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Low-Emission Operation of Aeroderivative Gas-Turbine Combustor over a Wide Range of Ambient Conditions

التفاصيل البيبلوغرافية
العنوان: Low-Emission Operation of Aeroderivative Gas-Turbine Combustor over a Wide Range of Ambient Conditions
المؤلفون: A. G. Tumanovskii, A. M. Sipatov, L. A. Bulysova, M. N. Gutnik, A. D. Nugumanov, V. D. Vasil’ev
المصدر: Power Technology and Engineering. 54:93-95
بيانات النشر: Springer Science and Business Media LLC, 2020.
سنة النشر: 2020
مصطلحات موضوعية: Gas turbines, geography, geography.geographical_feature_category, Nuclear engineering, Fuel supply, Energy Engineering and Power Technology, 02 engineering and technology, Inlet, 01 natural sciences, 010305 fluids & plasmas, 020401 chemical engineering, Low emission, Range (aeronautics), 0103 physical sciences, Combustor, Environmental science, 0204 chemical engineering, Gas compressor
الوصف: The capabilities of controlling a low-emission combustor (LEC) over a wide range of ambient conditions are analyzed. The LES is intended for a GTU-16P gas turbine that is a derivative of the PS-90A aircraft engine by the UEC Aviadvigatel company. The LEC is of premix swirl stabilized type based on GTE-110 prototype. Its burner consists of pilot and main burners. The main burner has two fuel supply channels that allow controlling the quality of the air-fuel mixture. The low-emission operation range of the LEC can be extended to 70% load at negative ambient temperatures by bleeding air to the compressor inlet.
تدمد: 1570-1468
1570-145X
URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::91782908c1a78fc61e546074bb8d04df
https://doi.org/10.1007/s10749-020-01173-3
حقوق: CLOSED
رقم الأكسشن: edsair.doi...........91782908c1a78fc61e546074bb8d04df
قاعدة البيانات: OpenAIRE
الوصف
تدمد:15701468
1570145X