Fuel feed system of airplane
作者： Hidefumi Saito , 英文 斎藤 , 宗浩 林 , Munehiro Hayashi
DOI:
关键词: Hydrogen fuel 、 Thrust specific fuel consumption 、 Hydrogen fuel enhancement 、 Aircraft fuel system 、 Automotive engineering 、 Engineering 、 Vapor lock 、 Brake specific fuel consumption 、 Range (aeronautics) 、 Fuel efficiency
摘要: PROBLEM TO BE SOLVED: To provide a fuel feed system providing highly efficient consumption without increasing the weight in an aircraft mounting Brayton cycle heat engine for flying and propulsion cells power interior. SOLUTION: Hydrogen obtained by converting molecular structure of hydrocarbon residual are fed to jet respectively so as efficiently obtain interior propulsion.
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