A process for assembling portions of an aeronautical wing, in which a wing covering is assembled with carrier structural elements, allows the simultaneous application of all filling tapes on an exposed surface, by speeding-up and making more reliable the process itself. The process includes: placing side by side the structural elements longitudinally, to form the spars, by determining a flat surface, having a plurality of longitudinal junctions, faced upwards; adhering to the longitudinal junctions respective filling tapes; translating and rotating by 180° the structural elements in one single solution, by keeping them fixed in the mutual positions thereof and by transferring them above an inner surface of a wing covering; and translating the structural elements in one single solution, by keeping them fixed in the mutual positions thereof, downwards, by making the flat surface thereof to coincide with said inner surface.
PROCESS FOR ASSEMBLING PORTIONS OF AN AERONAUTICAL WING
VERFAHREN ZUR MONTAGE VON TEILEN EINES AERONAUTISCHEN FLÜGELS
PROCÉDÉ D'ASSEMBLAGE DE PORTIONS D'UNE AILE AÉRONAUTIQUE
2021-12-29
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 / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge |
Modular wing portions, wing assemblies and methods of assembling the same
European Patent Office | 2025
|