Method for applying a cover (1) to an aircraft wing (2) comprising placing a skin (3) provided with one or more manholes (4) on the aircraft wing (2); placing a gasket (5) for the, or each, manhole (4) of the skin (3); placing a plug (6) in the, or each, manhole (4); and curing the aircraft wing (2) with the cover (1), the cover (1) comprising the skin (3), the gasket or gaskets (5) and the plug or plugs (6).The aircraft wing (2) comprises a cover (1) applied by said method including a skin (3), one or more gaskets (5) and one or more plugs (6).It reduces the application time, the recurrent costs and has a positive environmental footprint impact.
METHOD FOR APPLYING A COVER TO AN AIRCRAFT WING AND AIRCRAFT WING OBTAINED BY SAID METHOD
VERFAHREN ZUM AUFBRINGEN EINER ABDECKUNG AUF EINEN FLUGZEUGFLÜGEL UND DURCH DIESES VERFAHREN ERHALTENER FLUGZEUGFLÜGEL
PROCÉDÉ D'APPLICATION D'UN CAPOT SUR UNE AILE D'AÉRONEF ET AILE D'AÉRONEF OBTENUE PAR LEDIT PROCÉDÉ
2024-06-05
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
METHOD FOR APPLYING A COVER TO AN AIRCRAFT WING AND AIRCRAFT WING OBTAINED BY SAID METHOD
Europäisches Patentamt | 2024
|AIRCRAFT WING TORSION BOX, AIRCRAFT WING AND AIRCRAFT
Europäisches Patentamt | 2019
|Aircraft wing trailing edge closing device, aircraft wing and aircraft wing drag reduction method
Europäisches Patentamt | 2023
|