For fastening rotor blades to the hubs of wind turbines, it is prior art to arrange transverse pins in the region of the blade root in recesses extending substantially transversely to the longitudinal axis of the rotor blade, and to connect these to the rotor hub using a tension rod. According to DE 31 03 710 C2, access of the tension rod to the transverse pin is provided by a passage in the shell wall of the rotor blade root.
According to DE 197 33 372 C1, it is a disadvantage of this design that the rotor blade is significantly weakened in the region of the blade root by the passage bore for receiving the transverse pin. The solution proposed there is to design the passage bore in the form of two pocket holes and to arrange one tension rod, respectively, in two separate passages to the transverse pins located in the pocket holes.
Since these dual passages also entail weakening of the blade root material, WO 2004/106732 A1 proposes to fall back on transverse pins that go through but to place the tension rods outside the blade root.
The disadvantage of this solution is that the bending moment distribution requires a relatively large transverse pin diameter due to the greater distance of the connections of the tension rods to the respective transverse pins. This solution also applies the highest surface pressure onto the laminate edge of the blade root shell wall.
It is the object of this invention to eliminate these disadvantages.
This object is achieved with the features of claim 1, advantageous embodiments are the subject matter of the dependent claims.
For fastening rotor blades to the rotor hub of wind turbines using transverse pins and tension rods in the region of the blade root, wherein the transverse pins pass through the blade root shell wall and can be connected to a flange in the hub using the tension rods, it is proposed, according to the invention, that each transverse pin can be connected to the flange of the rotor hub by two tension rods, wherein each tension rod is provided in a separate tension rod bore in the blade root shell wall.
It was surprisingly found that, unlike the prior art solutions cited, the forces applied to the blade root shell and therefore the stress characteristics it is subjected to can be optimized by connecting the rotor blade using two tension rods, each of which is provided in a separate through bore and can be connected to the transverse pins that penetrate the blade root shell wall.
In this way, high surface pressure onto the structurally critical laminate edges of the blade root shell wall can be prevented and shifted towards the inside of the blade root shell wall.
Furthermore, the diameters of both the transverse pins and the tension rods can be reduced, which results in a wider distribution of the reduction in blade root cross section that has been considered problematic, and allows its compensation.
Three variants are provided depending on the application:
The tension rod bores are equidistant from the outer or inner surface line, respectively, of the blade root shell wall, or
the distance of the inner tension rod bore to the inner surface line of the blade root shell wall is smaller than the distance of the outer tension rod bore to the outer surface line of the blade root shell wall, or
the distance of the inner tension rod bore to the inner surface line of the blade root shell wall is greater than the distance of the outer tension rod bore to the outer surface line of the blade root shell wall.
A more complete appreciation of the invention will be readily obtained by reference to the following detailed description when considered in connection with the accompanying drawings, wherein:
The rotor blade is fastened using transverse pins 4 and tension rods 5, 6 in the region of the blade root, wherein the transverse pins 4 are arranged to pass through the blade root shell wall 3.
The transverse pin 4 can be connected to the flange 2 using the tension rods 5, 6 in the form of expansion screws, wherein each transverse pin 4 is connected to the flange 2 of the rotor hub 1 by two tension rods 5, 6 and each tension rod 5, 6 is arranged in a separate tension rod bore 7, 8 in the blade root shell wall 3.
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Number | Date | Country | Kind |
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20 2011 100 897 U | May 2011 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/DE2012/000465 | 5/2/2012 | WO | 00 | 11/15/2013 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2012/155881 | 11/22/2012 | WO | A |
Number | Name | Date | Kind |
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4412784 | Wackerle et al. | Nov 1983 | A |
6371730 | Wobben | Apr 2002 | B1 |
8408875 | Quell et al. | Apr 2013 | B2 |
20070122283 | Wobben | May 2007 | A1 |
20070231146 | Birkemeyer et al. | Oct 2007 | A1 |
20090263250 | Quell | Oct 2009 | A1 |
Number | Date | Country |
---|---|---|
3103710 | Mar 1983 | DE |
19733372 | Jan 1999 | DE |
102006022272 | Nov 2007 | DE |
1840372 | Oct 2007 | EP |
2004106732 | Dec 2004 | WO |
Entry |
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International Preliminary Report on Patentability and Written Opinion of the International Searching Authority dated Nov. 19, 2013. |
Number | Date | Country | |
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20140079554 A1 | Mar 2014 | US |