An example aircraft wing disclosed herein includes a rear spar (200) having a rear side (306) and a front side (308) opposite the rear side, a side-of-body rib (502) coupled to the rear spar, a rib post (510) disposed on the front side of the rear spar, where the rib post is to couple a second rib (508) to the rear spar, a side-of-body fitting (516) coupled to the side-of-body rib, an intercostal member (518) coupled between the side-of-body fitting and the rib post, and a drag brace fitting (216) disposed on the rear side of the rear spar. The drag brace fitting is coupled to the rib post and the side-of-body fitting via a first plurality of fasteners (310(a,b)) extending through the rear spar.
AIRCRAFT MAIN LANDING GEAR DRAG BRACE BACKUP FITTING ASSEMBLIES AND RELATED METHODS
BACKUP-MONTAGEANORDNUNGEN FÜR EINE FLUGZEUGHAUPTFAHRWERKSKNICKSTREBE UND ZUGEHÖRIGE VERFAHREN
ENSEMBLES DE FIXATION DE RENFORT DE CONTREFICHE DE TRAIN D'ATTERRISSAGE PRINCIPAL D'AÉRONEF ET PROCÉDÉS ASSOCIÉS
2023-12-20
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT MAIN LANDING GEAR DRAG BRACE BACKUP FITTING ASSEMBLIES AND RELATED METHODS
European Patent Office | 2020
|Aircraft main landing gear drag brace backup fitting assemblies and related methods
European Patent Office | 2021
|AIRCRAFT MAIN LANDING GEAR DRAG BRACE BACKUP FITTING ASSEMBLIES AND RELATED METHODS
European Patent Office | 2020
|