Parameters of the optimal gas generator developed on the basis of the VK-800 have been defined. A possibility of development of the 6000-hp engine with the use of the gas generator of the VK-2500 serial engine has been considered.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):98-105
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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.
Abstract

For the purpose to provide the fuel efficiency and the engine reliability the article analyses characteristics of the temperature field, the fuel flow turbulence downstream of the combustion chamber, depth of the nozzle guide vanes cooling in their interconnection on the basis of optimization of the value of the corrected gas flow rate upstream of the turbine as a matching parameter of the joint operation of these thermal and gas dynamic units taking the effective efficiency of the engine thermo-dynamic cycle as a goal function considering the strength limit of the rotor blades.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):106-111
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Mixing processe research in 10…15 N thrusters
Salich V.L., Semkin E.V.
Abstract

This paper presents the research of possible three numerical simulation technique applications in designed calculations of 10…15 N thruster swirl atomizer. Comparison results are given.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):112-119
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The numerical modelling of processes in combustion chambers of low thrust rocket engines
Salich V.L.
Abstract

The mathematical model of processes in combustion chambers of low trust rocket engines with diphasic fuel compositions and results of calculations of the chamber of the engine with fuel composition gaseous oxygen / ethanol are presented.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):120-125
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Character creator of electropneumatic valve for 49 MPa gaseous oxygen working pressure. Statement of problems and problem solving ways
Kazankin F.A., Kalnitsky I.D.
Abstract

This paper describes an electropneumatic valve (EPV) structure for gaseous oxygen with 49 MPa working pressure and defines problems which are necessary to be solved in order to provide EPV working capacity.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):126-129
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Testing of combined air-rocket engine mak-up with pulsing combustion chamber
Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.
Abstract

This paper describes the test results of combined air-rocket engine mak-up at air (V = const) and rocket modes (р = const), the main technical characteristics have been obtained.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):130-136
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Thermal physics of hydrogen-oxygen combuster chambers for high-temperature turbines combined-cycle power plant
Guryanov A.I., Piralishvili G.S., Vereschagin I.M.
Abstract

There are presented the results of the numerical modeling hydrogen combustion in oxidizing environment of the premixed steam-oxygen mixture in operating conditions of the promising combustion chambers that can be used as high-temperature steam’s generators for combined cycle power plants. It is defined a geometry of the mixing module, flame stabilizer and primary combustion zone that provides high mixing quality and absence of local zones of overheating construction’s elements of the combustion chamber.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):137-144
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Calculation of indicator diagram dynamic test at internalcombustion engine in KDAM environment
Kosenok B.B.
Abstract

The description of the environment KDAM created on the basis of the vector unit models, made substantiation of necessity modeling the indicator diagram, the analysis of the possible construction of the vector model, which describes the indicator diagram, selected two options for constructing such vector models. This study substantiates the method of modeling the indicator diagram based on the method of mathematical modeling of vector closed contours and shows some of the advantages of this model.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):145-149
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Improving the efficiency of diesel engines by means of electroprocessing of fuel
Kozmenkov I.N., Nosyrev D.Y.
Abstract

In the article the method of diesel locomotive efficiency upgrading by the process of electrical fuel manufacturing ispresented. An expression capable for evaluating the increase of proportion of active centers in the fuel after manufacturing by an electric discharge was obtained. A model of fuel diffusion combustion after manufacturing was developed. Processing and burning diesel fuel experiments are presented. Simulating of the work process of a diesel locomotive 10Д100’ diesel engine by using of electrothermal processing of fuel is conducted. The results received in work connect parameters of fuel manufacturing with diesel engine indicators. This allows providing feedback and more effective usage of fuel manufacturing in locomotive power stations.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):150-155
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Experimental and numerical investigation of the combustion process in vortex gas burner
Yevdokimov O.A.
Abstract

There are presented the results of numerical and analytical calculations of the combustion efficiency in the tubular combustion and gas ejection burner and. There is performed its experimental confirmation.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):156-163
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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.
Abstract

In the results of research structure, physico-mechanical properties and heat-resistance characteristics of combined heat-resistant coatings NiCrCoAlY/ZrO2 obtained by gas evaporation method using plasma torch Coverage introduced improved design, consisting of repair or replacement work and technology extension resource guide vanes of turbine power plants.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):164-169
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Optimization of the technology of ion-plasma coating of titanium nitride in the small-sized thin-walled details
Tarasenko Y.P., Krivina L.A., Tsareva I.N., Il'ichev V.A.
Abstract

The influence of technological factors (arc current, the partial pressure of nitrogen) the structure and physicomechanical properties of ion-plasma coating of titanium nitride. The regularities of formation of nanostructured columnar TiN coatings.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):170-174
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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.
Abstract

Using microfractographic observations the mechanisms of low cycle fatigue crack kinetics in aero engine disks under operating conditions have been established. On this basis the techniques for disc residual life estimation have been developed. The techniques have been verified with the data of crack growth microfractographic reconstitution and crack kinetics direct observation on a disk surface.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):175-184
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Complex failure analysis of aero engine compressor blades
Sachin V.M., Tumanov N.V., Lavrentyeva M.A., Cherkasova S.A.
Abstract

Techniques for blade flutter diagnostics using stationary transducers and microfractographic observations are presented. Both these methods have been applied for compressor blade failure analysis of preproduction aero engines. As a result the cause and kinetics of the failures have been established.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):185-194
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Way of the determination to long toughness unidirectional polymeric composition material and device for measurement effort, displacement and time before destruction sample
Lebedev D.N., Shcherbakov E.S., Larin M.N., Migachev A.S., Ilyin E.A.
Abstract

The describes the experimental installation for studying long-term strength of unidirectional polymer composites materialov. Used as a model sample mikroplastics is loaded using chart changes in forces and displacements are recorded hydraulic cylinders to its destruction, the info light-sensitive tape recording. Experiments are repeated at different speeds of displacement of rod hydraulic cylinder. The dependence of the tensile strength of the samples from the rate of load application is estimated.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):195-199
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Design procedure of fundamental parameters of the direct-flow detonation pulsing engine
Porshnev V.A.
Abstract

The design procedure of fundamental parameters of the direct-flow detonation pulsing engine (DDPE) for small dimensional the pilotless flying machine is considered. The algorithm of calculation is presented.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):200-205
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Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle
Grigoriev V.A., Kuznetsov S.P.
Abstract

Ensuring reliable and safe flight operation of the aircraft engines is actually attained by the developers, manufacturers and operators at all stages of the engine life cycle. This necessitates the analysis of the engine configuration, which is formed while making up engine sets and assembling using a specific for the moment design of parts or components, which were manufactured, subjected to inspection and tests under the specific manufacturing conditions. The results of such analysis in connection with the results and conditions of operation form the engine airworthiness management system. Such a system implies methodology, which provides for account of all normative requirements beginning with the design stage and their further execution control at stages of development, serial production and operation. One of the main aspects of the system is definition of parts, components and assembly units and further classification thereof depending on the extent of their impact on flight safety.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):206-211
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The experimental thermoacoustic device
Kharitonov A.A.
Abstract

The transition processes in the thermoacoustic heat pump are presented. The thermoacoustic heat pump was designed and build by “Thermoacoustic Technology Ltd” in cooperation with the ФГУП ГНП РКЦ «ЦСКБ-ПРОГРЕСС». The experimental thermoacoustic device may be used as a refrigerator, heat pump or an acoustic pulsator. It consists of the thermoacoustic engine, thermoacoustic refrigerator and the acoustic resonator. The work of the experimental device based on the direct and the reverse thermoacoustic effects. The direct thermoacoustic effect is the generation of the acoustic waves due the temperature gradient. The reverse thermoacoustic effect is the generation of the temperature gradient due the work of the acoustic waves. The thermoacoustic technology has many various applications at different branches of the science and technique.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):212-216
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Turboprofan jet modeling and equivalent specific fuel consumption optimization subsystem construction on the seminatural modelling stand
Pogorelov G.I., Krivosheev I.A., Godovanyuk A.G., Danilin O.E., Badamshin B.I.
Abstract

There was shown offered method’s of linear interpolation propfan’s multidimensional characteristic results using for modeling turboprofan jet in a total range of flight conditions and approach to equivalent specific fuel consumption optimization subsystem construction in automatic control system structure for reduction of environmental tests and maintenance costs. The offered methods considers requirements to mathematical models for the seminatural modeling stand - simplicity, ensuring of sufficient accuracy of result, work and functioning engine’s mathematical model in a mode of real time.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):217-226
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About relaxational resistance of the compressor’s blades from titanium alloys
Smyslov A.M., Smyslova M.K., Dubin A.I.
Abstract

The questions of fatigue strength and surface parameters of the compressor’s blades gas-turbine’s engine (GTE) from titanium alloy VT6 investigation are considered. The complex vacuum-plasma treatment of the surface (CVPT) comparing with serial (base) technology is described. Recommendations for practice use of CVPT technology are given.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):227-232
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Compressor blade erosion modeling
Gumerov A.V., Akmaletdinov R.G.
Abstract

Jet engines are the basic type of engines in a civil and military aviation, used as main and forcings energy plant is in shipbuilding, energy, gas industry. A major requirement to the engines is high operating reliability. The design of processes of erosion by modern numerical complexes give new benefits for prognostication of the impermissible states of JE in exploitation, to apply on the stage of planning necessary and sufficient methods to protect engine details from erosion.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):233-239
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Development of technology extension resource ХН65ВМТЮ alloy turbine blades
Berdnik O.B., Tsareva I.N., Razov E.N.
Abstract

The goal was to examine postèkspluatacion of material working blades of gas turbine engines have a long lifespan and determining their maintainability. Looking for studies of chemical composition, microstructure, phase, physical and mechanical properties of heat-resistant nickel alloy. Have been developed for high-temperature heat treatment alloy modes (ЭИI893) to save the product.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):240-247
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Possibility of use of passing gases in gasturbine engines created within the limits of conversion
Rosljakov A.D., Kocherov E.P., Tsibizov J.I.
Abstract

The requirements shown to газотурбинным to engines of land application and a problem which arise at use as fuel of passing gases and топлив, coals received by gasification are analysed. It is shown that a vital issue at use of passing gases is possibility of formation of a condensate of hydrocarbonic gases at increase of pressure of air behind the compressor and in channels of giving of fuel. Creation of systems of use of alternative kinds of fuel by association of means and other resources of the enterprises of customers of such systems and the enterprises of manufacturers land GTE can be a comprehensible variant of the decision of such problem.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):248-252
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Estimation of a tension of a columnar thermal barrier coatings on nozzle turbine blades and segments of flame pipes of combustion chambers subject to frictional force between a ceramic layer and gas-dynamic flow
Bychkov N.G., Khamidullin A.S., Pershin A.V.
Abstract

In the present work the destruction model of columnar ceramic thermal barrier coatings deposited by electron beam technology is proposed. Estimation of a tension of a columnar thermal barrier coatings on nozzle turbine blades and segments of flame pipes of combustion chambers subject to conditions of their work is made.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):253-258
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The development of the optimization methodology of the turbine blade-disk interlock of the type “fir tree”
Bukaty A.S., Bukaty S.A., Andreev I.B.
Abstract

The methodology of the optimization of the interlock blade-disk of the type “fir tree” is examined within the bounds of this paper. The methodology is based on the method of the complex experiment. Agodjino criterion of the stress-state rigidity and the plasto-elastic deformation energy of the material are used as the optimization criteria.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):259-265
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Analysis and ballistics design of a laboratory installation system a small calibre with a joined drive on chambers
Safronov A.I., Zorkin V.A., Potapenko V.V.
Abstract

This article discusses issues of designing systems with two a joined drive on chambers. These systems give a greater gain in the initial speeds than systems with single-camera about 9%, as compared with the classical scheme more 25%.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):266-270
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Comparative analysis of facilities for the implementation of thermoplastic hardening blades of gas turbine engines and pumping units
Karpov A.V.
Abstract

In the article the basic design of patented plants to implement the process of hardening the thermoplastic (TPU) blades of gas turbine engines and gas compressor units.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):271-276
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Prospects and problems of movement and power plants in powder metal fuel
Egorov A.G., Tizilov A.S.
Abstract

The possibility of improving the energy characteristics of missilesystems by the use of powdered metal powder as the main fuel in a ramjet engine and their basic dignity.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):277-281
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The possibilities of engine volumetric efficiency increasing at the expense of self-closing inlet valve
Kozin A.M., Rusakoff M.M.
Abstract

The volumetric efficiency process of engine cylinders with self-closing inlet valve was studied. The relations of engine cylinder volumetric efficiency from engine speeds for various variants and closing times of self-closing inlet valve are established. The possibilities of increasing engine performance are shown.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):282-286
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HUMANITIES
Identifying the high school teachers` readiness to distance learning in the modernization of the education system
Belousov A.I., Gromova T.V.
Abstract

The article is devoted to the necessity of special preparation of higher school teachers to tutor activity organization, the insufficient readiness (professional, psychological and technical) of whom seems to be the main obstacle in distance training implementation in the Russian educational system.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):287-295
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Modeling and experimental research of the multi-level drawing and geometric training system
Ivashchenko V.I.
Abstract

Drawing subjects improvement possibilities for the training of the innovation machinery construction specialists are considered. The model of the multi-level drawing and geometric training system is worked out and realized at «Aircraft engines» faculty of Samara State Aerospace University. The results of the pedagogical experimental research are produced.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):296-303
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On content of discipline «Dynamics and control of hydro-and pneumatic systems»
Gimadiev A.G., Bystrov N.D., Kruchkov A.N.
Abstract

Composed of educational-methodical material on the subject «Dinamika and regulation of hydraulic and pneumatic systems», designed for students majoring 121100 «Hydraulic machines, hydraulic and Hydro, and several other specialties», which include the study of hydraulic and pneumatic systems for the preparation of examinations, laboratory and of course work and the protection of graduation projects. Can also be used for training of masters on direction «Technological machinery and equipment» 151000.62, opened in Samara State Aerospace University in 2011. Consists of four parts: the lecture notes on the dynamics and management of hydraulic and pneumatic systems, laboratory course, which consists of six labs, the course project on the calculation of the dynamic behavior of an autonomous hydraulic servo steering gear with throttle control and checklists for the current and final control of the degree of assimilation material.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):304-308
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Analysis of the experience of preparing the users machine-building CAD in centre of the computer designing
Cherepashkov A.A.
Abstract

In article are discussed the problems of training to designing of mechanical engineering products. Systems and methods of computer aided design which are used in the school of mechanical engineering of the Samara technical university (SSTU) are analyzed. Experience of creation the CAD/CAM/PLM/-center are described.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):309-314
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Training for innovative engineering through through parametrization
Balyakin V.B., Ermakov A.I., Chempinsky L.A.
Abstract

The CAD system world already became 3D. But 2D modeling is still actual for many of engineering tasks. This article gives the retrospective for 2D modeling tools in CAD systems and explains some special methods, used in ADEM-VX system. Samples are given in 2D solid mechanism and layer-mechanism for assembly creation in 2D.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):315-322
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Sales training methods based on through the use of CAD / CAM / CAE systems for aero engines
Balyakin A.V., Ermakov A.I., Pronichev N.D., Chempinsky L.A.
Abstract

The article discusses the implementation of modern methods of training qualified specialists for the aircraft engine based on the through the use of CAD / CAM / CAE systems. In particular, sets out the stages of a geometric graphstudent training, engineering and technological design of aircraft engine parts

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):323-329
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Development of the programme complex for student independent work «ARMS - graphics»
Solovatskaya L.V.
Abstract

The programme complex is designed for independent work student. The considered questions connected with his(its) building - is analysed structure and composition database. It is shown that under is - use this programme complex possible to raise efficiency graphic and geometry training by means of act of concentration of the whole necessary information in one place - normative and reference data, as well as technological accompaniment in the manner of video, demonstrating processing the details on tool with CNC. The Results of the study are intended for using on all faculty of Samara state aerospace university (SSAU).

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):330-333
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Mathematical model of mastering educational information of the academic process
Titov B.A., Ryabinova E.N.
Abstract

The article gives the results of working out the mathematical model of mastering the educational material based on continuous monitoring of developments of learning abilities of students and corresponding adjustment of process of education by definite, structured in advance its component parts. The model of mastering presents the system of ordinary differential equations of the twelfth noted concerning functions of mastering and so called motivational components of educational information.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):334-340
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The management peculiarities of college administration in introducing federal state educational standard for vocational education
Gusev V.A.
Abstract

The article deals with the questions of effective management in educational establishment during introducing the standards of the third generation. In “The Volga Region State College” it carried out as an experiment on the basis of The Federal State Establishment “Federal Institute of Development of Education”. The subject is “Working Out and Approving The Complex Of Managing, Standard, Education And Methodic Documentation For Realization Main Vocational Educational Programs In Concordance With Federal State Educational Standard Of Vocational Education of The Third Generation”. The articles shows the results of experimental researches and suggests the system of personal management which increase personnel potential in ensuring high results of activity.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):341-345
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Forming professional-significant qualities of students-future engineers in terms of modular-rating technology of education
Rakhimova J.I.
Abstract

The article is devoted to modular-rating educational system while “energy-saving in heat-power engineering and technology” course teaching for IV year students of Heat Power Department.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):346-350
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Implementation of control technigue for institute of higher technological education students' self-educational activity
Tarabrina T.B.
Abstract

This article is dedicated to the inspection methods of self-depended students work in academy. Organization and inspection are impulse forces for learning process and acquirement. The Theory of supposed patterns for organization forming and for inspection of self-dependent students’ work is also set in this article.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):351-356
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The professionally-directed aspect of educational tools for self study
Rudina T.V.
Abstract

In the article is devoted to the professional orientation of mathematics teaching in the preparation of engineers. This approach is implemented in the educational-methodical manual on linear algebra. Approbation of this handbook was successfully held at the Samara state technical university and Samara state university of means of communication.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):357-365
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The reflective aspect of forming the students’ communication culture
Drokina S.V.
Abstract

The reflective tasks are the means of managing the process of forming the students’ communicative competence. Different classifications of training objectives as well as reflective ones are analyzed in the article. The most important things are: describing the situations for analysis, questions to work with texts, subjects for discussions during forums and seminars which are considered to be reflective tasks in the process of teaching students philosophy.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):366-373
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Education organization in common information sphere given about product
Prodanov M.Y.
Abstract

In the article it is considered the organization of product life cycle management in university education. Оrganization structure, composition and methods of use of common information sphere given product for making is described. An area of process-oriented and object-oriented systems use is determined.

VESTNIK of Samara University. Aerospace and Mechanical Engineering. 2011;10(3-2):374-379
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