The present invention relates to vertical axis wing turbines and, in particular, to the blades and the fabrication thereof.
International Patent Application No. PCT/AU2005/001621 discloses a vertical axis wind turbine in which the blades are relatively thin. Depending upon the size of the wind turbine, the blades may have a thickness which varies between approximately 1 mm and approximately 200-300 mm. One of the problems of fabricating vertical axis wind turbine blades which are thin is that the blade is not very rigid. There is also a tendency for the blade to flutter or vibrate whilst in use. Since wind turbines can be subjected to very strong winds and thus substantial loads, it is necessary for the blades to be mounted in such a way that they can withstand the loads to which they are subjected.
Preferably the blades are moulded from resin reinforced with carbon fibres or are pressed from sheet aluminium. Furthermore, each surface of the thin blades has an aerodynamic function. Consequently, the blade must be mounted in such a way that the mounting does not itself interfere to any appreciable extent with the aerodynamic performance of the blades.
The genesis of the present invention is a desire to increase blade rigidity and/or reduce the incidence or severity of such blade flutter and to meeting these inherently conflicting requirements.
In accordance with a first aspect of the present invention there is disclosed in a vertical axis wind turbine having a plurality of main blades each of which is relatively thin, the improvement comprising a thickened portion extending along the trailing edge of each said blade.
In accordance with another aspect of the present invention a method of construction of the main blade of a vertical axis wind turbine is also disclosed.
In accordance with a further aspect of the present invention there is disclosed a vertical axis wind turbine having a central support column and at least one blade, the or each blade being fabricated in at least two sub-sections, wherein at least one strut extends between said central support column and a junction where said blade sub-sections abut, and said strut is thin in vertical extent.
In accordance with a still further aspect of the present invention there is provided a vertical axis wind turbine blade extending vertically a predetermined length and extending a width horizontally between a blade mounting end and a blade distal end, said blade mounting end configured for vertically mounting to a central core wherein said blade is circularly curved by a predetermined curvature along a predetermined horizontal width from said blade mounting end, said blade being circularly elliptically curved by a predetermined curvature along a predetermined horizontal width from an end of said circular curving, said blade being substantially flat from an end of said circular-eliptical curving to said blade distal end, wherein said blade in horizontal cross-section is substantially uniform along said blade length.
Preferred embodiments of the present invention will now be described with reference to the drawings in which:
As seen in
The turbine 1 has three main blades 7, 8, 9 which extend between an upper disc 11 and a lower disc 12. A central cylindrical core 13 extends between the two discs 11, 12, and is coaxial with the shaft 3, there is a vertical gap between each of the main blades 7, 8, 9 and the central core 13. The wind turbine 1 rotates in an anticlockwise direction as seen in
The blades 7, 8, 9 are preferably moulded from resin reinforced with carbon fibres or pressed from sheet aluminium.
As best seen in relation to
y=(R12−x2)1/2 R2/R1
where R1 is the radius of the discs 11, 12 and thus constitutes the maximum radial extent of each main blade and R2 is the minimum radial extent of each main blade.
As also seen in
In prior art wind turbine arrangements where the turbine blades are made from thin sheet material, the trailing edge of each blade is simply formed from cutting the material and thus the trailing edge has a generally rectangular configuration as illustrated in
Also extending along the trailing edge 18 is an auxiliary blade 25 which, as indicated by broken lines in
In a still further embodiment illustrated in
In addition, the auxiliary blade 25 is connected by means of another ear 41 to an extension device 42 which can take the form of a solenoid with a reciprocable magnetic armature, or a small hydraulic ram, or similar. The extension device 42 is reciprocal as indicated by arrow B in
Turning now to
The abovedescribed arrangements mean that the thickened portion 28 stiffens the main rail 7, 8, 9 and thereby counteracts any tendency to vibrate or flap, and does not interfere with the flow of air over the main blades 7, 8, 9.
Turning now to
Where adjacent blade sub-sections abut, one or more struts 50, 51, 52 extend from the central column 13 to the junction between the blade sub-sections. The struts 50, 51, 52 are formed from a thin blade of metal or composite material. In
As seen in
As schematically illustrated in
It will be appreciated that the struts 50, 51, 52 are formed from a strip of preferably stainless steel having a rectangular transverse cross-section and in which the vertical dimension of the strut is thin relative to the other dimensions of the strut. Accordingly, the struts 50, 51, 52 do not disturb the flow of air past the blades 7, 8, 9 and so the aerodynamic performance of the blades is not diminished to any significant extent by the presence of the struts. However, the struts do provide a strong mounting mechanism which ensures that the blades 7, 8, 9 are securely held and are able to withstand the loads applied to them.
Referring to
In this arrangement, the main blade 8 extends vertically a predetermined length (not shown). The blade 8 extends a width horizontally between a blade mounting end 870 and a blade distal end 871. Although not shown, the blade mounting end 870 is configured to be mounted along the central core 13.
The blade 8 is circularly curved 872 along a predetermined horizontal width from the blade mounting end 870. At the end of the circular curvature, the blade 8 is circular-eliptically curved 873 by a predetermined curvature along a horizontal blade width from the end of the circularly curved section 872.
The blade 8 is substantially flat 874 along a predetermined width of the blade 8 from the end of the circular-eliptically curved section 873 to the blade distal end 871. The horizontal cross-section of the blade 8 along the vertical extend of the blade is substantially uniform.
The blade 8 is twisted about the vertical axis by 90° or 120°. As shown in this
The foregoing describes only some embodiments of the present invention and modifications, obvious to those skilled in the art, can be made thereto without departing from the scope of the present invention. For example, the auxiliary blade 25 can be mounted either on the leading side, or on the trailing side, of the main blade.
Furthermore, the upper surface of the upper disc 17 can be provided with a generally shallow cone shape so as to ensure runoff of rainwater.
In addition, a vertical axis wind turbine can be formed from two or more wind turbines 1 which are conically mounted and vertically spaced apart so as to form a stack of turbines 1. With reference to
The term “comprising” (and its grammatical variations) as used herein is used in the inclusive sense of “including” or “having” and not in the exclusive sense of “consisting only of”.
Number | Date | Country | Kind |
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2006901827 | Apr 2006 | AU | national |
2006902971 | Jun 2006 | AU | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/AU07/00340 | 3/21/2007 | WO | 00 | 8/25/2009 |