发明名称 Method of producing a joining structure for an aircraft fairing
摘要 <p>Joining structure for aircraft fairing (7), said fairing (7) being arranged between the horizontal stabilizer and the vertical stabilizer or fuselage section (6) of said aircraft, said structure comprising fittings (2) in the shape of angle, said fittings in turn comprising a vertical surface and a horizontal surface, the fittings (2) being joined via their vertical surface to the fairing (7) by means of removable fixing parts (12), said structure also comprising a deformable resilient element (13) between the fairing (7) and the vertical surface of the fitting (2), such that said resilient element (13) is able to compensate for the necessary deformation play and the manufacturing and assembly tolerances of the fittings (2), the fairing (7), the horizontal stabilizer and the vertical stabilizer or fuselage section (6) by means of different torques for tightening of the above parts.</p>
申请公布号 EP2415668(B1) 申请公布日期 2014.01.08
申请号 EP20100713348 申请日期 2010.03.18
申请人 AIRBUS OPERATIONS, S.L. 发明人 LOBO BARROS, ABEL;LOZANO GARCIA, JOSE LUIS
分类号 B64C7/00;B64C1/26;F16B5/02 主分类号 B64C7/00
代理机构 代理人
主权项
地址