초록 ▼

A turbine blade assembly has a plurality of blades mounted on a central rotor. Each of the blades has a proximal section and a variable pitch section. A number of stays extend in groups from the central rotor to converge and terminate on an associated one of the blades. The stays each have a proxima

A turbine blade assembly has a plurality of blades mounted on a central rotor. Each of the blades has a proximal section and a variable pitch section. A number of stays extend in groups from the central rotor to converge and terminate on an associated one of the blades. The stays each have a proximal end spaced from the blades.

대표청구항 ▼

The invention claimed is: 1. A turbine blade assembly comprising: a central rotor having a central axis; a plurality of blades mounted on said rotor to rotate through a plane of rotation, each of said blades lying along a blade axis and having a proximal section and a variable pitch section, said v

The invention claimed is: 1. A turbine blade assembly comprising: a central rotor having a central axis; a plurality of blades mounted on said rotor to rotate through a plane of rotation, each of said blades lying along a blade axis and having a proximal section and a variable pitch section, said variable pitch section being adjustable to a pitch that may differ from that of said proximal section; and a plurality of stays each extending from said central rotor to approach and terminate on an associated one of said blades, each of said stays having a proximal end spaced from said blades and a distal end attached to an associated one of said blades, the proximal section of each of said blades connecting to the distal ends of a different corresponding trio of said stays, for each of the blades the proximal ends of said different corresponding trio circumscribing the blade axis, each of the stays of the trio distally converging with respect to the other stays of the trio in order to reduce blade deflection front to back and along the plane of rotation. 2. A turbine blade assembly according to claim 1 wherein said trio of said stays comprises a pair whose proximal ends are at substantially diametrically opposed positions relative to said central axis. 3. A turbine blade assembly according to claim 1 wherein said trio has the proximal end of a forward one of the trio located in front of the blades and the other two of the trio have their proximal ends located at substantially diametrically opposed positions relative to said central axis. 4. A turbine blade assembly according to claim 3 wherein said central rotor comprises: a coaxial pylon having a distal end connected to the proximal ends of the forward one of the trio in the group of stays for each of the blades. 5. A turbine blade assembly according to claim 1 wherein the proximal section of each of said blades comprises: a plurality of struts each having a receptacle for engaging an affiliated one of said stays. 6. A turbine blade assembly according to claim 5 wherein the proximal section of each of said blades comprises: a plurality of rungs arranged polygonally with vertices adjacent to the receptacles of the struts. 7. A turbine blade assembly according to claim 6 wherein the proximal section of each of said blades comprises: a plurality of converging legs extending distally from the rungs. 8. A turbine blade assembly according to claim 1 wherein said rotor comprises: a wheel having a plurality of terminals for holding the proximal ends of at least some of the stays. 9. A turbine blade assembly according to claim 8 wherein the stays that are held on said wheel extend substantially tangentially from said wheel. 10. A turbine blade assembly according to claim 8 wherein said wheel is arranged to position said terminals behind said blades. 11. A turbine blade assembly according to claim 10 wherein said wheel has a rim with a plurality of braces that extend forwardly to reinforce said blades. 12. A turbine blade assembly according to claim 10 wherein said wheel has a hub, said blades being mounted on said hub. 13. A turbine blade assembly according to claim 1 wherein each of said blades comprises: a motor for rotating the variable pitch section to adjust pitch to a highest value, a lowest value, and to values in between in order to accommodate prevailing wind conditions. 14. A turbine blade assembly according to claim 13 wherein said motor has a spur gear and is located adjacent to a location between the proximal section and the variable pitch section. 15. A turbine blade assembly according to claim 1 comprising: an electrical generator coupled to said rotor; and a tower supporting said generator. 16. A turbine blade assembly comprising: a central rotor having a central axis; a plurality of blades mounted on said rotor to rotate through a plane of rotation, each of said blades lying along a blade axis; and a plurality of stays each having a proximal end spaced from said blades and a distal end attached to an associated one of said blades, each of said blades connecting to the distal ends of a different corresponding trio of said stays, for each of the blades the proximal ends of said different corresponding trio circumscribing the blade axis, each of the stays of the trio distally converging with respect to the other stays of the trio in order to reduce blade deflection front to back and along the plane of rotation. 17. A turbine blade assembly according to claim 16 wherein said different corresponding separate pair of said stays comprises a pair whose proximal ends are at diametrically opposed positions relative to said central axis. 18. A turbine blade assembly according to claim 17 wherein one of the trio is located in front of the blades and the other two of the trio have their proximal ends located at diametrically opposed positions relative to said central axis. 19. A turbine blade assembly according to claim 18 wherein said central rotor comprises: a coaxial pylon having a distal end connected to the proximal ends of a forward one of the trio for each of the blades. 20. A turbine blade assembly according to claim 16 wherein each of said blades comprises: a plurality of struts each having a receptacle for engaging an affiliated one of said stays. 21. A turbine blade assembly according to claim 20 wherein each of said blades comprises: a plurality of rungs arranged polygonally with vertices adjacent to the receptacles of the struts. 22. A turbine blade assembly according to claim 16 wherein said rotor comprises: a wheel having a plurality of terminals for holding the proximal ends of at least some of the stays. 23. A turbine blade assembly according to claim 22 wherein said stays that are held on said wheel extend substantially tangentially from said wheel. 24. A turbine blade assembly according to claim 22 wherein said wheel is arranged to position said terminals behind said blades. 25. A turbine blade assembly according to claim 24 wherein said wheel has a rim with a plurality of braces that extend forwardly to reinforce said blades. 26. A turbine blade assembly according to claim 24 wherein said wheel has a hub, said blades being mounted on said hub.