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1. (WO2010112648) INTEGRATION OF AN AIRCRAFT FAIRING

Pub. No.:    WO/2010/112648    International Application No.:    PCT/ES2010/070160
Publication Date: Fri Oct 08 01:59:59 CEST 2010 International Filing Date: Fri Mar 19 00:59:59 CET 2010
IPC: B64C 7/00
B64C 1/26
F16B 5/02
Applicants: AIRBUS OPERATIONS, S.L.
LOBO BARROS, Abel
LOZANO GARCÍA, José Luis
Inventors: LOBO BARROS, Abel
LOZANO GARCÍA, José Luis
Title: INTEGRATION OF AN AIRCRAFT FAIRING
Abstract:
Structure for the coupling of the fairing (7) of an aircraft, said fairing (7) being located between the horizontal stabilizer and the vertical stabilizer or fuselage section (6) of said aircraft, said structure comprising angled fittings (2), said fittings in turn comprising a vertical surface and a horizontal surface, the vertical surface of the fittings (2) being connected to the fairing (7) by means of detachable fastening elements (12), said structure further comprising a deformable elastic element (13) between the fairing (7) and the vertical surface of the fitting (2) such that said elastic element (13) is capable of absorbing the necessary deformation clearance and the manufacturing and assembly tolerances of the fittings (2), of the fairing (7), of the horizontal stabilizer and of the vertical stabilizer or fuselage section (6) by means of tightening the above elements to various torques.