A system (401) for use with a tripod landing gear assembly of an aircraft may comprise: a tension strut assembly (450) having a tension strut (452) extending from an upper end to a lower end; a drag brace assembly (402) having an upper brace and a lower brace, the upper brace pivotably coupled to the lower brace at a center point, the lower brace rotatably coupled to the lower end of the tension strut; and a jury linkage (414) pivotally coupled to the drag brace assembly at the center point rotatably coupled to a middle portion of the tension strut, the middle portion between the upper end and the lower end.
TRIPOD LANDING GEAR ASSEMBLY
DREIBEINIGE FAHRWERKSANORDNUNG
ENSEMBLE TRÉPIED DE TRAIN D'ATTERRISSAGE
2021-10-20
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |