发明名称 Tank module for a structurally integrated vacuum sewage system for aircraft
摘要 A tank module for an aircraft is designed for being fitted into the aircraft fuselage from outside. The tank module comprises at least one receptacle and a shell section that forms an outer end of the tank module and is connected to the receptacle. The shell section can be fitted into a fuselage opening in such a way that the receptacle is positioned in the interior of the aircraft fuselage.
申请公布号 US2010019088(A1) 申请公布日期 2010.01.28
申请号 US20060990367 申请日期 2006.08.03
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 HOFFJANN CLAUS;ZIEROLD WOLFGANG
分类号 B64D11/02 主分类号 B64D11/02
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