A support structure (10) to mount landing gear (90) to a wing spar (104) of an aircraft. The support structure includes a trunnion assembly (18) having a first trunnion (20) and a second trunnion (30) that are connected together with the first trunnion positioned on a first side of the wing spar and a second trunnion positioned on an opposing second side of the wing spar. The trunnion assembly is configured to support a first section of the landing gear.
SUPPORT STRUCTURE FOR AN AIRCRAFT LANDING GEAR
TRAGSTRUKTUR FÜR EIN FLUGZEUGFAHRWERK
STRUCTURE DE SUPPORT POUR UN TRAIN D'ATTERRISSAGE D'AÉRONEF
21.09.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |