초록 ▼

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 porti

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.

대표청구항 ▼

What is claimed is: 1. A helicopter comprising: an aerodynamic body having opposite side portions, a top portion and a bottom portion, the aerodynamic body having a cockpit: a pilot seat in the cockpit; landing gear attached to the bottom portion of the aerodynamic body; a rotor supported by the ae

What is claimed is: 1. A helicopter comprising: an aerodynamic body having opposite side portions, a top portion and a bottom portion, the aerodynamic body having a cockpit: a pilot seat in the cockpit; landing gear attached to the bottom portion of the aerodynamic body; a rotor supported by the aerodynamic body, the rotor having a portion extending from the top portion of the aerodynamic body; rotor blades attached to the portion of the rotor that extends from the top portion of the aerodynamic body, the rotor blades rotating above the aerodynamic body wherein rotation of the rotor blades produces a torque; 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 to control a yaw of the helicopter and supplement forward thrust of the helicopter wherein the thruster device includes an air intake port and an exhaust port, and wherein the thruster device is incorporated into the aerodynamic body, the aerodynamic body having openings therein that are aligned with the air intake and exhaust ports of the thruster device. 2. The helicopter according to claim 1 wherein the thruster device comprises a jet engine. 3. A helicopter comprising: an aerodynamic body having opposite side portions, a top portion and a bottom portion, the aerodynamic body having a cockpit; a pilot seat in the cockpit; landing gear attached to the bottom portion of the aerodynamic body; a rotor supported by the aerodynamic body, the rotor having a portion extending from the top portion of the aerodynamic body; rotor blades attached to the portion of the rotor that extends from the top portion of the aerodynamic body, the rotor blades rotating above the aerodynamic body wherein rotation of the rotor blades produces a torque; a thruster device operative on one of the side portions of the aerodynamic body to produce an aft-directed thrust that counteracts the torque to control a yaw of the helicopter and supplement forward thrust of the helicopter; and a balancing device attached to the side portion of the aerodynamic body that is opposite the side portion on which the thrusting device is operative so as to balance the helicopter. 4. A helicopter comprising: an aerodynamic body having opposite side portions, a top portion and a bottom portion, the aerodynamic body having a cockpit; a pilot seat in the cockpit; landing gear attached to the bottom portion of the aerodynamic body; a rotor supported by the aerodynamic body, the rotor having a portion extending from the top portion of the aerodynamic body; rotor blades attached to the portion of the rotor that extends from the top portion of the aerodynamic body, the rotor blades rotating above the aerodynamic body wherein rotation of the rotor blades produces a torque; 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 to control a yaw of the helicopter and supplement forward thrust of the helicopter; wherein the pilot's seat is offset to the side portion of the aerodynamic body that is opposite the side portion on which the thrusting device is operative so as to balance the helicopter.