The present disclosure relates generally to wind turbines, and more particularly to systems and methods for suspending a rotor blade of a wind turbine uptower.
Wind power is considered one of the cleanest, most environmentally friendly energy sources presently available, and wind turbines have gained increased attention in this regard. A modern wind turbine typically includes a tower, generator, gearbox, nacelle, and one or more rotor blades. The rotor blades capture kinetic energy of wind using known airfoil principles. The rotor blades transmit the kinetic energy in the form of rotational energy so as to turn a shaft coupling the rotor blades to a gearbox, or if a gearbox is not used, directly to the generator. The generator then converts the mechanical energy to electrical energy that may be deployed to a utility grid.
Further, each of the rotor blades are configured to rotate about a pitch axis via a pitch bearing mounted between the rotor blade and the hub. If one of the pitch bearings becomes damaged and needs to be replaced and/or repaired, a large crane must be transported to the wind turbine site in order to provide a means for raising and/or lowering the associated rotor blade relative to the hub. Operation of such cranes is complex and the process for raising and/or lowering the rotor blades using such cranes is time-consuming and labor intensive.
Accordingly, improved methods and related systems for suspending a rotor blade of a wind turbine uptower while the pitch bearing is repaired or replaced that addresses the aforementioned issues would be welcomed in the technology.
Aspects and advantages of the invention will be set forth in part in the following description, or may be obvious from the description, or may be learned through practice of the invention.
In one aspect, the present disclosure is directed to a method for suspending a rotor blade uptower. The method includes mounting a first end of a support structure at a first uptower location of the wind turbine. The method also includes securing the rotor blade to a second end of the support structure. Further, the method includes mounting at least one pulley block assembly between a second uptower location and the support structure. Moreover, the method includes routing at least one pulley cable from at least one winch over the at least one pulley block assembly. In addition, the method includes detaching the rotor blade from the hub of the wind turbine. Once the rotor blade is detached, the method includes rotating the support structure about the first end via coordinated winch operation so as to lower the rotor blade a predetermined distance away from the hub. Thus, the method also includes suspending the rotor blade at the predetermined distance away from the hub via the support structure.
In one embodiment, the method may include positioning the rotor blade toward a ground location in a substantially six o'clock position. In another embodiment, the method may also include detaching the rotor blade from the hub of the wind turbine with a pitch bearing attached thereto.
In further embodiments, the method may include securing the rotor blade to the second end of the support structure via one or more clamp members.
In several embodiments, the first and second uptower locations may be located on a bedplate and/or a nacelle of the wind turbine. In such embodiments, the method may include mounting the first end of the support structure to the bedplate at a hinge point and rotating the support structure about the hinge point via coordinated winch operation so as to lower the rotor blade the predetermined distance away from the hub.
In additional embodiments, the support structure may include, at least, a first support structure arm and a second support structure arm. In such embodiments, the method may include mounting first ends of the first and second support structure arms to opposing sides of the bedplate.
In particular embodiments, the pulley block assembly(ies) may include at least one first pulley block mounted on the bedplate of the wind turbine and at least one second pulley block mounted to the support structure. More specifically, in one embodiment, the method may include providing first and second pulley block assemblies on opposing sides of the bedplate. For example, in several embodiments, the first and second pulley block assemblies may include at least one first pulley block mounted at the second uptower location of the wind turbine and at least one second pulley block mounted to the first and second support structure arms.
In further embodiments, the step of rotating the support structure about the first uptower location via coordinated winch operation so as to lower the rotor blade the predetermined distance away from the hub may include lowering the rotor blade from a first position at the hub to a second position that is closer to a tower of the wind turbine than the first position. In additional embodiments, the method may include securing the rotor blade to the tower of the wind turbine at a blade root and a blade tip of the rotor blade during suspension thereof via at least one of a clamp member, a sleeve, one or more support lines, or combinations thereof.
In another aspect, the present disclosure is directed to a system for suspending a rotor blade uptower. The system includes a support structure having a first end and a second end. The first end includes a hinge point for securing to a first uptower location of the wind turbine. The second end is configured to receive and secure the rotor blade thereto. The system further includes at least one pulley block assembly mounted between the first uptower location and the support structure. Moreover, the system includes at least one winch and at least one pulley cable routed from at least one winch over the at least one pulley block assembly. Thus, the support structure is configured to rotate about the hinge point via coordinated winch operation so as to lower the rotor blade a predetermined distance away from a hub of the wind turbine and suspend the rotor blade at the predetermined distance away from the hub.
In one embodiment, the second end of the support structure may include one or more clamp members configured to receive and secure the rotor blade therein. It should be further understood that the system may further include any of the additional features as described herein.
These and other features, aspects and advantages of the present invention will become better understood with reference to the following description and appended claims. The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and, together with the description, serve to explain the principles of the invention.
A full and enabling disclosure of the present invention, including the best mode thereof, directed to one of ordinary skill in the art, is set forth in the specification, which makes reference to the appended figures, in which:
Reference now will be made in detail to embodiments of the invention, one or more examples of which are illustrated in the drawings. Each example is provided by way of explanation of the invention, not limitation of the invention. In fact, it will be apparent to those skilled in the art that various modifications and variations can be made in the present invention without departing from the scope or spirit of the invention. For instance, features illustrated or described as part of one embodiment can be used with another embodiment to yield a still further embodiment. Thus, it is intended that the present invention covers such modifications and variations as come within the scope of the appended claims and their equivalents.
Referring now to the drawings,
Referring now to
The wind turbine 10 may also include a controller 35 centralized within the nacelle 16. Alternatively, the controller 35 may be located within any other component of the wind turbine 10 or at a location outside the wind turbine 10. Further, the controller 35 may be communicatively coupled to any number of the components of the wind turbine 10 in order to control the operation of such components and/or implement various correction actions as described herein.
Still referring to
Referring now to
Moreover, as shown in
Various embodiments of methods for suspending one of the rotor blades 22 from the hub 20 of the wind turbine 10, including various system components that may be used in performing such methods, will now be described with reference to
Referring particularly to
Referring particularly to
Thus, as shown in
Further, as shown at 102, the method 100 includes mounting the first end 64 of the support structure 62 at the first uptower location 67 of the wind turbine 10. More specifically, as shown in
As shown at 106, the method 100 includes mounting at least one pulley block assembly 70 between a second uptower location 69 and the support structure 62. As shown at 108, the method 100 includes routing at least one pulley cable 74 from at least one winch 70 over the at least one pulley block assembly 70. In several embodiments, the first and second uptower locations 67, 69 may be located on the bedplate 58 of the wind turbine 10. Alternatively, the first and second uptower locations 67, 69 may be located at any suitable location within or outside of the nacelle 16 of the wind turbine 10. Thus, as shown in
As shown at 110, the method 100 includes detaching the rotor blade 22 from the hub 20 of the wind turbine 10. In particular embodiments, the rotor blade 22 may be detached from the hub 20 with or without the pitch bearing 52 still attached thereto. If the pitch bearing 52 remains attached, the pitch bearing replacement process can be expedited because the rotor blade 22 and the pitch bearing 52 are detached from the hub 20 at the same time and the bearing removal from the rotor blade 22 can occur on the ground. Removing the pitch bearing 52 from the blade 22 on the ground can be safer than uptower and can occur in parallel with the bearing installation process to the hub 20.
Once the rotor blade 22 is detached, as shown at 112, the method 100 includes rotating the support structure 62 about the first end 64 via coordinated winch operation so as to lower the rotor blade 22 a predetermined distance 76 away from the hub 20. More specifically, in one embodiment, the method 100 may include rotating the support structure 62 about the hinge point 65 via coordinated winch operation so as to lower the rotor blade 22 the predetermined distance 76 away from the hub 20. In addition, as shown in
In additional embodiments, the method 100 may include securing the rotor blade 22 to the tower 12 of the wind turbine 10 during suspension, e.g. to mitigate tower strikes by the rotor blade 22. For example, in certain embodiments, the rotor blade 22 may be secured to the tower 12 at the blade root 24 and the blade tip 26 of the rotor blade 22 during suspension thereof via at least one of an additional clamp member, a sleeve, one or more support lines, or combinations thereof.
More specifically, as shown in
Further, as shown in
In addition, as shown in
Still referring to
This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they include structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.
Number | Name | Date | Kind |
---|---|---|---|
7353603 | Wobben | Apr 2008 | B2 |
7735290 | Arsene | Jun 2010 | B2 |
7785073 | Wobben | Aug 2010 | B2 |
7832101 | Koesters | Nov 2010 | B2 |
7877934 | Livingston et al. | Feb 2011 | B2 |
8033791 | Watanabe | Oct 2011 | B1 |
8052396 | Wobben | Nov 2011 | B2 |
8069634 | Livingston et al. | Dec 2011 | B2 |
8083212 | Numajiri et al. | Dec 2011 | B2 |
8118552 | Nies | Feb 2012 | B2 |
8191253 | Vangsy | Jun 2012 | B2 |
8240962 | Livingston et al. | Aug 2012 | B2 |
8360398 | Diaz De Corcuera et al. | Jan 2013 | B2 |
8528735 | Nies | Sep 2013 | B2 |
8562302 | Bakhuis et al. | Oct 2013 | B2 |
8584355 | Holling | Nov 2013 | B2 |
8595931 | Riddell et al. | Dec 2013 | B2 |
8602700 | Johnson | Dec 2013 | B2 |
8651462 | Van Berlo et al. | Feb 2014 | B2 |
9617981 | Hancock | Apr 2017 | B2 |
9651021 | Neumann et al. | May 2017 | B2 |
20070266538 | Bervang | Nov 2007 | A1 |
20070290426 | Trede et al. | Dec 2007 | A1 |
20090167023 | Nies | Jul 2009 | A1 |
20100018055 | Fomsgaard et al. | Jan 2010 | A1 |
20100028152 | Tomohro et al. | Feb 2010 | A1 |
20100135797 | Nies | Jun 2010 | A1 |
20100139062 | Reed et al. | Jun 2010 | A1 |
20100254813 | Dawson et al. | Oct 2010 | A1 |
20110142636 | Curtin | Jun 2011 | A1 |
20120027561 | Riddell et al. | Feb 2012 | A1 |
20120076663 | From | Mar 2012 | A1 |
20120137481 | Lindberg et al. | Jun 2012 | A1 |
20120217089 | Fenger | Aug 2012 | A1 |
20130025113 | Arocena De La Rua et al. | Jan 2013 | A1 |
20130074335 | Amano | Mar 2013 | A1 |
20130098859 | See et al. | Apr 2013 | A1 |
20130236316 | Bitsch et al. | Sep 2013 | A1 |
20130236324 | Bech et al. | Sep 2013 | A1 |
20130318789 | Gabeiras et al. | Dec 2013 | A1 |
20140010658 | Nielsen | Jan 2014 | A1 |
20140010661 | Hancock | Jan 2014 | A1 |
20150048043 | Laurens et al. | Feb 2015 | A1 |
20150226179 | Neumann et al. | Aug 2015 | A1 |
20160327017 | Neumann et al. | Nov 2016 | A1 |
Number | Date | Country |
---|---|---|
2692705 | Aug 2010 | CA |
201400575 | Apr 2016 | DK |
2345811 | Oct 2012 | EP |
2369174 | Nov 2012 | EP |
2616670 | Jul 2013 | EP |
2483677 | Mar 2012 | GB |
2006152862 | Jun 2006 | JP |
WO2010147480 | Dec 2010 | WO |
WO2011064659 | Jun 2011 | WO |
WO2011095167 | Aug 2011 | WO |
WO2012065613 | May 2012 | WO |
Entry |
---|
Extended European Search Report and Opinion issued in connection with corresponding EP Application No. 18183699.0 dated Dec. 10, 2018. |
Number | Date | Country | |
---|---|---|---|
20190017495 A1 | Jan 2019 | US |