초록 ▼

A PAVA (parallel and vertical axis) turbine includes a plurality of wing assemblies having vertical pivot shafts extending between two vertically spaced end assemblies that are joined to a central driveshaft assembly. The wing assemblies are rotatable about their respective pivot axes from a drive p

A PAVA (parallel and vertical axis) turbine includes a plurality of wing assemblies having vertical pivot shafts extending between two vertically spaced end assemblies that are joined to a central driveshaft assembly. The wing assemblies are rotatable about their respective pivot axes from a drive position in which they extend radially outwardly from the central axis and transverse to incident fluid flow to maximally capture fluid flow and rotate the turbine, to a glide position in which the wings extend tangentially to the direction of rotation and parallel to incident fluid flow to minimize drag. The wings may have articulating flaps rotating outwardly from the wing assembly in the drive quadrant to capture more of the passing fluid flow.

대표청구항 ▼

1. A turbine assembly for converting fluid flow into rotational movement for useful work, including: a central drive shaft assembly rotatable about a central axis:a pair of end assemblies secured to said central driye shaft assembly and spaced apart along said central axis:a plurality of primary win

1. A turbine assembly for converting fluid flow into rotational movement for useful work, including: a central drive shaft assembly rotatable about a central axis:a pair of end assemblies secured to said central driye shaft assembly and spaced apart along said central axis:a plurality of primary wing assemblies secured between said end assemblies and rotatable about primary pivot axes that are parallel to said central axis:said primary wing assemblies impinging on the fluid flow and turnin said central drive shaft assembly in a rotational drive direction;said primary wing assemblies being reciprocally rotatable about their respective pivot from arp imary drive position in which said primary wing assemblies extend generally radially with respect to said central axis and transverse to incident fluid flow to maximally impinge on said fluid flow, to a primary glide position in which said primary wing assemblies extend generally tangentially to said rotational drive direction to minimize drag;pivot means for securing said primary wing assemblies between said end assemblies, said pivot means permitting limited angular motion of said primary wing assemblies between said primary drive and primary glide position; and,a central airfoil secured about said central drive shaft assembly for deflecting fluid flow towards said drive position of said primary wing assemblies. 2. The turbine assembly of claim 1, wherein said pivot means includes a pivot shaft extending between said end assemblies and secured to a proximal edge portion of each of said primary wing assemblies. 3. The turbine assembly of claim 2, further including at least one counterweight secured to said primary wing assemblies and extending transverse to the pivot shaft in diametrical opposition to a respective primary wing assembly. 4. The turbine assembly of claim 1, further including a plurality of glide stops secured to said central drive shaft assembly and disposed to cushion and detain said primary wing assemblies in said glide position. 5. The turbine assembly of claim 1, further including a plurality of drive stops secured to said end assemblies and disposed to cushion and detain said primary wing assemblies in said primary drive position. 6. The turbine assembly of claim 1, wherein said central airfoil has a closed curved shape concentric about said central axis, and said primary wing assemblies each include a curved surface adapted to impinge on said closed curved shape in flush, complementary fashion when said primary wing assemblies are in said primary glide position. 7. The turbine assembly of claim 6, further including mechanical means for connecting at least a pair of said primary wing assemblies for rotational motion in concert, whereby one of said pair of primary wing assemblies rotates into said drive position when the other primary wing assembly rotates into said glide position. 8. The turbine assembly of claim 1, further including a plurality of fairing elements disposed to circumscribe at least a portion of said primary wing assemblies in said drive position and deflect incident fluid flow toward said primary wing assemblies. 9. The turbine assembly of claim 1, wherein said primary wing assemblies each include a panel having a teardrop cross-sectional configuration defining a broad leading edge and an opposed thin trailing edge. 10. The turbine assembly of claim 9, wherein said pivot means extend from said end assemblies to said broad leading edge of said panel. 11. The turbine assembly of claim 10, wherein said panel is curved about a focal axis that is parallel to said central axis. 12. A turbine assembly for converting fluid flow into rotational movement for useful work, including: a central drive shaft assembly rotatable about a central axis:a pair of end assemblies secured to said central drive shaft assembly and spaced apart along said central axis;a plurality of primary wing assemblies secured between said end assemblies and rotatable about primary pivot axes that are parallel to said central axis:said primary wing assemblies impinging on the fluid flow and turning said central drive shaft assembly in a rotational drive direction;said primary wing assemblies being reciprocally rotatable about their respective pivot axes from a primary drive position in which said primary wing assemblies extend generally radially with respect to said central axis and transverse to incident fluid flow to maximally impinge on said fluid flow, to a primary glide position in which said primary wing assemblies extend generally tangentially to said rotational drive direction to minimize drag:pivot means for securing said primary wing assemblies between said end assemblies, said pivot means permitting limited angular motion of said primary wing assemblies between said primary drive and primary glide positions: and,a plurality of secondary wing assemblies secured between said end assemblies and rotatable about secondary pivot axes That are parallel to said central axis;said secondary wing assemblies being reciprocally rotatable about their respective secondary pivot axes from a secondary drive position in which said secondary wing assemblies extend generally radially with respect to said central axis and transverse to incident fluid flow to maximally impinge on said fluid flow, to a secondary glide position in which said secondary wing assemblies extend generally tangentially to said rotational drive direction to minimize drag;each of said secondary pivot axes being disposed directly adjacent a respective one of said primary wing assemblies, whereby each primary wing assembly and a respective secondary wing assembly are disposed generally contiguously when in said primary and secondary drive positions. 13. The turbine assembly of claim 12, further including a plurality of secondary glide stops secured between said end assemblies and disposed to cushion and detain said secondary wing assemblies in said secondary glide position. 14. The turbine assembly of claim 12, further including a plurality of secondary drive stops secured to said end assemblies and disposed to cushion and detain said secondary wing assemblies in said secondary drive position.