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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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