| 摘要 |
This invention discloses a helicopter that can directly propel rotors into the hovering state with drive, comprising a fuselage (13), a rotor (5) with a pull rod and jackstay (2), a turbine (1), a pair of wings (14), a hollow short shaft (37), a hollow short dead axle (36) with a bearing and a base (7), a plurality of throttle lines (35), a plurality of wires (34), a fuel delivery pipe (30), a hydraulic system, a axle sleeve (4) and a root axle (3), wherein the centrifugal-force-resistant turbine (1) directly drives the two-symmetrical-blade rotor (5), the turbine (1) is installed on the hollow short shaft (37), the hollow short shaft (37) is installed inside the hollow short dead axle (36), the hollow short dead axle (36) is fixed beside a root of the rotor (5), the hydraulic system controls a propelling direction of the turbine, the throttle lines (35), the wires (34) and the fuel delivery pipe (30) pass through the hollow short shaft (37) and are received in a crossbeam of the rotor, the axle sleeve (4) of the rotor is installed on the hollow dead axle (36), and hinged with the root axle (3) and the pull rod and jackstay (2), the base (7) is fixed on the back of a gravity center of the fuselage (13), pipelines are led to a underneath of the base and connected with a control system, and steering, outward pushing, positioning and propelling control is provided by a drive under the wings (14) or the fuselage (13).
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