A wing with slipstream turbine comprising: a wing or airfoil and at least one turbine, wherein wing or airfoil has at least one partial cylindrical void in a surface and at least one turbine is partially encapsulated within partial cylindrical void. Optionally, wing with slipstream turbine may furth
A wing with slipstream turbine comprising: a wing or airfoil and at least one turbine, wherein wing or airfoil has at least one partial cylindrical void in a surface and at least one turbine is partially encapsulated within partial cylindrical void. Optionally, wing with slipstream turbine may further comprise at least one slipstream outrigger to help focus the flow of the slipstream more directly on a turbine. Optionally, wing with slipstream turbine may further comprise at least one lateral outrigger to create a low-pressure area which functions to add additional energy transfer to turbine. Optionally, wing with slipstream turbine may further comprise two leading outriggers to help focus the flow of the slipstream more directly on a turbine. Optionally, wing or airfoil may further comprise a leading subcomponent, a left subcomponent, and a right subcomponent to create a super low-pressure area which functions add additional energy transfer to turbine.
대표청구항▼
1. A windmill comprising: an airfoil [10];a left partial cylindrical void [22];a right partial cylindrical void [24];a left turbine [26];a right turbine [28];a center evacuation channel [76]; anda super low pressure chamber [78], wherein said airfoil [10] comprises a leading subcomponent [70], a lef
1. A windmill comprising: an airfoil [10];a left partial cylindrical void [22];a right partial cylindrical void [24];a left turbine [26];a right turbine [28];a center evacuation channel [76]; anda super low pressure chamber [78], wherein said airfoil [10] comprises a leading subcomponent [70], a left subcomponent [72], and a right subcomponent [74], whereinsaid leading subcomponent [70], said left subcomponent [72], and said right subcomponent [74] are each an elongated planar member with rounded edges, elongated ellipsoid shaped planar member, elongated airfoil-shaped member, or wing-shaped member,said leading subcomponent [70], said left subcomponent [72], and said right subcomponent [74] are shaped and positioned to form an overall symmetric airfoil shape with a leading edge [11], a trailing edge [14], a left surface [12], a right surface [13], an upper end [15], and a lower end [16], with said leading edge [11] located on said leading subcomponent [70], said left surface [12] located on said left subcomponent [72], and said right surface [13] located on said right subcomponent [74],said left partial cylindrical void [22] is a cylindrical-shaped void in said left surface [12] where a complete cylindrical shaped void has not been carved, removed, or voided from said left subcomponent [70],said right partial cylindrical void [24] is a cylindrical-shaped void in said right surface [13] where a complete cylindrical shaped void has not been carved, removed, or voided from said right subcomponent [72],said left turbine [26] comprises an axle, a plurality of spoke members, a drum, and a plurality of blades [38] or a fibrous surface covering [39] that is carpet or a plurality of individual fibers, rods, bumps, indentations, paddles, fins, or appendages protruding radially outward out from said drum,said left turbine [26] is cylindrical shaped and sized slightly smaller than the cylindrical shape of said left partial cylindrical void [22] so that said left turbine [26] may be nested within said left partial cylindrical void [22] to form a slip fit therein,said right turbine [28] comprises an axle, a plurality of spoke members, a drum, and a plurality of blades [38] or a fibrous face covering [39] that is carpet or a plurality of individual fibers, rods, bumps, indentations, paddles, fins, or appendages protruding radially outward out from said drum,said right turbine [28] is cylindrical shaped and sized slightly smaller than the cylindrical shape of said right partial cylindrical void [24] so that said right turbine [28] may be nested within said right partial cylindrical void [24] to form a slip fit therein,said center evacuation channel [76] is defined by said left subcomponent [72], said trailing edge [14], said right subcomponent [74], and said super low pressure chamber [78],said center evacuation channel [76] is an open slot or channel running between said left subcomponent [72] and said right subcomponent [74] from respective leading edges of said left subcomponent [72] and said right subcomponent [74] to respective trailing edges of said left subcomponent [72] and said right subcomponent [74], andsaid super low pressure chamber [78] is defined by said subcomponent [70], said left turbine [26], said center evacuation channel [76], and said right turbine [28].
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이 특허에 인용된 특허 (4)
Bailey, Laura J.; Bailey, John T., Shrouded vertical axis dual-turbine generator.
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