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 |
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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