A system and method are provided to automate the assembly of a wing panel, such as utilized by commercial aircraft. In the context of a system, a tacking cell is provided that is configured to tack one or more stringers to a skin plank. The system also includes a riveting cell configured to receive a tacked plank from the tacking cell and to rivet the one or more stringers to the skin plank. The system also includes a splicing cell configured to receive a plurality of riveted planks from the riveting cell and to attach one or more splice stringers to the plurality of riveted planks. Further, the system includes a side of body cell configured to receive a spliced panel from the splicing cell and to attach a side of body chord thereto to produce a wing panel.
SYSTEM AND METHOD FOR MANUFACTURING A WING BOX
AUFBAU UND METHODE FÜR DIE HERSTELLUNG EINES FLÜGELKASTENS
SYSTÈME ET PROCEDE DE FABRICATION D'UNE BOÎTE D'AILE
2017-10-04
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 / B21J FORGING , Schmieden / B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL |
WING RIB, WING HAVING WING RIB, AND METHOD FOR MANUFACTURING WING RIB
European Patent Office | 2019
|Flapping-wing flexible wing and manufacturing method thereof
European Patent Office | 2021
|Wing unit, wing flapping apparatus, and method of manufacturing wing unit
European Patent Office | 2022
|