发明名称 Estrutura de fuselagem para fuselagem de aeronave de material compósito, e, aeronave
摘要 <p>A fuselage structure for an aircraft fuselage in composite material and an aircraft including such a fuselage structure. The fuselage structure provides savings in mass while allowing grounding of electric systems, and with which substantial mechanical stiffness characteristics may be guaranteed. In the fuselage structure attachment modules provide an assembling function as well as an electric function.</p>
申请公布号 BRPI0817758(A2) 申请公布日期 2015.03.24
申请号 BR2008PI17758 申请日期 2008.09.29
申请人 AIRBUS OPERATIONS 发明人 GUILLAUME GALLANT;LAURENT GIUSEPPIN;DAMIEN AGUERA
分类号 B64C1/12;B64C1/06 主分类号 B64C1/12
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