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
2022-09-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |