An aircraft is provided including an airframe, an extending tail, and a counter rotating, coaxial main rotor assembly including an upper rotor assembly and a lower rotor assembly. A translational thrust system positioned at the extending tail, the translational thrust system providing translational thrust to the airframe. A cockpit in the airframe, the cockpit including two seats and a single collective control input positioned between the two seats.
SINGLE COLLECTIVE STICK FOR A ROTARY WING AIRCRAFT
2017-09-28
Patent
Electronic Resource
English
Collective flight control system for rotary wing aircraft
European Patent Office | 2018
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