This patent application discloses a helicopter having a torque- correcting thruster device. The helicopter has an aerodynamic body which has opposite side portions, a top portion and a bottom portion. The aerodynamic body has a cockpit and a pilot seat in the cockpit. The helicopter includes landing gear attached to the bottom portion of the aerodynamic body. The helicopter includes a rotor that is supported by the aerodynamic body and a rotor blade attached to the rotor, and a thruster device operative on one of the side portions of the aerodynamic body to produce an aft-directed thrust that counteracts the torque produced by rotation of the rotor blade so as to control the yaw of the helicopter. The aft- directed thrust simultaneously supplements the forward thrust of the helicopter.
Helicopter with Torque-Correcting Thruster Device
2005
30 pages
Report
Keine Angabe
Englisch
Preliminary Evaluation of a Diffuser Thruster for Use as a Helicopter Anti-Torque System
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