Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Ya A Ostapyuk"'
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
Publikováno v:
Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering. :41-53
The paper presents a procedure for selecting work cycle parameters and describes thermodynamic design of a small-scale gas turbine engine family consisting of a small-scale gas turbine engine and a gas turbine plant comprising a free turbine driving
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::85374b8901ef16a6c02f1aeb62c864cf
https://doi.org/10.18698/0236-3941-2019-3-41-53
https://doi.org/10.18698/0236-3941-2019-3-41-53
Autor:
Ilia N. Krupenich, V. S. Kuz'michev, H H Omar, Yu A Tkachenko, Evgeniy P. Filinov, Ya A Ostapyuk
Publikováno v:
Journal of Physics: Conference Series. 1891:012011
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::140ce45e3fe7fc516c1364337a202700
https://doi.org/10.1088/1742-6596/1891/1/012011
https://doi.org/10.1088/1742-6596/1891/1/012011
Publikováno v:
MATEC Web of Conferences, Vol 220, p 03001 (2018)
This article describes the multi-level approach to developing the virtual testing rig of gas turbine engines and power plants. The described virtual rig is developed on the basis of computer-aided system of thermogasdynamic calculations and analysis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::81b46d751196889b77219c0853eb39da
https://doi.org/10.18502/keg.v3i4.2245
https://doi.org/10.18502/keg.v3i4.2245
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 302:012022
This article describes how the thrust level influences the turbojet architecture (types of turbomachines that provide the maximum efficiency) and its working process parameters (turbine inlet temperature (TIT) and overall pressure ratio (OPR)). Funct
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::41214c4e6acc031bfba4ea6cfa5e42cc
https://doi.org/10.1088/1757-899x/302/1/012022
https://doi.org/10.1088/1757-899x/302/1/012022
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 302:012038
The article describes the approach for axial turbine modeling along the mean line. It bases on the developed model of an axial turbine blade row. This model is suitable for both nozzle vanes and rotor blades simulations. Consequently, it allows the s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::949df7c0552392e20f27288dc76b3326
https://doi.org/10.1088/1757-899x/302/1/012038
https://doi.org/10.1088/1757-899x/302/1/012038
Publikováno v:
IOP Conference Series: Materials Science & Engineering; Feb2018, Vol. 302 Issue 1, p1-1, 1p