发明名称 |
Fuselage structure for an aircraft fuselage in composite material and aircraft equipped with such a fuselage structure |
摘要 |
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.
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申请公布号 |
US8550399(B2) |
申请公布日期 |
2013.10.08 |
申请号 |
US20080681836 |
申请日期 |
2008.09.29 |
申请人 |
GALLANT GUILLAUME;GIUSEPPIN LAURENT;AGUERA DAMIEN;AIRBUS OPERATIONS (S.A.S.) |
发明人 |
GALLANT GUILLAUME;GIUSEPPIN LAURENT;AGUERA DAMIEN |
分类号 |
B64C1/00 |
主分类号 |
B64C1/00 |
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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