ROTOR BLADE ASSEMBLY
20190271298 ยท 2019-09-05
Inventors
- Uffe Eriksen (Horsens, DK)
- Jens Hald Jensen (Give, DK)
- Jesper Bjerre Pedersen (Torring, DK)
- Jeppe Soee (Ronde, DK)
Cpc classification
B66C1/62
PERFORMING OPERATIONS; TRANSPORTING
F05B2240/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02P70/50
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y02E10/728
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B66C1/108
PERFORMING OPERATIONS; TRANSPORTING
F03D13/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2230/61
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D13/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D13/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/72
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F03D80/50
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F03D13/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Provided is a wind turbine rotor blade assembly including a rotor blade with an airfoil section and a root section; a carrier assembly arranged in an interior cavity of the blade and including a number of lifting fittings, wherein a lifting fitting and adapted to engage with a connector of a blade lifting apparatus. A method of lifting a wind turbine rotor blade is also provided.
Claims
1. A wind turbine rotor blade assembly comprising a rotor blade with an airfoil section and a root section; a carrier assembly arranged in an interior cavity of the rotor blade and including a number of lifting fittings, wherein a lifting fitting is adapted to engage with a connector of a blade lifting apparatus.
2. The wind turbine rotor blade assembly according to claim 1, wherein the carrier assembly is shaped to engage with a surface of the interior cavity of the rotor blade.
3. The wind turbine rotor blade assembly according to claim 1, wherein the carrier assembly comprises a plate orthogonal to a longitudinal axis of the rotor blade.
4. The wind turbine rotor blade assembly according to claim 1, wherein the carrier assembly is arranged in the region of the center of mass of a load comprising at least the rotor blade.
5. The wind turbine rotor blade assembly according to claim 1, wherein a lifting fitting comprises a bushing to receive a bolt of the blade lifting apparatus and/or a lifting fitting comprises a trunnion to receive a sling of the blade lifting apparatus and/or a lifting fitting comprises a peg to fit into a tongue of the blade lifting apparatus.
6. The wind turbine rotor blade assembly according to claim 1, comprising a shaft arranged to extend into the interior cavity of the rotor blade, and wherein the carrier assembly is arranged on the shaft.
7. The wind turbine rotor blade assembly according to claim 6, comprising a shaft end bearing arranged about the outer end of the shaft, and wherein the carrier assembly and the shaft end bearing are realized in a single unit.
8. The wind turbine rotor blade assembly according to claim 6, comprising a shaft end bearing arranged about the outer end of the shaft, and wherein the carrier assembly is mounted on the shaft at a distance from the shaft end bearing.
9. The wind turbine rotor blade assembly according to claim 1, comprising an access opening in the rotor blade body, which access opening is arranged to provide access to the lifting fitting in the interior cavity of the rotor blade.
10. A blade lifting apparatus comprising a lifting yoke realized for connection to a crane; a main blade holder mounted to the lifting yoke and comprising at least one connector adapted to engage with a lifting fitting of a carrier assembly of a wind turbine rotor blade assembly according to claim 1.
11. The blade lifting apparatus according to claim 10, comprising a number of auxiliary blade holders mounted to the lifting yoke, and wherein a blade holder has a contact surface shaped to lie against an outer surface of a wind turbine rotor blade.
12. A method of lifting a wind turbine rotor blade, which method comprises the steps of providing a carrier assembly including a number of lifting fittings, wherein a lifting fitting is adapted to engage with a connector of a blade lifting apparatus; arranging the carrier assembly in an interior cavity of the rotor blade; bringing the blade lifting apparatus into place at the exterior of the rotor blade; engaging a connector of the blade lifting apparatus to a lifting fitting; performing a blade lifting maneuver and subsequently disengaging the connector of the blade lifting apparatus from the lifting fitting.
13. The method according to claim 12, comprising a prior step of forming an access opening in the rotor blade to provide access to a lifting fitting arranged in the interior cavity of the rotor blade.
14. The method according to claim 13, comprising the step of sealing an access opening after completion of a blade lifting maneuver.
15. The method according to claim 12, wherein the step of engaging a connector of the blade lifting apparatus to the lifting fitting comprises extending a bolt into a bushing and/or arranging a sling around a trunnion and/or fitting a tongue over a peg.
Description
BRIEF DESCRIPTION
[0018] Some of the embodiments will be described in detail, with reference to the following figures, wherein like designations denote like members, wherein:
[0019]
[0020]
[0021]
[0022]
[0023]
[0024]
[0025]
[0026]
[0027]
[0028]
[0029]
[0030]
[0031]
[0032] In the diagrams, like numbers refer to like objects throughout. Objects in the diagrams are not necessarily drawn to scale.
DETAILED DESCRIPTION
[0033]
[0034] The other, inner end of the shaft is not shown, but it will be understood that the inner end or root end of the shaft engages with the blade root end by means of a root end bearing and a pitch system. When installed on the hub of a wind turbine, the inner shaft will extend outward from the hub and is stationary relative to the hub; and the rotor blade can be pitched by a pitch drive unit that turns the rotor blade about the inner shaft.
[0035]
[0036]
[0037] The diagram shows that the carrier assembly 2 and the blade adapter 20 of the shaft 12 are realized as separate entities. In this embodiment, the carrier assembly 2 is arranged around the shaft 12 and is positioned further inward (i.e. toward the root end) than the outer bearing 121, with a distance D between carrier assembly 2 and blade adapter 20. The distance D may be as large or as small as necessary to achieve a stable lifting point. This type of embodiment may be exemplary to allow more freedom in deciding where to place the carrier assembly 2, for example to achieve a lifting point (which may coincide with the crane hook as shown here) that is positioned directly above the center of mass of the combined blade/lifting apparatus, as indicated in the diagram. Another reason to manufacture the carrier assembly separately from the blade adapted may be to avoid making any structural alterations to an existing bearing/adapter design.
[0038] The exemplary embodiment shows that the main blade holder 40 comprises a pair of vertical bolts 41 extending downward. The bolt diameters and the bolt spacing are such to allow the bolts to extend through bushings of the lifting fitting of
[0039]
[0040]
[0041] Since the blade root end 11 is generally heavy on account of its thickness, the shaft 12 is heavy since it is made of a structurally strong material such as steel, but the airfoil section 10 is thin and relatively light in spite of its length, the center of mass of the blade 1 can be located near the outer end of the shaft 12. This makes the position of the outer bearing 121 a good candidate for the carrier 2 of the inventive rotor blade assembly, and a bearing/blade adapter can simultaneously act as the carrier 2 for the lifting fitting(s) 3.
[0042] The root end diameter of the inner shaft 12 can be in the order of 4-7 m, while the diameter of the outer end of the inner shaft 12 can be in the order of 2-4 m. The inner shaft 12 is left open at its outer end so that a technician can enter the blade interior cavity C in order to access the lifting fittings 3 prior to the lifting maneuver (e.g. to place nuts over bolt ends, to arrange slings over trunnions, to fit a tongue over a horizontal pin, etc.) and to perform the reverse operation at the end of a lifting maneuver. The diagram also clearly shows that the weight of the blade 1 is held mainly by the main blade holder 40 and the lifting fitting connection, while the auxiliary blade holders 42 serve to stabilize the blade 1 during the lifting maneuver.
[0043]
[0044]
[0045] As described above, access openings are provided in the outer surface of the blade to allow connectors of the main blade holder to mate with the lifting fittings. Such access openings can be sealed using an appropriately shaped plug and/or an appropriate adhesive after completion of a final lifting maneuver, for example after the blade has been lifted into place and installed on the hub of a wind turbine.
[0046] Although the present invention has been disclosed in the form of preferred embodiments and variations thereon, it will be understood that numerous additional modifications and variations could be made thereto without departing from the scope of the invention.
[0047] For the sake of clarity, it is to be understood that the use of a or an throughout this application does not exclude a plurality, and comprising does not exclude other steps or elements.