Vol. 14 No. 3 (38) (2010): Вестник УГАТУ

Published: 2018-09-03

The usage experimental method for improvement of characteristics of flue path of turbine GTE

Igor Aleksandrovich Krivosheev, Evgeniy Vladimirovich Osipov

3-15
- PDF (Русский)
About using Ol’shteyn method for predicting off-design performance of multistage axial compressors

Dmitriy Albertovich Ahmedzyanov, Yuriy Mavlyutovich Ahmetov, Aleksandra Borisovna Kozlovskaya, Aleksey Evgenevich Mihaylov

16-31
- PDF (Русский)
Maintenance support information system of gas-turbine engine electronic technical systems based on multiaspect model

Gennadiy Grigorevich Kulikov, Grigoriy Ivanovich Pogorelov, Yuliya Olegovna Bagaeva

32-41
- PDF (Русский)
Algorithms of checking and diagnosis from gas-turbine engine of on-board implementation with use of neural network technology

Sergey Vladimirovich Zhernakov

42-56
- PDF (Русский)
The account of influence of non-uniformity of parameters working body on characteristics of knots GTE and PE

Aleksey Ivanovich Goryunov, Ivan Mihaylovich Goryunov

57-61
- PDF (Русский)
Design procedure and simulation of centrifugal compressors

Dmitriy Albertovna Ahmedzyanov, Aleksandra Borisovna Kozlovskaya, Nataliya Borisovna Proskurina

62-71
- PDF (Русский)
The comparative analysis of innovative regularities of aviation engines development

Sergey Grigorevich Selivanov, Svetlana Nikolaevna Poezzhalova

72-83
- PDF (Русский)
Methodology of the system analysis to the decision of the condition information monitoring problem of the aviation engine

Sergey Vladimirovich Zhernakov

84-100
- PDF (Русский)
Information technology of integration the intellectual pyrometric module in the control system, the control and diagnostics (FADEC) GTE

Evgeniy Viktorovich Raspopov, Gennadiy Grigorevich Kulikov, Vladimir Alekseevich Trushin, Viktor Sergeevich Fatikov, Tatyana Petrovna Andreeva, Irek Timeryanovich Gubaydullin

101-110
- PDF (Русский)
Hardening of the top piston flutes of internal combustion engines by the method of spark hardening

Natalya Yurevna Dudareva

111-115
- PDF (Русский)
Optimization geometry of blade apparatus and object of turbines of GTE with use of planning of numeral experiments

Igor Aleksandrovich Krivosheev, Evgeniy Vladimirovich Osipov

116-123
- PDF (Русский)
Analysis of options for superstructure of the CHP by the gas turbine installation

Konstantin Nikolaevich Brezgin, Ivan Mihaylovich Goryunov

124-130
- PDF (Русский)
Estimate of flame velocity using numerical thermogas dynamic simulation

Aleksandr Evgenevich Kishalov, Damir Hanyafievich Sharafutdinov

131-136
- PDF (Русский)
Tool solutions to problems of the complex hightech products

Ruslan Rafailovich Yamaliev, Roman Alekseevich Zavyalov, Andrey Vladimirovich Suhanov

137-143
- PDF (Русский)
Gas-turbine engine units design using resources of stereo lithography for form models production

Veronika Pavlovna Monahova, Vadim Vasilevich Terentev, Aleksey Aleksandrovich Yakovlev

144-150
- PDF (Русский)

Vol. 14 No. 3 (38) (2010): Вестник УГАТУ

The usage experimental method for improvement of characteristics of flue path of turbine GTE

About using Ol’shteyn method for predicting off-design performance of multistage axial compressors

Maintenance support information system of gas-turbine engine electronic technical systems based on multiaspect model

Algorithms of checking and diagnosis from gas-turbine engine of on-board implementation with use of neural network technology

The account of influence of non-uniformity of parameters working body on characteristics of knots GTE and PE

Design procedure and simulation of centrifugal compressors

The comparative analysis of innovative regularities of aviation engines development

Methodology of the system analysis to the decision of the condition information monitoring problem of the aviation engine

Information technology of integration the intellectual pyrometric module in the control system, the control and diagnostics (FADEC) GTE

Hardening of the top piston flutes of internal combustion engines by the method of spark hardening

Optimization geometry of blade apparatus and object of turbines of GTE with use of planning of numeral experiments

Analysis of options for superstructure of the CHP by the gas turbine installation

Estimate of flame velocity using numerical thermogas dynamic simulation

Tool solutions to problems of the complex hightech products

Gas-turbine engine units design using resources of stereo lithography for form models production

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