A method for manufacturing a connecting part between a wing box and a leading edge module. The method comprises performing a three-dimensional scanning of a first representative part of the wing box to obtain a first computer model and performing a three-dimensional scan of a second representative part of the leading edge module in order to obtain a second computer model. The first part comprises a first reference region and a first connecting region, the second part comprises a second reference region and a second connecting region. A relative position of the first reference region is defined with respect to the reference region. From the first and second computer model, the connecting part is configured to connect the first and the second connecting region such that the first and the second reference region are located in said relative position. The connecting part is then manufactured.
ATTACHEMENT RAPIDE POUR UN MODULE DE VOLET MOBILE D'UNE AILE D'UN AERONEF
RAPID ATTACHMENT FOR A MOVABLE FLAP MODULE OF A WING OF AN AIRCRAFT
SCHNELLBEFESTIGUNG FÜR EIN BEWEGLICHES KLAPPENMODUL EINES FLÜGELS EINES FLUGZEUGS
14.08.2024
Patent
Elektronische Ressource
Französisch
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