Rotor blade joint assembly with multi-component shear web

Abstract

A wind turbine rotor blade joint assembly and method of manufacturing same is disclosed. The rotor blade includes an upper shell member having a spar cap configured on an internal face thereof and a lower shell member having a spar cap configured on an internal face thereof. A shear web extends between the spar caps along a longitudinal length of the blade. The shear web includes first and second longitudinally aligned components that extend from and are integral with respective spar caps. A joint assembly is configured between facing transverse ends of the first and second components of the shear web. The joint assembly includes a connecting structure configured to receive the transverse ends of the first and second components. The connecting structure is infused and integral with the first component of the shear web and bonded with the second component of the shear web.

Claims

1. A wind turbine rotor blade, comprising: an upper shell member having a spar cap configured on an internal face thereof; a lower shell member having a spar cap configured on an internal face thereof; a shear web extending between said spar caps along a longitudinal length of said blade, said shear web further comprising first and second components extending from and integral with respective said spar caps; and, a joint assembly configured between facing transverse ends of said first and second components of said shear web, said joint assembly further comprising: a connecting structure comprising a plurality of connecting members, each connecting member comprising an H-shaped cross-section defined by generally parallel side walls connected together by a chord-wise extending structural wall, the parallel side walls and the chord-wise extending structural wall of each connecting member having a first compartment and second compartment, the first and second compartments of the connecting members configured to receive said transverse end of said first and second components, respectively, wherein said connecting structure is infused and integral with said first component of said shear web, and wherein said connecting structure is bonded with said second component of said shear web.

2. The wind turbine rotor blade of claim 1, wherein said plurality of connecting members are aligned end to end in a span-wise direction of the rotor blade, each of the plurality of connecting members contacting adjacent connecting members.

3. The wind turbine rotor blade of claim 2, wherein said second compartments of said plurality of connecting members comprise one or more flared ends configured to guide said second component of said shear web within said second compartments of said plurality of connecting members.

4. The wind turbine rotor blade of claim 2, wherein said joint assembly further comprises an adhesive configured within said second compartments of each of the plurality of connecting members so as to bond said second component of said shear web within said second compartments.

5. The wind turbine rotor blade of claim 4, wherein said adhesive comprises one of or a combination of the following: a bond paste, a binder, a tape, a gum, a wax, a plaster, a grout, a resin, an epoxy, a sealant, or a glue.

6. The wind turbine rotor blade of claim 1, wherein said connecting structure comprises a flexible material.

7. The wind turbine rotor blade of claim 1, wherein said joint assembly further comprises one or more fasteners configured to bond said connecting structure to said second component of said shear web.

8. The wind turbine rotor blade of claim 1, said first and second components of said shear web comprise longitudinal side walls that surround a filler material, the longitudinal side walls extending substantially perpendicular from said respective spar caps and being bonded to said respective spar caps at a juncture between said first or second component and said respective spar caps.

9. The wind turbine rotor blade of claim 8, wherein said longitudinal side walls and said filler material of said first and second components are infused directly with respective said spar caps.

10. A method for manufacturing a joint assembly for a wind turbine rotor blade, said method comprising: infusing a first component of a shear web with a first spar cap of a lower shell member of the rotor blade; infusing a second component of the shear web onto an opposing spar cap of an upper shell member of the rotor blade; forming a connecting structure having an H-shaped cross-section configured to join the first and second components of the shear web, the connecting structure having a plurality of connecting members, the plurality of connecting members each having a first compartment and second compartment; infusing the first component of the shear web within the first compartments of the plurality of connecting members; and, inserting the second component of the shear web within the second compartments of the plurality of connecting members so as to join the lower and upper shell members.

11. The method of claim 10, further comprising applying an adhesive within the second compartments of the plurality of connecting members so as to secure the second component of the shear web within the second compartments of the plurality of connecting members.

12. The method of claim 11, wherein the adhesive comprises one of or a combination of the following: a bond paste, a binder, a tape, a gum, a wax, a plaster, a grout, a resin, an epoxy, a sealant, or a glue.

13. The method of claim 10, further comprising securing the connecting structure to the second component of the shear web via one or more fasteners.

14. The method of claim 10, further comprising aligning the plurality of connecting members end to end in a span-wise direction of the rotor blade.

15. The method of claim 10, wherein infusing the first and second components of the shear web with the first and second spar caps of the lower and upper shell members further comprises: infusing longitudinal side walls to the respective spar caps, the longitudinal side walls extending substantially perpendicular from the respective spar caps; and inserting a tiller material within the longitudinal side walls so as to form the first and second components such that the first and second components of the shear web are infused directly with the respective spar caps.

16. The method of claim 10, wherein each of the plurality of connecting members further comprises one or more flared ends configured to guide the second component of the shear web within the second compartments of the plurality of connecting members.

17. The method of claim 10, wherein the connecting structure comprises a flexible material.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) 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:

(2) FIG. 1 illustrates a perspective view of a conventional wind turbine;

(3) FIG. 2 illustrates a perspective view of a conventional wind turbine blade;

(4) FIG. 3 illustrates a cross-sectional view of an exemplary wind turbine blade incorporating aspects of the invention;

(5) FIG. 4 illustrates an enlarged cross-sectional component view of a multi-component shear web joint assembly in accordance with an embodiment of the invention;

(6) FIG. 5 illustrates one embodiment of a connecting structure according to the present disclosure;

(7) FIG. 6 illustrates a schematic diagram of one embodiment of the manufacturing process steps according to the present disclosure; and,

(8) FIG. 7 illustrates one embodiment of a method of manufacturing a multi-component shear web joint assembly in accordance with an embodiment of the invention.

DETAILED DESCRIPTION OF THE INVENTION

(9) 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 include such modifications and variations as come within the scope of the appended claims and their equivalents.

(10) Generally, the present subject matter is directed to a wind turbine rotor blade having a multi-component shear web configuration joined by a joint assembly with a single bonded joint. More specifically, the wind turbine rotor blade includes first and second shell members each having a spar cap configured on an internal face thereof. A shear web extends between the spar caps along a longitudinal length or span of the rotor blade and includes first and second components extending from and integral with respective spar caps. The joint assembly is configured between facing transverse ends of the first and second components of the shear web and includes a connecting structure configured to receive the transverse ends of the first and second components. Further, the connecting structure is infused with the first component of the shear web and bonded with the second component of the shear web.

(11) The present subject matter provides numerous advantages not present in the prior art. For example, the present disclosure reduces and/or eliminates the number of bonded joints, i.e. between the shear web and the spar caps, in the joint assembly by infusing the shear web components directly with the spar caps. In addition, the connecting structure, which in various embodiments has an H-shaped cross-section, may be integral with the first component of the shear web. Thus, the joint assembly, in certain embodiments, may require only one bonded joint between the connecting structure and the second component of the shear web. The connecting structure also provides further reinforcement to the joint assembly. In addition, the connecting structure controls and/or restricts the adhesive used to bond the connecting structure and the second component of the shear web. In still further embodiments, the connecting structure may be constructed of a flexible material such that it can move or bend with the rotor blade as needed.

(12) Referring now to the drawings, FIG. 1 illustrates a wind turbine 10 of conventional construction. The wind turbine 10 includes a tower 12 with a nacelle 14 mounted thereon. A plurality of rotor blades 16 are mounted to a rotor hub 18, which is in turn connected to a main flange that turns a main rotor shaft. The wind turbine power generation and control components are housed within the nacelle 14. The view of FIG. 1 is provided for illustrative purposes only to place the present invention in an exemplary field of use. It should be appreciated that the invention is not limited to any particular type of wind turbine configuration.

(13) Referring now to FIG. 2, a more detailed view of one of the rotor blades 16 of FIG. 1 is illustrated. As shown, the rotor blade 16 includes an upper shell member 20 and a lower shell member 22. Further, the upper shell member 20 is configured as the suction side surface of the blade 16, while the lower shell member 22 is configured as the pressure side surface of the blade 16. The rotor blade 16 also includes a leading edge 24 and a trailing edge 26, as well as a root portion 28 and a tip portion 30. As is well known in the art, the upper shell member 20 and the lower shell member 22 may be joined together at the leading edge 24 and trailing edge 26. The rotor blade 16 also includes an internal cavity 25 (FIG. 3) in which various structural members, such as spar caps 32 and one or more shear webs 42 according to the present disclosure, may be configured.

(14) Referring now to FIG. 3, a cross-sectional view of the rotor blade 16 of FIG. 2 is illustrated and incorporates various aspects of the invention. As shown, the rotor blade 16 includes a joint assembly 62 having at least one internal structural shear web 42 that spans between the upper 20 and lower shell members 22. In particular embodiments, the shear web 42 spans between structural spar caps 32 that are fixed to the internal faces of the shell members 20, 22. In accordance with aspects of the invention, the shear web 42 is a multi-component combination with a first component 50 affixed to the spar cap 32 on the lower shell member 22 and a second component 56 affixed to the spar cap 32 on the upper shell member 20.

(15) Referring now to FIG. 4, the shear web components 50, 56 may be formed similar to conventional shear webs with a filler material 54 between laminated side walls 74, 76 (“skin”), or as any other suitable structural member. For example, in various embodiments, the components 50, 56 may be affixed to respective spar caps 32 by any suitable bonding or attachment means, e.g. by directly molding or infusing the components 50, 56 with the spar caps 32, as depicted for example in FIG. 4. In this type of embodiment, the components 50, 56 may include longitudinal side walls 74, 76 that are infused directly to the respective spar caps 32 at a juncture between the first and second component 50, 56. Further, the longitudinal side walls 74, 76 may extend substantially perpendicular from the respective spar caps 32. In addition, the components 50, 56 may include a filler material 54 that is infused into longitudinal side walls 74, 76 such that they are integral with respective spar caps 32.

(16) The filler material 54 may generally include any suitable material which is capable of being injected between the longitudinal side walls 74, 76. For example, in several embodiments, the filler material 54 may comprise a relatively lightweight, low-density foam material. More specifically, the filler material 54 may include a foam material having a density ranging from about 0.5 pounds per cubic feet (lbs/ft.sup.3) to about 3 lbs/ft.sup.3, more preferably about 2 lbs/ft.sup.3. In further embodiments, the filler material 54 may have a density of less than 0.5 lbs/ft.sup.3 or a density greater than 3 lbs/ft.sup.3, such as 20 lbs/ft.sup.3, or any other suitable density. Suitable low-density foam materials may include, but are not limited to, polystyrene foams (e.g., expanded polystyrene foams), polyurethane foams (e.g. polyurethane closed-cell foam), other foam rubbers/resin-based foams and various other open cell and closed cell foams. Alternatively, the filler material 54 may include other suitable low-density materials, such as balsa wood, cork, and the like.

(17) Referring generally to FIGS. 3 and 4, the joint assembly 62 also includes a connecting structure 64 configured between the aligned transverse ends 52, 58 of the shear web components 50, 56 at an intermediate point along the longitudinal aspect of the shear web 42. The connecting structure 64 may be variously configured as explained in greater detail below. For example, as shown, the connecting structure 64 may be configured to receive the transverse ends 52, 58 of the first and second components 50, 56. In addition, the connecting structure 64 may be integral with the first component 50 of the shear web 42 and may be bonded with the second component 56 of the shear web 42.

(18) In various embodiments, and referring particularly to FIG. 5, the connecting structure 64 may generally include one or more connecting members 65 generally aligned end to end along a span or span-wise direction 28 of the rotor blade 16. As such, the individual connecting members 65 may be easier to handle and install than a single connecting structure than extends the entire span 28 of the rotor blade 16. For example, as shown in the embodiment of FIG. 5, the connecting structure 64 includes four connecting members 65. It should be understood by those skilled in the art that any number of connecting members 65 may be utilized in the connecting structure 64, including more than four or less than four.

(19) In addition, it should be understood that the connecting structure 64 may be located at any location along the longitudinal aspect or height H of the shear web 42. For example, as illustrated in the embodiment of FIG. 4, the connecting structure 64 is located at a location corresponding to approximately 50% of the height of the shear web 42 from each respective spar cap 32. In still further embodiments, the connecting structure 64 may be located at about 25% of the height H from one spar cap and 75% of the height H from the opposing spar cap 32. In still further embodiments, the connecting structure 64 may be located at any percent (%) height H of the shear web 42.

(20) In additional embodiments, the connecting members 65 may include any suitable cross-sectional shape. For example, as shown in FIGS. 3-5, each of the connecting members 65 has an H-shaped cross-section. In still further embodiments, the connecting members 65 may have an I-shaped cross-section or any other shape having the capability of functioning as described herein. More specifically, as shown in FIGS. 4 and 5, the H-shaped cross-section generally includes a first section 66 or compartment and a second section 68 or compartment configured to receive the transverse ends 52, 58 of the shear web components 50, 56, respectively. In addition to receiving the transverse ends 52, 58 of the shear web components 50, 56, the first and second sections 66, 68 may also be configured to receive a portion of the shear web components 50, 56, e.g. a portion of the filler material 54 and the longitudinal side walls 74, 76.

(21) Referring particularly to FIG. 4, the joint assembly 62 may also include an adhesive 70 configured within the second sections 68 of each connecting member 65 so as to bond the second component 56 of the shear web 42 within the second sections 68. It should be understood that the adhesive 70 may include any suitable adhesive now known or later developed in the art, including, but not limited to any one of or a combination of the following: a bond paste, a binder, a tape, a gum, a wax, a plaster, a grout, a resin, an epoxy, a sealant, a glue, or similar. In alternative embodiments, the joint assembly 62 may include one or more fasteners configured to secure the second component 56 of the shear web 42 within the connecting structure 64. For example, rather than using adhesive 70, the second component 56 may be secured within the second section 68 of the connecting member 65 via a mechanical fastener, a bolt, a screw, a pin, a dowel, or similar.

(22) Referring particularly in FIGS. 4 and 5, in certain embodiments, the second sections 68 of the connecting members 65 may also include one or more flared ends 72. The flared ends 72 may be configured to guide the second component 56 of the shear web 42 within the connecting structure 64. In addition, the flared ends 72 may assist in retaining a quantity of adhesive 70 within the second section 68 of the connecting structure 64.

(23) In addition, it should be understood that the connecting structure 64 may be constructed of any suitable material. For example, in one embodiment, the connecting structure 64 may be constructed of a flexible material. As used herein, the term “flexible” is meant to encompass its general broad meaning and the ability of the material to bend or flex with the rotor blade 16 easily without breaking. For example, in various embodiments, the flexible material may include any suitable elastomeric material. Suitable elastomeric materials may include woven or nonwoven elastomeric materials, elastomeric films, elastomeric laminates and combinations thereof. The flexible material may also include other woven or nonwoven materials, or stretchable but inelastic materials. As used herein and in the claims, the terms “elastic” and “elastomeric” have their usual broad meanings. For example, for purposes of this invention “elastic” and “elastomeric” may be conveniently defined as any material, such as natural or synthetic rubber, that is able to resume its original shape when a deforming force is removed. It should also be understood that the terms “elastic” and “elastomeric” are not limited by the definition and can have any suitable definition commonly known in the art.

(24) Referring now to FIG. 6, a schematic diagram of one embodiment of the manufacturing process steps according to the present disclosure is illustrated. As shown in STEP 1, a connecting structure 64 having any combination of the features described herein is formed using any suitable manufacturing technique. For example, in one embodiment, the connecting structure 64 is formed by infusion molding. In addition, as mentioned, the connecting structure 64 may have one or more connecting members 65 having first and second sections 66, 68. At STEP 2, the first component 50 of the shear web 42 is infused with a first spar cap 32 of the lower shell member 22 of the rotor blade 16. For example, in one embodiment, the first component 50 is formed by infusing the longitudinal side wall 76 directly to the first spar cap 32. The filler material 54 may then be injected into the longitudinal side wall 76 such that the first component 50 of the shear web 42 is integral with the first spar cap 32. The pre-fabricated connecting structure 64 is then infused with the first component 50 of the shear web. At STEP 3, the second component 56 of the shear web 42 is infused with a second, opposing spar cap 34 of the upper shell member 20 of the rotor blade 16. For example, in one embodiment, the second component 56 is formed by infusing the longitudinal side wall 74 directly to the second spar cap 34. The filler material 54 may then be injected into the longitudinal side wall 74 such that the second component 56 of the shear web 42 is integral with the second spar cap 34. At STEP 4, adhesive 70 is applied within the second section 68 of the connecting member 65 so as to provide a means for securing the second component 56 of the shear web 42 within the second section 68 of the connecting member 64. Thus, at STEP 5, the first and second components 50, 56 may be joined by inserting the second component 56 formed in STEP 3 into the second section 68 of the connecting member 64.

(25) Referring now to FIG. 7, a flow diagram of a method 100 for manufacturing a joint assembly for a wind turbine rotor blade is illustrated. As shown, the method 100 includes a step 102 of infusing a first component of a shear web with a first spar cap of a lower shell member of the rotor blade. Another step 104 includes infusing a second component of the shear web onto an opposing spar cap of an upper shell member of the rotor blade. The method 100 also includes a step 106 of forming a connecting structure configured to join the first and second components of the shear web, the connecting structure having one or more connecting members, the connecting members each having a first section and second section. A next step 108 includes infusing the first component of the shear web within the first sections of the connecting members. A further step 110 includes inserting the second component of the shear web within the second sections of the connecting members so as to join the lower and upper shell members.

(26) While the present subject matter has been described in detail with respect to specific exemplary embodiments and methods thereof, it will be appreciated that those skilled in the art, upon attaining an understanding of the foregoing, may readily produce alterations to, variations of, and equivalents to such embodiments. Accordingly, the scope of the present disclosure is by way of example rather than by way of limitation, and the subject disclosure does not preclude inclusion of such modifications, variations and/or additions to the present subject matter as would be readily apparent to one of ordinary skill in the art.