作者: Milton R. Adams , Klaus K.G. Huber , Harvey B. Jansen , Robert B. Sumegi , John A. Salisbury
DOI:
关键词: Combustion chamber 、 Automotive engineering 、 Internal combustion engine 、 External combustion engine 、 Engine efficiency 、 Combustor 、 Heat engine 、 Turbine 、 Engineering 、 Aircraft fuel system
摘要: ABSTRACT A recuperated gas turbine engine fuel control valve and method which controls flow during accelera-tion as a preselected empirical function of combustor gauge pressure inlet temperature, can also deceleration without interruption the combustion process.