Method for manufacturing the trailing edge ribs (1) and the bearing ribs (2) of trailing edges (3) of aircraft lifting surfaces, in which the trailing edge ribs (1) and the bearing ribs (2) are made by joining simple C-shaped parts and/or simple L-shaped parts so as to obtain the final trailing edge ribs (1) and bearing ribs (2), such that the manufacturing of the simple C-shaped parts uses the same tooling both for the trailing edge ribs (1) and the bearing ribs (2), and the manufacturing of the simple L-shaped parts uses the same tooling both for the trailing edge ribs (1) and the bearing ribs (2).
METHOD FOR MANUFACTURING THE TRAILING EDGE RIBS AND THE BEARING RIBS OF TRAILING EDGES OF AIRCRAFT LIFTING SURFACES
VERFAHREN ZUR HERSTELLUNG DER HINTERKANTENRIPPEN UND DER AUFLAGERIPPEN VON HINTERKANTEN VON FLUGZEUGHUBFLÄCHEN
PROCÉDÉ POUR FABRIQUER LE BORD DE FUITE DES NERVURES ET DES NERVURES DE SUPPORT DES BORDS DE FUITE DES SURFACES DE LEVAGE D'AÉRONEFS
2021-06-23
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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