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
30.10.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |