发明名称 Aircraft with removable structural payload module
摘要 An aircraft includes a forward fuselage segment, an aft fuselage segment, a wing structure supported from the aft fuselage segment, a tail structure supported from either the aft fuselage segment or the wing structure, and an engine supported from either the aft fuselage segment or the wing structure. A payload module is disposed between and connects the forward fuselage segment and the aft fuselage segment, so as to form the structural attachment between the forward fuselage segment and the aft fuselage segment. The payload module is disconnectable from the forward fuselage segment and the aft fuselage segment such that the forward fuselage segment and the aft fuselage segment are not connected to each other when the payload module is disconnected from the forward fuselage segment and the aft fuselage segment.
申请公布号 US5975464(A) 申请公布日期 1999.11.02
申请号 US19980158186 申请日期 1998.09.22
申请人 SCALED COMPOSITES, INC. 发明人 RUTAN, ELBERT
分类号 B64C39/02;(IPC1-7):B64C1/00 主分类号 B64C39/02
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