发明名称 CONNECTION OF A FUSELAGE TO AN AIRCRAFT WING
摘要 A wing box rib (13), joining an aircraft wing (3) to the wing box and to the rest of the structure, extends advantageously over an adjacent part of the fuselage (2), having in particular an upper line (14) situated above a junction line (15) of the wing upper surface panel (3). The connection is simplified, as is the structure of the aircraft and its manufacture, a lightening is possible, and the transmission of stresses takes place in a more favourable manner.
申请公布号 US2012286090(A1) 申请公布日期 2012.11.15
申请号 US201213428291 申请日期 2012.03.23
申请人 AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE) 发明人 GUITTARD DOMINIQUE;EVE OLIVIER;FORT FREDERIC;COLMAGRO JEROME;LOYANT FRANCOIS
分类号 B64C1/26 主分类号 B64C1/26
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