Factors Determining the Flame Configuration and Affecting Combustion Stability in Gas-Turbine Combustors

Autor:	A. G. Tumanovskii, M. N. Gutnik, L. A. Bulysova, V. D. Vasil’ev
Rok vydání:	2020
Předmět:	geography geography.geographical_feature_category Flow velocity Atmospheric pressure Range (aeronautics) Nuclear engineering Combustor Energy Engineering and Power Technology Exhaust gas Environmental science Combustion Inlet Stability (probability)
Zdroj:	Power Technology and Engineering. 54:537-540
ISSN:	1570-1468 1570-145X
DOI:	10.1007/s10749-020-01247-2
Popis:	The possibilities of influencing combustion stability during changeover to low-emission combustion and ways of extending the stable combustion range are analyzed. The flow velocity, temperature, and pressure in the low-emission combustor (LEC) are considered as influencing factors. A premixed swirl-stabilized combustor is considered. The burner unit consists of main and pilot burners. The main burner has two fuel channels that allow controlling the quality of the air-fuel mixture. The LEC developed for an aeroderivative gas turbine was tested at an inlet air pressure of 2 MPa and an inlet air temperature of 475°C and an exhaust gas temperature of up to 1320°C.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::1822ec422d41dd91fd736729e4099c71 https://doi.org/10.1007/s10749-020-01247-2 Zobrazit plný text záznamu Full text from SpringerLink