A method for manufacturing a leading edge comprising a structure and at least one outer wall, the manufacturing method comprising a step of mounting of the structure and an assembly step aiming to link the structure and the outer wall during which the outer wall is held pressed against a conformation surface having a profile identical to a theoretical outer surface configured to limit aerodynamic disturbances. This manufacturing method makes it possible to improve the aerodynamic efficiencies of the leading edge thus obtained and of the aerodynamic aircraft profile incorporating same.
METHOD FOR MANUFACTURING A LEADING EDGE LIMITING AERODYNAMIC DISTURBANCES, A LEADING EDGE OBTAINED FROM THE METHOD AND AERODYNAMIC AIRCRAFT PROFILE COMPRISING SUCH A LEADING EDGE
2021-05-27
Patent
Electronic Resource
English
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B21D WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL , Bearbeiten oder Verarbeiten von Blechen, Metallrohren, -stangen oder -profilen ohne wesentliches Abtragen des Werkstoffs / B64C AEROPLANES , Flugzeuge |
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