A support structure to mount landing gear to a wing spar of an aircraft. The support structure includes a trunnion assembly having a first trunnion and a second trunnion 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
2022-09-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |