Windmill

• US 4,291,235 A
• Filed: 02/26/1979
• Issued: 09/22/1981
• Est. Priority Date: 02/26/1979
• Status: Expired due to Term

• Current Assignee: Karl H. Bergey Jr, Michael L.S. Bergey
• Original Assignee: Karl H. Bergey Jr, Michael L.S. Bergey
• Inventors: Bergey, Karl H. Jr., Bergey, Michael L. S.
• Primary Examiner(s): Truhe, J. V.
• Assistant Examiner(s): Conklin, John B.
• Application Number:
  US06/015,290
• Time in Patent Office: 939 Days
• Field of Search: 290/44, 290/43, 290/54, 290/55, 290/52, 290/5, 310/49 R, 310/156 R, 310/67 R, 310/112, 416/240, 416/132
• US Class Current: 290/55
• CPC Class Codes: F03D 15/20 Gearless transmission, i.e. direct-drive
• CPC Class Codes: F03D 7/0224 Adjusting blade pitch
• CPC Class Codes: F03D 9/25 the apparatus being an electrical generator F03D9/22 takes precedence
• CPC Class Codes: F05B 2220/7066 via a direct connection, i.e. a gearless transmission
• CPC Class Codes: F05B 2260/74 by turning around an axis perpendicular the rotor centre line
• CPC Class Codes: F05B 2260/77 the adjusting mechanism driven or triggered by centrifugal forces
• CPC Class Codes: H02K 7/183 wherein the turbine is a wind turbine adaptation of a wind turbine to an electric generator F03D9/25
• CPC Class Codes: H02K 7/1838 Generators mounted in a nacelle or similar structure of a horizontal axis wind turbine
• CPC Class Codes: Y02E 10/72 Wind turbines with rotation axis in wind direction
• CPC Class Codes: Y10S 416/04 Fluid current motor and generator

Abstract

This invention relates generally to an improved windmill design that combines the blade and rotor support system with the electrical generating system in such a way as to simplify the windmill construction. Specifically, it eliminates the need for shafts, gears, and other coupling devices between the turbine blade system and the electrical generating system. In addition, the windmill design also includes a means for varying the pitch of the turbine blades automatically so as to provide near-optimum blade angles under varying wind conditions, and a tendency toward self-governing at high wind speeds. Furthermore, the blades are attached rigidly to the hub without the need for bearings or other mechanical couplings. Blade pitch changes are produced by twisting the blades elastically by forces produced by fixed weights. The effect of these features individually and in combination is to reduce the complexity of the wind turbine, the generating system, and their associated parts.

Claims

1. A variable pitch turbine blade system, comprising:

a blade, including a radially inner fixed end and a radially outer free end, said blade being continuously torsionally flexible between said free end and a radially inner point on said blade, said radially inner point being intermediate of said fixed end and said free end; and

an out-of-plane weight means, attached to said blade, for continuously varying a pitch of said blade in response to a variation in rotational speed of said turbine blade system, said pitch being continuously varied between a maximum variation adjacent said weight means and a smaller variation at said radially inner point for a given variation of said rotational speed of said turbine blade system;

wherein said weight means includes a mass with a center of mass thereof leading an elastic axis of said blade so that said turbine blade system operates free from flutter, and with said center of mass located out of a plane of rotation of said elastic axis of said blade so that a component of a centrifugal force acting on said mass acts to twist said blade about said elastic axis to vary the pitch of said blade.

2. Apparatus of claim 1, wherein said weight means is further characterized as being attached to a radially outer location on said blade and as being a means for continuously varying said pitch of said blade along substantially the entire radial distance between said free end and said radially inner point.

3. Apparatus of claim 2, wherein said center of mass is located forward of said elastic axis, so that said pitch is decreased as the rotational velocity of said turbine blade system is increased.

4. Apparatus of claim 3, wherein said pitch of said blade is oriented at a relatively high positive angle along a radially outer portion of said blade when said turbine blade system is not rotating.

5. Apparatus of claim 4, wherein said blade and said weight means are constructed so that at a predetermined rotational velocity the pitch of the radially outer end of said blade is decreased to a value sufficient to stall the outer end of said blade and cause said turbine blade system to be self-governing at approximately that predetermined rotational velocity.

6. Apparatus of claim 1, 2, 3, 4 or 5, wherein said blade is a cambered sheet blade.

7. A variable pitch turbine blade system, comprising:

a blade, including a radially inner fixed end and a radially outer free end, said blade being continuously torsionally flexible between said fixed end and said free end; and

an out-of-plane weight means, attached to said blade, for continuously varying a pitch of said blade in response to a variation in rotational speed of said turbine blade system, said pitch being continuously varied between a zero pitch variation at said fixed end and a maximum pitch variation adjacent said weight means for a given variation of said rotational speed of said turbine blade system;

wherein said weight means includes a mass with center of mass thereof leading an elastic axis of said blade so that said turbine blade system operates free from flutter, and with said center of mass located out of a plane of rotation of said elastic axis of said blade so that a component of a centrifugal force acting on said mass acts to twist said blade about said elastic axis to vary the pitch of said blade.

8. Apparatus of claim 7, wherein said weight means is further characterized as being attached to a radially outer location on said blade and as being a means for continuously varying said pitch of said blade along substantially its entire radial length.

9. Apparatus of claim 8, wherein said center of mass is located forward of said elastic axis, so that said pitch is decreased as the rotational velocity of said turbine blade system is increased.

10. Apparatus of claim 9, wherein said pitch of said blade is oriented at a relatively high positive angle along a radially outer portion of said blade when said turbine blade system is not rotating.

11. Apparatus of claim 10, wherein said blade and said weight means are constructed so that at a predetermined rotational velocity the pitch of the radially outer end of said blade is decreased to a value sufficient to stall the outer end of said blade and cause said turbine blade system to be self-governing at approximately that predetermined rotational velocity.

12. Apparatus of claim 7, 8, 9, 10, or 11, wherein said blade is a cambered sheet blade.

13. A windmill, comprising:

a shaft;

a turbine blade system;

first and second permanent magnet alternators, each of said alternators including a multiple pole stator fixedly mounted on said shaft and a multiple magnet permanent magnet structure rotatably mounted coaxial with said stator, said turbine blade system being connected to said magnet structures to rotate therewith, the poles of said stator of said second alternator being angularly offset from the poles of said first alternator and wherein the magnets of said magnet structures of said first and second alternators are aligned in axial rows so that only one of said first and second alternators can have the poles of its stator radially aligned with the magnets of its magnet structure at any given time.

14. Apparatus of claim 13, wherein the magnets of each of said axial rows are further characterized as being oriented so that magnet ends facing the stators all have the same magnetic sign.

15. Apparatus of claim 13, further comprising a third alternator, the poles of said third alternator being angularly offset from the poles of said second alternator so that only one of said first, second and third alternators can have the poles of its stator radially aligned with the magnets of its magnet structure at any given time.

16. Apparatus of claim 15, wherein the magnets of said magnet structures of said first, second and third alternators are aligned in axial rows.

17. Apparatus of claim 16, wherein the magnets of each of said axial rows are further characterized as being oriented so that magnet ends facing the stators all have the same magnetic sign.

18. Apparatus of claim 15, further comprising first, second and third stator spacers, slidingly received on said shaft and fixed thereto, said first, second and third stators being attached to said first, second and third stator spacers, respectively.

19. Apparatus of claim 13, wherein said turbine blade system comprises:

a central hub, attached to said magnet structures;

a blade having a radially inner end, fixedly attached to said hub, and a radially outer free end.

20. Apparatus of claim 19, wherein said blade is torsionally flexible.

21. Apparatus of claim 20, wherein said turbine system blade system further comprises an out-of-plane weight attached to a radially outer location on said blade, so that the pitch of said blade is continuously decreased, with increasing rotational velocity of said turbine blade system, until a portion of said blade is stalled causing the turbine blade system to be self-governing at approximately the rotational velocity at which said stall occurs.

22. Apparatus of claim 21, wherein a center of mass of said weight leads an elastic axis of said blade, and is located forward of said elastic axis.

23. Apparatus of claim 13, 14, 15, 16, 17, 18, 19, 20, 21 or 22, wherein:

said first permanent magnet alternator includes an equal number of poles and magnets; and

said second permanent magnet alternator includes an equal number of poles and magnets.

24. A windwill, comprising:

a turbine blade system;

first and second electrical generating means, each of said generating means including a fixedly mounted multiple pole stator and including a multiple pole rotor rotatably mounted coaxial with said stator, said turbine blade system being connected to said rotors to rotate therewith, said first and second electrical generating means being arranged so that at any given time only one of said first and second electrical generating means can have its stator poles and its rotor poles so relatively positioned as to present a maximum cogging force for said one generating means, so that at any given time a total cogging force presented by said first and second electrical generating means is less than a total of a maximum cogging force of said first generating means plus a maximum cogging force of said second generating means.

25. The windmill of claim 24, wherein:

the poles of said stator of said second generating means are angularly offset from the poles of said stator of said first generating means.

26. The windmill of claim 25, wherein:

the poles of said rotors of said first and second generating means are aligned in axial rows.

27. The windmill of claim 26, wherein:

the rotor poles of each of said axial rows all have the same magnetic sign.

28. The windmill of claim 24, wherein:

said first generating means includes an equal number of stator poles and rotor poles; and

said second generating means includes an equal number of stator poles and rotor poles.

29. A windmill, comprising:

a shaft;

a turbine blade system;

first and second permanent magnet alternators, each of said alternators including a multiple pole stator fixedly mounted on said shaft and a multiple magnet permanent magnet structure rotatably mounted coaxial with said stator, said turbine blade system being connected to said magnet structures to rotate therewith, the poles of said stator of said second alternator being angularly offset from the poles of said first alternator;

wherein said turbine blade system includes;

a central hub, attached to said magnet structures;

a torsionally flexible blade having a radially inner end, fixedly attached to said hub, and a radially outer free end; and

an out-of-plane weight attached to a radially outer location on said blade, so that the pitch of said blade is continuously decreased, with increasing rotational velocity of said turbine blade system, until a portion of said blade is stalled causing the turbine blade system to be self-governing at approximately the rotational velocity at which said stall occurs.

30. Apparatus of claim 29, wherein a center of mass of said weight leads an elastic axis of said blade, and is located forward of said elastic axis.

31. Apparatus of claim 29 or 30, wherein:

said first permanent magnet alternator includes an equal number of poles and magnets; and

said second permanent magnet alternator includes an equal number of poles and magnets.