초록 ▼

System for producing electricity from wind energy includes a shaft, at least two turbines rotatably mounted to the shaft and arranged to rotate independent of one another and in opposite directions when subjected to the same wind, and one or more generators that convert rotation of the turbines into

System for producing electricity from wind energy includes a shaft, at least two turbines rotatably mounted to the shaft and arranged to rotate independent of one another and in opposite directions when subjected to the same wind, and one or more generators that convert rotation of the turbines into electricity. The magnitude of electricity generation by the generator(s) is related to the magnitude of torque induced by the generator(s) on the shaft, and the electricity generation by the generator(s) may be controlled such that torques induced on the shaft by the generator(s) is controlled such that a sum of torques induced on the shaft is substantially zero. Generated electricity is conducted to users, to electricity storage, or to processing components. In an airborne embodiment, a lifting structure generates a lifting force to lift the turbines to a desired altitude, and an anchoring system anchors the turbines relative to the ground.

대표청구항 ▼

The invention claimed is: 1. A system for producing electricity from wind energy, comprising: a turbine section comprising: a shaft; at least first and second turbines rotatably mounted to said shaft and arranged to rotate independently of one another and in opposite directions about said shaft whe

The invention claimed is: 1. A system for producing electricity from wind energy, comprising: a turbine section comprising: a shaft; at least first and second turbines rotatably mounted to said shaft and arranged to rotate independently of one another and in opposite directions about said shaft when subjected to a same wind; and at least one generator coupled to said at least first and second turbines and arranged to convert rotation of said first and second turbines into electricity, said at least one generator being mounted so as to be fixed relative to said shaft, the magnitude of electricity generation by said at least one generator being related to a torque induced on said shaft by said at least one generator responsive to rotation of said turbines relative to said shaft, said turbines having aerodynamic characteristics which provide in combination with the effect of the electricity generation by said at least one generator a situation where a sum of torques acting on said shaft is substantially zero; wherein electricity generated by said at least one generator is conducted to an energy utilization device for usage or to electricity storage. 2. The system of claim 1, wherein said at least one generator comprises first and second generators respectively coupled to said first and second turbines. 3. The system of claim 1, wherein said at least one generator includes a rotatable shaft whose rotation causes generation of electricity, and further comprising a transmission system interposed between said turbines and said at least one generator for transmitting rotation of said turbines into rotation of said shaft of said at least one generator and thus generation of electricity by said at least one generator. 4. The system of claim 1, further comprising: a lifting system coupled to said turbine section for generating a lifting force to cause said turbine section to be airborne at a desired altitude; and an anchoring section arranged to anchor said turbine section relative to the ground, whereby said system is an airborne system. 5. The system of claim 4, further comprising an angular stability controller coupled to said at least one generator for controlling the electricity generation by said at least one generator and thus the magnitude of the torque that each of said at least one generator induces on said shaft, said angular stability controller being adapted to control said at least one generator in order to achieve substantially zero resultant torque induced on said shaft by said first and second turbines through said generators and thereby enable continuous angular stability of the system. 6. The system of claim 5, further comprising at least one fin fixed relative to said shaft, and a controllable flap attached to each of said at least one fin, said controllable flap having a variable angular position relative to said fin to which it is attached, and said angular stability controller being arranged to control said variable angular position of said flap of each of said at least one fin to aid in maintaining angular stability of the system. 7. The system of claim 5, wherein said first and second turbines comprise blades which have a controllable variable angle of attack, said angular stability controller being arranged to control the angle of attack of said blades of said first and second turbines to aid in maintaining the angular stability of the system. 8. The system of claim 4, wherein said anchoring section comprises a tether connected to said lifting structure or to said shaft, and a winch for adjusting a length of said tether relative to the ground. 9. The system of claim 4, wherein said lifting system comprises a first inflatable body arranged on one side of said turbine section and a second inflatable body arranged on an opposite side of said turbine section, said first and second inflatable bodies being receivable of a lighter-than-air gas. 10. The system of claim 4, wherein said lifting system comprises a single inflatable body coupled to said turbine section and receivable of a lighter-than-air gas, and said anchoring section comprises a tether connected to said turbine section. 11. The system of claim 4, wherein said lifting system comprises at least one independent lift-generating body spaced apart from said turbine section, and said at least one lift-generating body being connected to said turbine section to transfer a lifting force generated by said at least one lift-generating body to said turbine section. 12. The system of claim 11, further comprising: a connecting device connecting said at least one lift-generating body to said shaft; an angular stability controller coupled to said at least one generator for controlling the electricity generation by said at least one generator and thus the magnitude of the torque that each of said at least one generator induces on said shaft, said angular stability controller being adapted to control said at least one generator in order to achieve substantially zero resultant torque induced on said shaft by said first and second turbines through said at least one generator and thereby enable continuous angular stability of the system; and at least one fin coupled to said shaft and a controllable flap attached to each of said at least one fin, said controllable flap having a variable angular position relative to said fin to which it is attached, and said angular stability controller being arranged to control said flap of each of said at least one fin to aid in maintaining angular stability of the system. 13. The system of claim 11, wherein said at least one lift-generating body is non-inflatable and has aerodynamic characteristics which enable it to assume a position in which it generates and transfers sufficient lifting force to said turbine section when exposed to wind to enable said turbine section to remain airborne. 14. The system of claim 11, wherein said at least one lift-generating body comprises an unmanned helicopter driven by power drawn from a power source or from electricity generated by said turbine section. 15. The system of claim 1, wherein said first and second turbines each comprise rotatable blades, and wherein the blades of a turbine upwind of another turbine have a smaller diameter than the blades of the turbine which is downwind of the upwind turbine. 16. The system of claim 1, wherein said at least one generator consists of a single generator, further comprising a transmission structure for coupling both of said first and second turbines to said single generator. 17. The system of claim 16, wherein said transmission structure comprises a first gear fixed to each of said turbines and rotating with said turbines, and a pair of second gears each in meshing engagement with a respective one of said first gears and connected to a common shaft of said generator. 18. The system of claim 1, further comprising a structure that fixes said turbine section to the ground such that the system is a stationary, non-airborne wind turbine system. 19. The system of claim 18, wherein said structure is a tower, said shaft being attached to said tower to prevent movement of said shaft, said at least one generator being mounted on said tower. 20. The system of claim 18, wherein said tower is connected to said shaft between said first and second turbines, further comprising: a bearing assembly for rotatably supporting each of said first and second turbines on said shaft and which is arranged between said first and second turbines; and a gear attached to each of said bearing assemblies and rotatable with a respective one of said first and second turbines, said at least one generator being arranged one said tower structure and being mechanically coupled to both of said gears. 21. The system of claim 18, wherein said first turbine is upwind of said second turbine and said first and second turbines are spaced apart from one another such that said first turbine imposes an angular velocity component on the wind passing through its rotation area in an opposite direction of its rotation with the wind having the imposed angular velocity component passing through said second turbine to thereby increase efficiency of said second turbine.