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pro vyhledávání: '"A S, Kuz'michev"'
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 19, Iss 4, Pp 43-57 (2020)
Recent studies related to fuel economy in air transport conducted in our country and abroad show that the use of recuperative heat exchangers in aviation gas turbine engines can significantly, by up to 20...30%, reduce fuel consumption. Until recentl
Externí odkaz:
https://doaj.org/article/385a565d1a344f46b5edf0d6c6588d65
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 19, Iss 3, Pp 85-99 (2020)
Continuous improvement of fuel efficiency of aircraft engines is the main global trend in modern engine construction. To date, aviation gas turbine engines have reached a high degree of thermodynamic and design-and technology perfection. One of the p
Externí odkaz:
https://doaj.org/article/d131c61e28694e96998121c63571d986
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 3, Pp 67-80 (2019)
Despite the fact that aviation gas turbine engines (GTE) have reached a high degree of sophistication, requirements for the improvement of their efficiency are constantly increasing. Reduction of specific fuel consumption and specific weight of the e
Externí odkaz:
https://doaj.org/article/ee59010aba704ad2bfe42dd4f83bfaf2
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 15, Iss 4, Pp 91-101 (2016)
The article describes a thermo-gas-dynamic model of small gas turbine engines. The model takes into account the influence of the engine size on the efficiency of work processes in the crucial components. Gas turbine engines are classified according t
Externí odkaz:
https://doaj.org/article/33049aa173d647b09c74a0efab051733
Improving the efficiency of aviation turboshaft engine with the recuperator in the helicopter system
Publikováno v:
AIP Conference Proceedings.
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 235:2014-2021
Development of a gas turbine engine starts with optimization of the working process parameters. Turbine inlet temperature is among the most influential parameters that largely determine performance of an engine. As typical turbine inlet temperatures
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 19, Iss 4, Pp 43-57 (2020)
Recent studies related to fuel economy in air transport conducted in our country and abroad show that the use of recuperative heat exchangers in aviation gas turbine engines can significantly, by up to 20...30%, reduce fuel consumption. Until recentl
Autor:
M. V. Spiridonov, A. S. Kuz’michev, A. P. Kotkov, O. S. Anoshin, Yu. P. Shapovalov, D. M. Polezhaev, A. I. Skosyrev, Ya. Ya. Ponurovskii, D. B. Stavrovskii, N. D. Grishnova, A. I. Nadezhdinskii
Publikováno v:
Inorganic Materials. 56:1284-1289
We present our findings on the use of diode laser spectroscopy (DLS) for monitoring СО2, Н2О, СН4, C2H2, C2H4, NH3, and other gas impurities during low-temperature fractional distillation purification of gaseous hydrides. We demonstrate a lineu
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 3, Pp 67-80 (2019)
Despite the fact that aviation gas turbine engines (GTE) have reached a high degree of sophistication, requirements for the improvement of their efficiency are constantly increasing. Reduction of specific fuel consumption and specific weight of the e
Publikováno v:
2020 International Multi-Conference on Industrial Engineering and Modern Technologies (FarEastCon).
Finding the right engine for a given aircraft is a complicated task itself. Small-scale engines feature extra complexity as the Reynolds number is an additional factor that impacts their efficiency and is to be taken into the account during the optim