发明名称
摘要 An engine (101) propels the aircraft. A fuel cell (102) supplies electric energy to the aircraft. A kerosene reservoir (103) supplies the engine with engine fuel. A hydrogen reservoir (104) supplies the fuel cell with fuel cell fuel. The kerosene reservoir is decoupled and arranged separately from the hydrogen reservoir.
申请公布号 JP2008521693(A) 申请公布日期 2008.06.26
申请号 JP20070543788 申请日期 2005.12.02
申请人 发明人
分类号 B64D41/00;B64D11/00;B64D13/06;B64D15/02 主分类号 B64D41/00
代理机构 代理人
主权项
地址