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
23.06.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
ADAPTIVE LANDING GEAR ASSEMBLY FOR ROTARY WING AIRCRAFT
Europäisches Patentamt | 2016
|ADAPTIVE LANDING GEAR ASSEMBLY FOR ROTARY WING AIRCRAFT
Europäisches Patentamt | 2018
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