发明名称 FUSELAGE REAR END OF AN AIRCRAFT
摘要 Fuselage rear end of an aircraft, comprising: - a structural part (1) comprising a skin and longitudinal (30) and transversal reinforcing members (31, 32), and - a fairing (5). The structural part (1) longitudinally spans over the whole rear end and comprises a first portion (2) in which the transversal reinforcing members (32) occupy the whole perimeter of the corresponding fuselage section and at least a second portion (3) in which the transversal reinforcing members (31) occupy only a portion of the perimeter of the corresponding fuselage section, the fairing (5) being located below the second portion (3) of the structural part (1).
申请公布号 WO2016107944(A1) 申请公布日期 2016.07.07
申请号 WO2015ES70934 申请日期 2015.12.21
申请人 AIRBUS OPERATIONS S.L. 发明人 ARÉVALO RODRÍGUEZ, ELENA;CRUZ DOMÍNGUEZ, FRANCISCO JOSÉ;MONEO PEÑACOBA, ANA REYES
分类号 B64C1/06;B64C1/14;B64C1/16;B64C1/26;B64C5/02;B64C7/00;B64D29/04;B64D29/08;B64D41/00 主分类号 B64C1/06
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