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).
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
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