Method for balancing segmented wind turbine rotor blades
A method for balancing segmented rotor blades for a wind turbine may include determining a weight for each of a plurality of blade segments, wherein each blade segment extends between a first end and a second and is configured to form a common spanwise section of a segmented rotor blade between the first and second ends. The method may also include determining an initial static moment for each blade segment based on the weight of the blade segment, wherein the initial static moment of at least one of the blade segments differing from the initial static moments of the remainder of the blade segments. Additionally, the method may include adding mass to each of the blade segments to increase the initial static moment for each blade segment to a predetermined static moment, wherein the predetermined static moment is greater than each of the initial static moments of the blade segments.
1. A method for balancing segmented rotor blades for a wind turbine, the method comprising:
determining a weight for each of a plurality of blade segments, each blade segment of the plurality of blade segments extending between a first end and a second end and being configured to form a common spanwise section of a respective segmented rotor blade between the first and second ends;
determining an initial static moment for each blade segment of the plurality of blade segments based on the weight of the blade segment, the initial static moment of at least one blade segment of the plurality of blade segments differing from the initial static moments of the remainder of the plurality of blade segments; and
adding mass to each of the plurality of blade segments to increase the initial static moment for each blade segment of the plurality of blade segments to a predetermined static moment, the predetermined static moment being greater than each of the individual initial static moments of all of the plurality of blade segments.
2. The method of claim 1 , wherein each blade segment of the plurality of blade segments corresponds to a tip segment, the first end corresponding to a joint end of the tip segment and the second end corresponding to a tip end of the tip segment, the joint end being configured to be coupled to a corresponding root segment of the respective segmented rotor blade.
3. The method of claim 1 , wherein each blade segment of the plurality of blade segments corresponds to a root segment, the first end corresponding to a root end of the root segment and the second corresponding to a joint end of the root segment, the joint end being configured to be coupled to a corresponding tip segment of the respective segmented rotor blade.
4. The method of claim 1 , further comprising determining a center of gravity for each blade segment of the plurality of blade segments, wherein determining the initial static moment for each blade segment of the plurality of blade segments comprises determining the initial static moment for each blade segment of the plurality of blade segments based on both the weight of the blade segment and a location of the center of gravity of the blade segment.
5. The method of claim 1 , wherein adding mass to each of the plurality of blade segments comprises adding mass within a balance box installed within an interior of each of the plurality of blade segments.
6. The method of claim 1 , wherein the first end of each of the plurality of blade segments corresponds to a joint end of each blade segment and each blade segment of the plurality of blade segments defines a spanwise length between the first and second ends; the balance box being located within the interior of each blade segment a distance from the joint end equal to less than 25% of the spanwise length.
7. The method of claim 1 , wherein the predetermined static moment corresponds to a static moment that is equal to or greater than a maximum static moment for the plurality of blade segments based on allowable manufacturing variations.
8. The method of claim 1 , wherein the initial static moment of each blade segment of the plurality of blade segments differs from the initial static moments of the remainder of the plurality of blade segments.
9. A method for balancing segmented rotor blades for a wind turbine, the method comprising:
providing a plurality of tip segments and a plurality of root segments, each of the plurality of root segments having a predetermined root static moment and being configured to be coupled to a respective tip segment of the plurality of tip segments to form a respective segmented rotor blade;
determining a weight of each of the plurality of tip segments;
determining an initial tip static moment for each tip segment of the plurality of tip segments based on the weight of the tip segment, the initial tip static moment of at least one tip segment of the plurality of tip segments differing from the initial tip static moments of the remainder of the plurality of tip segments; and
adding mass to each of the plurality of tip segments to increase the initial tip static moment for each tip segment of the plurality of tip segments to a predetermined tip static moment, the predetermined tip static moment being greater than each of the individual initial tip static moments of all of the plurality of tip segments.
10. The method of claim 9 , further comprising:
weighing each of the plurality of root segments;
determining an initial root static moment for each root segment of the plurality of root segments based on the weight of the root segment, the initial root static moment of at least one root segment of the plurality of root segments differing from the initial root static moments of the remainder of the plurality of root segments; and
selecting the predetermined root static moment as the highest initial root static moment of the plurality of root segments.
11. The method of claim 10 , further comprising adding mass to each root segment of the plurality of root segments having an initial root static moment that is less than the predetermined root static moment to increase the initial root static moment for the root segment to the predetermined root static moment.
12. The method of claim 9 , further comprising determining a center of gravity for each tip segment of the plurality of tip segments, wherein determining the initial tip static moment for each tip segment of the plurality of tip segments comprises determining the initial static moment for each tip segment of the plurality of tip segments based on both the weight of the tip segment and a location of the center of gravity of the tip segment.
13. The method of claim 9 , wherein adding mass to each of the plurality, of tip segments comprises adding mass within a balance box installed within an interior of each of the plurality of tip segments.
14. The method of claim 9 , wherein each tip segment of the plurality of tip segments extends lengthwise between a joint end and a tip end and defines a spanwise length between the joint and tip ends, the balance box being located within the interior of each tip segment of the plurality of tip segments a distance from the joint end equal to less than 25% of the spanwise length.
15. The method of claim 9 , wherein the predetermined tip static moment corresponds to a static moment that is equal to or greater than a maximum static moment for the plurality of tip segments based on allowable manufacturing variations.
16. The method of claim 9 , wherein the initial tip static moment of each tip segment of the plurality of tip segments differs from the initial tip static moments of the remainder of the plurality of tip segments.
17. The method of claim 9 , further comprising pairing each tip segment of the plurality of tip segments with a respective root segment of the plurality of root segments.