An adaptive landing gear assembly for a rotary wing aircraft, the adaptive landing gear assembly including a controller; a first landing gear support having a first ground contact element; and a second landing gear support having a second ground contact element; the controller independently controlling the first landing gear support and the second landing gear support.
ADAPTIVE LANDING GEAR ASSEMBLY FOR ROTARY WING AIRCRAFT
24.05.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
ADAPTIVE LANDING GEAR ASSEMBLY FOR ROTARY WING AIRCRAFT
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