发明名称 |
FUSELAGE ELEMENT COMPRISING A FUSELAGE SEGMENT AND JOINING MEANS |
摘要 |
The invention relates to a fuselage element comprising a fuselage segment (1a) comprising a skin (3a), and junction means (6) for connecting the skin of said segment (1a) to an adjacent segment (1b). The segment (1a) extends along the longitudinal axis (X) of the fuselage, and the skin (3) includes at least one first section (10) at least one end of said segment (1a). The fuselage segment (1a) comprises at least one longitudinal stiffening element (5a) for the fuselage. The junction means (60) are arranged so as to contact an outer surface (30) of said first section (10) of the skin (3a), and the stiffening element (5a) partially extends at the junction means (6) along the longitudinal axis (X).
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申请公布号 |
US2012104170(A1) |
申请公布日期 |
2012.05.03 |
申请号 |
US201013381673 |
申请日期 |
2010.07.02 |
申请人 |
GALLANT GUILLAUME;DELAHAYE ROMAIN;DUGERIE MARC;CASTANET MARC-ANTOINE;AIRBUS OPERATIONS (SAS) |
发明人 |
GALLANT GUILLAUME;DELAHAYE ROMAIN;DUGERIE MARC;CASTANET MARC-ANTOINE |
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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