发明名称
摘要 PROBLEM TO BE SOLVED: To provide a small power generator for a missile, capable of operating for a long time. SOLUTION: A large amount of hydrogen contained in fuel gas generated in a primary combustion chamber 5 of ducted rocket engine 2 acting as a propulsion device of the missile is supplied to a fuel cell 10 to generate power. Since the ducted rocket engine 2 is an engine capable of operating until the missile 1 bits a target, power is continuously generated during operation of the missile, and by commonly using fuel, miniaturization is made possible, and the space inside the missile can be saved.
申请公布号 JP3941381(B2) 申请公布日期 2007.07.04
申请号 JP20000346770 申请日期 2000.11.14
申请人 发明人
分类号 F42B15/00;H01M8/06;F02K9/78;H01M8/00;H01M8/04;H01M8/08;H01M8/10 主分类号 F42B15/00
代理机构 代理人
主权项
地址