A nose gear spin down apparatus includes a spin down device and a resistance device. The spin down device is rotatable about a central longitudinal axis. The spin down device rotates about the central longitudinal axis after engagement with a spinning nose gear wheel of an aircraft. The resistance device contacts the spin down device without imparting a resistance to the spin down device. The resistance device imparts the resistance to the spin down device after conditions are met.
Nose Gear Spin Down Apparatus
24.04.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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