A landing gear assembly is provided. The landing gear assembly includes a shock strut. The shock strut includes a shock strut cylinder (204) and a shock strut piston slidably disposed within the shock strut cylinder (204). The landing gear assembly further includes a temperature control unit assembly (250) disposed within the shock strut cylinder (204). The temperature control unit assembly (250) is configured to, responsive to a temperature within the shock strut cylinder (204) falling below a predetermined temperature, circulate heated fluid into a chamber of the shock strut cylinder (204) to heat gas within the shock strut cylinder (204).
TEMPERATURE COMPENSATED LANDING GEAR SHOCK STRUT
TEMPERATURKOMPENSIERTER FAHRWERKFEDERBEIN
JAMBE DE AMORTISSEUR DE TRAIN D'ATTERRISSAGE À COMPENSATION DE TEMPÉRATURE
22.01.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |