Flight control surface comprising:- a main body (1) comprising an upper and lower cover (3, 4), upper and lower skins (5, 6, 7, 8) and a core member (9, 10), a prolongation (12) of their length over the length of the core member (9, 10) defining a stepped area (16),- a trailing edge (2) comprising a U-shaped profile (11) enclosing the prolongation (12),- the U-shaped profile (11) extending towards the main body in the chordwise direction up to the stepped area (16) and comprising a section that progressively decreases,the trailing edge (2) comprising a first and a second set of rivets (13, 14) located in the prolongation (12), the first set of rivets (14) joining the upper (3) and lower (4) covers and the second set of rivets (13) joining the U-shaped profile (11), the upper (3) and lower (4) covers.
FLIGHT CONTROL SURFACE FOR AN AIRCRAFT AND METHOD FOR MANUFACTURING SAID FLIGHT CONTROL SURFACE
FLUGSTEUERUNGSFLÄCHE FÜR EIN FLUGZEUG UND VERFAHREN ZUR HERSTELLUNG DER FLUGSTEUERUNGSFLÄCHE
SURFACE DE COMMANDE DE VOL POUR AÉRONEF ET PROCÉDÉ DE FABRICATION DUDIT DE SURFACE DE COMMANDE DE VOL
2021-07-28
Patent
Elektronische Ressource
Englisch
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