发明申请
US20120256042A1 HELICOPTER WITH CYCLOIDAL ROTOR SYSTEM 有权
直升机与循环转子系统

HELICOPTER WITH CYCLOIDAL ROTOR SYSTEM
摘要:
The invention is related to a helicopter (10) comprising a main rotor (12), a cycloidal rotor (14) and a rotating cylinder (18). The rotating cylinder (18) extends along a longitudinal axis of a tail boom (13). The cycloidal rotor (14) extends at least partly along said same tail boom (13) and rotates outside the rotating cylinder (18).
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