초록

Power generating apparatus (10) including a cable (12) which rotatably mounts a plurality of power units (14). The power units (14) include wind power turbines (46) for producing power from the wind as the power units (14) fly in the sky whilst connected to the cable (12).

대표청구항 ▼

The invention claimed is: 1. Power generating apparatus, the apparatus comprising a power generating assembly including a plurality of power units each including a wind power turbine, the units being attached sequentially to a cable, with one end of the cable being mountable to the ground with the

The invention claimed is: 1. Power generating apparatus, the apparatus comprising a power generating assembly including a plurality of power units each including a wind power turbine, the units being attached sequentially to a cable, with one end of the cable being mountable to the ground with the cable extending upwardly therefrom such that the power units are located above the ground and can be driven by the wind. 2. Apparatus according to claim 1, characterised in that each assembly includes greater than 20 power units. 3. Apparatus according to claim 2, characterised in that each assembly includes greater than 50 power units. 4. Apparatus according to claim 3, characterised in that each assembly includes greater than 100 power units. 5. Apparatus according to claim 1, characterised in that the cable is greater than 1,000 m long. 6. Apparatus according to claim 5, characterised in that the cable is greater than 5,000 m long. 7. Apparatus according to claim 1, characterised in that each wind power turbine includes one or more turbine rotors. 8. Apparatus according to claim 1, characterised in that some or all of the power units are configured to generate aerodynamic lift. 9. Apparatus according to claim 8, characterised in that the assembly is configured such that the aerodynamic lift generated by the power units in use maintains the cable substantially taut. 10. Apparatus according to claim 8, characterised in that some or all of the power units include a wing to generate aerodynamic lift. 11. Apparatus according to claim 8, characterised in that some or all of the power units include rotors to generate aerodynamic lift. 12. Apparatus according to claim 8, characterised in that some or all of the power units include a rotor or rotors rotatable about a substantially vertical axis in use, which rotors may provide power extraction and lift. 13. Apparatus according to claim 7, characterised in that the rotor or rotors are retractable, or movable. 14. Apparatus according to claim 1, characterised in that each power unit is attached to the cable such that the power unit can be optimally aligned relative to the wind velocity vector. 15. Apparatus according to claim 14, characterised in that a mounting means is provided on each power unit which mounting means permits the units to freely rotate about the cable, whereby to prevent significant torsional loads on the cables. 16. Apparatus according to claim 15, characterised in that the mounting means is in the form of gimbals or a ball bushing, and the centre of rotation is at or close to the centre of gravity of the power units. 17. Apparatus according to claim 8, characterised in that the lift vector of each power unit is adjustable in magnitude and direction. 18. Apparatus according to claim 17, characterised in that adjustable aerodynamic control surfaces are provided to permit adjustment of the lift vector. 19. Apparatus according to claim 17, characterised in that some or all of the power units include rotors with variable cyclic and/or collective pitch to permit adjustment of the lift vector. 20. Apparatus according to claim 17, characterised in that the assembly is configured such that by adjusting the lift vectors of some or all of the power units, the altitude of the power units and also the tension in the cable can be controlled. 21. Apparatus according to claim 17, characterised in that the assembly is configured such that by adjusting the lift vectors of some or all of the power units it is possible to manoeuvre the assembly relative to the wind vector field. 22. Apparatus according to claim 17, characterised in that control means are provided to permit the lift vectors of each power unit to be controlled. 23. Apparatus according to claim 1, characterised in that the assembly includes means for providing power to drive one or more of the power units so as to provide lift. 24. Apparatus according to claim 23, characterised in that the assembly is arranged such that power can be provided through the cable to drive said one or more power units as a motor, with the turbine rotor acting as a propeller. 25. Apparatus according to claim 1, characterised in that said one or more power units include an internal combustion engine to selectively drive the unit. 26. Apparatus according to claim 25, characterised in that the engine drives the turbine rotor, or may generate electricity to cause the turbine to operate. 27. Apparatus according to claim 25, characterised in that the internal combustion engine drives an auxiliary propeller, which propeller may be featherable, retractable and/or foldable. 28. Apparatus according to claim 1, characterised in that the assembly is selectively detachable from the ground. 29. Apparatus according to claim 28, characterised in that the assembly is arranged such that when detached the assembly can be flown, propelled by at least some of the powered power units, to a required location. 30. Apparatus according to claim 28, characterised in that the apparatus includes a cable anchorage. 31. Apparatus according to claim 30, characterised in that the cable anchorage is arranged so as to permit the cable when attached thereto, to be movable relative to the anchorage in three dimensions, while maintaining electrical connection therewith. 32. Apparatus according to claim 30, characterised in that the cable is arranged to transmit power generated by the units to the cable anchorage. 33. Apparatus according to claim 32, characterised in that two or more insulated electrical conductors are provided in the cable for transmitting power generated by the units to the cable anchorage. 34. Apparatus according to claim 33, characterised in that a potential difference is provided between the electrical conductors. 35. Apparatus according to claim 15, characterised in that electrical connections are provided between the units and electrical conductors in the cable. 36. Apparatus according to claim 35, characterised in that the connections are in the form of slip rings. 37. Apparatus according to claim 35, characterised in that the connections are in the form of an electrical transformer. 38. Apparatus according to claim 37, characterised in that the transformer includes a first set of windings attached to the unit, and a second set attached to the cable. 39. Apparatus according to claim 1, characterised in that power is transported along the cable by the flow of one or more fluids in pipes located in the cable. 40. Apparatus according to claim 39, characterised in that the downwards flowing fluid is held at a higher pressure than the upwards flowing fluid. 41. Apparatus according to claim 39, characterised in that power is transmitted by means of the pressure differential, or by means of chemical changes in the fluid such that the downward flowing fluid has higher internal energy than the upwards flowing fluids. 42. Apparatus according to claim 1, characterised in that power is transmitted from the power units independently of the cable. 43. Apparatus according to claim 42, characterised in that power is transmitted by beams of microwave radiation. 44. Apparatus according to claim 1, characterised in that the assembly includes lightning strike handling equipment. 45. Apparatus according to claim 44, characterised in that the assembly includes any of protective earth conductors, Faraday cages, or electrodes. 46. Apparatus according to claim 1, characterised in that one or more transponders is provided on the assembly to warn aircraft of the existence and location of the assembly. 47. Apparatus according to claim 1, characterised in that one or more of the power units includes energy storage systems such that said unit or units can be driven using power from the energy storage systems. 48. Apparatus according to claim 47, characterised in that the energy storage systems uses batteries or includes a chemically transformable fluid, and such energy storage systems may be selectively rechargeable as required. 49. Apparatus according to claim 1, characterised in that the apparatus is arranged such that an assembly can take off from the ground and/or land on the ground, with the power units acting as aircraft. 50. Apparatus according to claim 49, characterised in that the apparatus is arranged such that an assembly can take off from the ground and/or land on the ground with at least some of the power units powered to take off in the nature of an aeroplane. 51. Apparatus according to claim 48, characterised in that the apparatus is arranged such that an assembly can take off from the ground and/or land on the ground with at least some of the power units powered to take off in the nature of an aeroplane. 52. Apparatus according to claim 50, characterised in that during take off the power units have power provided by microwave aerials or photocells. 53. Apparatus according to claim 1, characterised in that the apparatus is arranged such that an assembly can be towed by an aircraft during take off and/or landing on the ground. 54. Apparatus according to claim 1, characterised in that the power units include fixed or retractable undercarriage units. 55. Apparatus according to claim 1, characterised in that detachable carts are provided upon which the power units can ride during take-off, but which carts remain on the ground. 56. Apparatus according to claim 7, characterised in that detachable carts are provided upon which the power units can ride during take-off, but which carts remain on the ground. 57. Apparatus according to claim 1, characterised in that each power unit has a discrete control system. 58. Apparatus according to claim 57, characterised in that the control system is remotely operable, desirably by radiotelephony. 59. Apparatus according to claim 1, characterised in that the cable is provided in a number of detachable segments such that the length of the cable can be varied. 60. Apparatus according to claim 59, characterised in that a plurality of power units are provided on each segment. 61. Apparatus according to claim 59, characterised in that each segment is arranged to be selectively disengageable from a power source in the cable in adjacent segments. 62. Apparatus according to claim 1, characterised in that the spacing of the power units on the cable varies along the length thereof, and for instance the spacing reduced away from the ground. 63. Apparatus according to claim 1, characterised in that the thickness of the cable reduces away from the ground. 64. Apparatus according to claim 1, characterised in that one or more lift units are provided on the cable, for generating aerodynamic lift to the cable. 65. Apparatus according to claim 64 characterised in that the, or each, lift unit is substantially devoid of wind power turbines. 66. Apparatus according to claim 64 characterised in that the, or each, lift unit is capable of generating aerodynamic lift. 67. Apparatus according to claim 1, characterised in that one or more lighter than air members is attached to the cable to provide lift. 68. Apparatus according to claim 67, characterised in that the lighter than air members are in the form of balloons or airships. 69. Apparatus according to claim 64 characterised in that the, or each, lift unit comprises first and second hulls, each hull comprises an inflatable member comprising a gas of less density than air, and the, or each, lift unit includes a connection member extending between the hulls wherein the cable extends through the connecting member. 70. Apparatus according to claim 64, characterised in that the lift units are provided on the cable towards the lower end thereof in use. 71. Apparatus according to claim 1, characterised in that one or more driving units are provided which include means for driving the unit but do not include a wind power turbine. 72. Apparatus according to claim 71, characterised in that the unit driving means includes at least one motor driven propeller. 73. Apparatus according to claim 71 characterised in that the driving units include means for generating aerodynamic lift. 74. Apparatus according to claim 71, characterised in that each wind power turbine includes one or more electrical generators. 75. Apparatus according to claim 74, characterised in that the or each generator operates at a first lower voltage, which voltage is transformed to a second higher voltage for transmission along the cable. 76. Apparatus according to claim 37, characterised in that the or each generator operates at a first lower voltage, which voltage is transformed to a second higher voltage for transmission along the cable. 77. Apparatus according to claim 74, characterised in that each power unit includes a step up gear box to enable both the rotors and the electrical generators to run at their optimum speeds. 78. Apparatus according to claim 74, characterised in that the apparatus is arranged such that during operation the alternating current generators for each power unit can be synchronised, and the power generators could be synchronised with the local power grid for onwards transmission. 79. Apparatus according to claim 1, characterised in that the apparatus is arranged such that oscillations or vibrations within a power generating assembly are effectively damped. 80. Apparatus according to claim 1, characterised in that each power unit, lift unit and/or driving unit is preferably provided with a set of receivers for a local or a global positioning system, and desirably for a differential global positioning system. 81. Apparatus according to claim 80, characterised in that a plurality of receivers for a global positioning system are provided on each power unit, lift unit and/or driving unit at different positions on the unit to enable the orientation of each unit to be determined. 82. Apparatus according to claim 59, characterised in that each power unit, lift unit and/or driving unit is preferably provided with a set of receivers for a local or a global positioning system, and desirably for a differential global positioning system. 83. Apparatus according to claim 1, characterised in that each power unit includes two wind power turbines, with desirably one on each side thereof. 84. Apparatus according to claim 1, characterised in that each power unit includes a wing. 85. Apparatus according to claim 84, characterised in that the wing includes one or more pivotal control surfaces. 86. Apparatus according to claim 84, characterised in that the wind power turbines are mounted on the wing. 87. Apparatus according to claim 84, characterised in that each power unit is configured such that in a normal orientation the wing extends substantially horizontally, with the rotors of the wind power turbines facing the relative wind velocity vector. 88. Apparatus according to claim 84, characterised in that the rear of each power unit includes a pair of spaced booms extending rearwardly from the wing to the empennage, to provide clearance for the cable. 89. Apparatus according to claim 83, characterised in that each power unit is provided with variable pitch control. 90. Apparatus according to claim 1, characterised in that the apparatus includes a plurality of assemblies, each with a cable and a plurality of power units. 91. Apparatus according to claim 90, characterised in that the apparatus is arranged such that each assembly can be controlled to prevent contact between the cables and power units of adjacent assemblies. 92. A method of operating a power generating apparatus according to claim 1, the method including maintaining an assembly trailing downwind in high and moderately high wind speed conditions. 93. A method according to claim 92, characterised in that the method also includes, when the wind speed reduces, controlling the power units, lift units and/or driving units such that the assembly moves substantially in a circle above the ground mounting so that if the cable remains taut the assembly defines an imaginary cone. 94. A method according to claim 92, characterised in that the method includes when the wind speed reduces, controlling the power units, lift units and/or driving units such that the assembly moves substantially in a figure of eight above the ground, while the fixed length of the cable remains substantially taut. 95. A method according to claim 92, characterised in that the method includes controlling the power units, lift units and/or driving units such that the tension in the cable is regulated. 96. A method according to claim 92 when dependent upon claim 59, characterised in that the segments of cable and power units thereon take off one at a time, and are sequentially mounted to the ground and to each other in a required position once airborne. 97. A method according to claim 92, characterised in that the method includes substantially equalising the number of left hand and right hand turns of the power units around the cable, to minimise the torsional wind-up of the cable. 98. Apparatus according to claim 51, characterised in that during take off the power units are powered by their energy storage systems. 99. Apparatus according to claim 48, characterised in that the turbine rotor or rotors are folded or feathered in a horizontal position for landing. 100. Apparatus according to claim 76, characterised in that the first voltage is transformed to the second voltage by the electrical transformers. 101. Apparatus according to claim 82, characterised in that receivers for a positioning system are also provided on connectors at the ends of the cable segments.