A helicopter has a main rotor with propeller blades which is driven by a rotor shaft and which is hinge-mounted to this rotor shaft. The angle between the surface of rotation of the main rotor and the rotor shaft may vary. A swinging manner on an oscillatory shaft is essentially transverse to the ro
A helicopter has a main rotor with propeller blades which is driven by a rotor shaft and which is hinge-mounted to this rotor shaft. The angle between the surface of rotation of the main rotor and the rotor shaft may vary. A swinging manner on an oscillatory shaft is essentially transverse to the rotor shaft of the main rotor and is directed transversally to the longitudinal axis of the vanes. The main rotor and the auxiliary rotor are connected to each other by a mechanical link. The swinging motions of the auxiliary rotor controls the angle of incidence (A) of at least one of the propeller blades of the main rotor. There are wings from the body and a stabilizer at the tail.
대표청구항▼
The invention claimed is: 1. A rotor assembly for a remote control toy helicopter, comprising a motor and a battery for the motor, the motor being controllable by a controller remote from the helicopter body; a main rotor having two propeller blades mounted on a rotor shaft for rotation with the ro
The invention claimed is: 1. A rotor assembly for a remote control toy helicopter, comprising a motor and a battery for the motor, the motor being controllable by a controller remote from the helicopter body; a main rotor having two propeller blades mounted on a rotor shaft for rotation with the rotor shaft, an auxiliary rotor mounted on the rotor shaft for rotation in the sense of rotation of the main rotor, the auxiliary rotor being mounted in a swinging relationship on an oscillatory shaft provided essentially transverse to the rotor shaft of the main rotor and the swinging motion being relatively upwardly and downwardly about the oscillatory shaft, the main rotor and the auxiliary rotor having planes of rotation spaced from each other and being linked with each other by a mechanical linkage, such that the swinging motion of the auxiliary rotor controls an angle of incidence of the propeller blades of the main rotor, and wherein the main rotor is pivotably mounted with a spindle which is fixed on the rotor shaft, and wherein each blade includes a convex curve in a profile on its top face from a position towards a leading edge towards a position towards a trailing edge, the convex curve preferably being present over a portion of the generally longitudinal length of the blade, and wherein the blade has a width between the leading edge and the trailing edge, and a length from a tip of the blade to the rotor shaft, the blade being rigid in a direction from the tip of the blade to a position where the blade is mounted with the spindle, and a fastening point on the main rotor being situated at a first distance from an axis of the spindle of the propeller blades of the main rotor, and a fastening point on the auxiliary rotor being situated at a second distance from the axis of the oscillatory shaft of the auxiliary rotor, and the first distance being larger than the second distance, and wherein the first distance is about double of the second distance, and the fastening point with the auxiliary rotor being removed from the auxiliary rotor by an arm extending from the auxiliary rotor and the first distance and the second distance being such that the mechanical linkage between the fastening points is located in a substantially parallel relationship relative to the rotor shaft. 2. A remote control toy helicopter including the rotor assembly according to claim 1 wherein the helicopter includes a body with a front end and a rear end; and a second rotor driven by a second rotor shaft located towards the rear end. 3. A remote control toy helicopter including a rotor assembly for a remote control toy helicopter, comprising a motor and a battery for the motor, the motor being controllable by a controller remote from the helicopter; a main rotor having two propeller blades mounted on a rotor shaft for rotation with the rotor shaft, an auxiliary rotor mounted on the rotor shaft for rotation in the sense of rotation of the main rotor, the auxiliary rotor being mounted in a swinging relationship on an oscillatory shaft provided essentially transverse to the rotor shaft of the main rotor and the swinging motion being relatively upwardly and downwardly about the oscillatory shaft, the main rotor and the auxiliary rotor having planes of rotation spaced from each other and being linked with each other by a mechanical linkage, such that the swinging motion of the auxiliary rotor controls an angle of incidence of the propeller blades of the main rotor, and wherein the main rotor is pivotably mounted with a spindle which is fixed on the rotor shaft, and wherein each blade includes a convex curve in a profile on its top face from a position towards a leading edge towards a position towards a trailing edge, the convex curve preferably being present over a portion of the generally longitudinal length of the blade, and wherein the blade has a width between the leading edge and the trailing edge, and a length from a tip of the blade to the rotor shaft, the blade being rigid in a direction from the tip of the blade to a position where the blade is mounted with the spindle, a fastening point on the main rotor being situated at a first distance from an axis of the spindle of the propeller blades of the main rotor, and a fastening point on the auxiliary rotor being situated at a second distance from the axis of the oscillatory shaft of the auxiliary rotor, and the first distance being larger than the second distance, and wherein a top surface of each blade is substantially smooth over essentially the greater part of the area of each blade, and wherein the first distance is about double of the second distance, and the fastening point with the auxiliary rotor being removed from the auxiliary rotor by the second arm extending from the auxiliary rotor and the first distance and the second distance being such that the mechanical linkage between the fastening points is located in a substantially parallel relationship relative to the rotor shaft. 4. A remote control toy helicopter according to claim 3 wherein the helicopter includes a front end and a rear end; and a second rotor driven by a second rotor shaft located towards the rear end. 5. A rotor assembly for a remote control toy helicopter, comprising a motor and a battery for the motor, the motor being controllable by a controller remote from the helicopter body; a main rotor having two propeller blades mounted on a rotor shaft for rotation with the rotor shaft, an auxiliary rotor mounted on the rotor shaft for rotation in the sense of rotation of the main rotor, the auxiliary rotor being mounted in a swinging relationship on an oscillatory shaft provided essentially transverse to the rotor shaft of the main rotor and the swinging motion being relatively upwardly and downwardly about the oscillatory shaft, the main rotor and the auxiliary rotor having planes of rotation spaced from each other and being linked with each other by a mechanical linkage, such that the swinging motion of the auxiliary rotor controls an angle of incidence of the propeller blades of the main rotor, and wherein the main rotor is pivotably mounted with a spindle which is fixed on the rotor shaft, and wherein each propeller blade includes a convex curve in a profile on its top face from a position towards a leading edge towards a position towards a trailing edge, the convex curve preferably being present over a portion of the generally longitudinal length of the propeller blade, and wherein the propeller blade has a width between the leading edge and the trailing edge, and a length from a tip of the propeller blade to the rotor shaft, the blade being rigid in a direction from the tip of the propeller blade to a position where the propeller blade is mounted with the spindle, and a first arm extending laterally in substantially the plane of rotation of the main rotor and from the main rotor axis, the first arm having a first fastening point to the main rotor being situated at a first distance from an axis of the spindle of the propeller blades of the main rotor, and a second arm formed with and extending from the auxiliary rotor laterally in substantially the plane of rotation of the auxiliary rotor and from the auxiliary rotor axis, the second arm having a second fastening point to the auxiliary rotor being situated at a second distance from the axis of the oscillatory shaft of the auxiliary rotor, and the first distance being larger than the second distance, and including the mechanical linkage between the first and the second fastening points, and the second fastening point being removed from the auxiliary rotor by the second arm extending from the auxiliary rotor and the first distance and the second distance being such that the mechanical linkage is located in a substantially parallel relationship relative to the rotor shaft, and wherein the first distance is about the double of the second distance. 6. A rotor assembly for a remote control toy helicopter, comprising a motor and a battery for the motor, the motor being controllable by a controller remote from the helicopter body; a main rotor having two propeller blades mounted on a rotor shaft for rotation with the rotor shaft, an auxiliary rotor mounted on the rotor shaft for rotation in the sense of rotation of the main rotor, the auxiliary rotor being mounted in a swinging relationship on an oscillatory shaft provided essentially transverse to the rotor shaft of the main rotor and the swinging motion being relatively upwardly and downwardly about the oscillatory shaft, the main rotor and the auxiliary rotor having planes of rotation spaced from each other and being linked with each other by a mechanical linkage, such that the swinging motion of the auxiliary rotor controls an angle of incidence of the propeller blades of the main rotor, and wherein the main rotor is pivotably mounted with a spindle which is fixed on the rotor shaft, and wherein each propeller blade includes a convex curve in a profile on its top face from a position towards a leading edge towards a position towards a trailing edge, and wherein the blade has a width between the leading edge and the trailing edge, and a length from a tip of the propeller blade to the rotor shaft, the blade being rigid in a direction from the tip of the propeller blade to a position where the propeller blade is mounted with the spindle, and a first arm extending laterally in substantially the plane of rotation of the main rotor and from the main rotor axis, the first arm having a first fastening point to the main rotor being situated at a first distance from an axis of the spindle of the propeller blades of the main rotor, and a second arm extending from the auxiliary rotor laterally in substantially the plane of rotation of the auxiliary rotor and from the auxiliary rotor axis, the second arm having a second fastening point to the auxiliary rotor being situated at a second distance from the axis of the oscillatory shaft of the auxiliary rotor, and including the mechanical linkage between the first and the second fastening points, and the second fastening point being removed from the auxiliary rotor by the second arm extending from the auxiliary rotor and the first distance and the second distance being such that the mechanical linkage is located in a substantially parallel relationship relative to the rotor shaft, and wherein the first distance is about the double of the second distance. 7. A remote control toy helicopter including the rotor assembly according to claim 5 wherein the helicopter includes a body with a front end and a rear end; and a second rotor driven by a second rotor shaft located towards the rear end. 8. A remote control toy helicopter including the rotor assembly according to claim 6 wherein the helicopter includes a body with a front end and a rear end; and a second rotor driven by a second rotor shaft located towards the rear end. 9. A remote control toy helicopter including the rotor assembly according to claim 5 wherein the helicopter includes a body with a front end and a rear end; and a tail extending from the body. 10. A remote control toy helicopter including the rotor assembly according to claim 6 wherein the helicopter includes a body with a front end and a rear end; and a tail extending from the body. 11. A remote control toy helicopter including the rotor assembly according to claim 5 wherein the arm from the main blade extends from the blade at a position longitudinally removed from the rotor shaft. 12. A remote control toy helicopter including the rotor assembly according to claim 6 wherein the arm from the main blade extends from the blade at a position longitudinally removed from the rotor shaft. 13. A remote control toy helicopter including the rotor assembly according to claim 5 wherein the arm from the vane extends from the vane at a position longitudinally removed from the rotor shaft. 14. A remote control toy helicopter including the rotor assembly according to claim 6 wherein the arm from the vane extends from the vane at a position longitudinally removed from the rotor shaft. 15. A remote control toy helicopter including the rotor assembly according to claim 5 wherein the angle between the longitudinal axis of the main blade and the longitudinal axis of the vane is an acute angle. 16. A remote control toy helicopter including the rotor assembly according to claim 6 wherein the angle between the longitudinal axis of the main blade and the longitudinal axis of the vane is an acute angle. 17. A remote control toy helicopter including the rotor assembly according to claim 7 wherein the angle between the longitudinal axis of the main blade and the longitudinal axis of the vane is an acute angle. 18. A remote control toy helicopter including the rotor assembly according to claim 8 wherein the angle between the longitudinal axis of the main blade and the longitudinal axis of the vane is an acute angle. 19. A remote control toy helicopter including the rotor assembly according to claim 7 wherein the first arm is formed with main rotor and the second arm is formed with the auxiliary rotor. 20. A remote control toy helicopter including the rotor assembly according to claim 8 wherein the first arm is formed with main rotor and the second arm is formed with the auxiliary rotor. 21. A rotor assembly for a remote control toy helicopter according to claim 1, wherein the substantially parallel relationship exists when the blade and the vane are inclined in respective planes that are substantially parallel with each other. 22. A remote control toy helicopter including the rotor assembly according to claim 3 wherein the substantially parallel relationship exists when the blade and the vane are inclined in respective planes that are substantially parallel with each other. 23. A remote control toy helicopter including the rotor assembly according to claim 5 wherein the substantially parallel relationship exists when the blade and the vane are inclined in respective planes that are substantially parallel with each other. 24. A remote control toy helicopter including the rotor assembly according to claim 6 wherein the substantially parallel relationship exists when the blade and the vane are inclined in respective planes that are substantially parallel with each other. 25. A remote control toy helicopter according to claim 15 wherein the substantially parallel relationship exists when the blade and the vane are inclined in respective planes that are substantially parallel with each other. 26. A remote control toy helicopter according to claim 16 wherein the substantially parallel relationship exists when the blade and the vane are inclined in respective planes that are substantially parallel with each other. 27. A remote control toy helicopter according to claim 17 wherein the substantially parallel relationship exists when the blade and the vane are inclined in respective planes that are substantially parallel with each other. 28. A remote control toy helicopter according to claim 18 wherein the substantially parallel relationship exists when the blade and the vane are inclined in respective planes that are substantially parallel with each other. 29. A remote control toy helicopter according to claim 19 wherein the substantially parallel relationship exists when the blade and the vane are inclined in respective planes that are substantially parallel with each other.
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이 특허에 인용된 특허 (126)
Kastan Howard (Northridge CA), Advanced control system for a rotor and/or a compound or rotary wing vehicle.
Vuillet Alain E. (Bouc Belair FRX) Philippe Jean J. (Versailles FRX) Desopper Andr (Garches FRX), Blade with curved end for a rotary airfoil of an aircraft.
Sims Anson (Granada Hills CA) Jones Lawrence T. (Playa Del Rey CA) Howden Ashley G. (Los Angeles CA) Lee Robert S. (West Lake Village CA), Insect simulating mobile toy having flappable wings.
Rollet Philippe A. (Velaux FRX) Eglin Paul G. (Aix en Provence FRX), Single-rotor helicopter having a compound anti-torque system, and a method of countering the torque induced by said sing.
Bollinger Howard N. (Cincinnati OH) Allen Robert K. (Cincinnati OH) Langdon Nick H. (Cincinnati OH) Toth Stephen M. (Loveland OH) Williams W. Grey (Covington KY), Toy helicopter.
Eickmann Karl (2420 Isshiki Hayama-machi ; Kanagawa-ken JPX), Vehicle for traveling in the air and on the ground equipped with hydraulically driven propellers.
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