发明名称 CARENAGE AERODYNAMIQUE ARRIERE DE MAT DE MOTEUR D'AERONEF
摘要 The fairing has a structural framework (59) formed in outwardly to a fairing section. The framework comprises an end portion (E5), and is recessed in continuity of a lower longitudinal element (L3) between an end portion (P3) of the lower longitudinal element and ends of a transverse rib (50). The framework is extended between a lower side element and an upper side (L1) of a straight central portion (29) inclining with respect to the end portion to another end portion (E4), which is positioned continuity against a portion (P1) of the upper side and parallel to the former end portion.
申请公布号 FR2982845(B1) 申请公布日期 2013.12.20
申请号 FR20110060650 申请日期 2011.11.22
申请人 AIRBUS OPERATIONS SAS 发明人 MACHADO STEPHANE;RAISON FABIEN;ROMANI STEPHANE
分类号 B64D29/00 主分类号 B64D29/00
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