SPANWISE SEGMENT CONNECTION STRUCTURE FOR WIND TURBINE BLADES
20230407838 ยท 2023-12-21
Inventors
- Kunlun TAN (Changzhou, CN)
- Yelin LIU (Changzhou, CN)
- Gaoyu BAI (Changzhou, CN)
- Qiuping DU (Changzhou, CN)
- Lei CAO (Changzhou, CN)
- Shihai LIU (Changzhou, CN)
- Xiugang WANG (Changzhou, CN)
- Yichao CAO (Changzhou, CN)
Cpc classification
F05B2240/302
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/0677
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C66/541
PERFORMING OPERATIONS; TRANSPORTING
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
B29C66/116
PERFORMING OPERATIONS; TRANSPORTING
F05B2230/23
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C65/48
PERFORMING OPERATIONS; TRANSPORTING
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
International classification
Abstract
A spanwise segment connection structure for wind turbine blades includes a first segment and a second segment provided along the length direction of the wind turbine blade. At least one splicing surface is provided between the first and second segments; and a structural adhesive layer provided at the splicing surface for splicing and fixing the first and second segments; wherein the bonding length of the structural adhesive layer conforms to the inclination angle of the slope structure, and a biaxial fabric reinforcement layer is provided on the outer side of a skin interface of the splicing surface. The weight of the blade is reduced and the production cost is reduced through the bonding and fixing of the first and second segments. The splicing surface in form of the slope structure increases the bonding area and reduces the stress concentration on the splicing surface of the first and second segments.
Claims
1. A spanwise segment connection structure for wind turbine blades, comprising: a first segment (1) and a second segment (2) provided along the length direction of the wind turbine blade, wherein at least one splicing surface (3), in form of a slope structure, is provided between the first and second segments (1, 2); and a structural adhesive layer (4) provided at the splicing surface (3) for splicing and fixing the first and second segments (1, 2); wherein the bonding length of the structural adhesive layer (4) conforms to the inclination angle of the slope structure, and a biaxial fabric reinforcement layer (5) is provided on the outer side of a skin interface (16) of the splicing surface(3).
2. The spanwise block connection structure for wind turbine blades according to claim 1, wherein an end of the biaxial fabric reinforcement layer (5) smoothly transitions to an outer skin (14).
3. The spanwise block connection structure for wind turbine blades according to claim 1, wherein the splicing position of the outer skin (14) of the splicing surface (3) is provided with a slope recess (6) for laying a reinforcing layer (7) therein.
4. The spanwise block connection structure for wind turbine blades according to claim 1, wherein two splicing surfaces (3) are provided between the first and second segments (1, 2), the two splicing faces (3) symmetrically arranged and diffusing along the direction toward the outer skin (14), and a connecting segment (8) is provided between the first and second segments (1, 2), wherein the connecting segment (8) is bonded and fixed on the splicing surfaces (3) of the first and second segments (1, 2).
5. The spanwise block connection structure for wind turbine blades according to claim 4, wherein the connecting segment (8) is in form of a trapezoidal structure whose outer side is spliced with the outer skin (14) of the first and second segments (1, 2), and its inner side is spliced with an inner skin (15).
6. The spanwise block connection structure for wind turbine blades according to claim 4, wherein the connecting segment (8) is in form of a triangular structure whose outer surface is spliced with the outer skin (14) of the first and second segments (1, 2).
7. The spanwise block connection structure for wind turbine blades according to claim 4, wherein a butting surface including a horizontal portion (9) and a vertical portion (10) is provided between the two splicing surfaces (3), wherein the horizontal portion (9) is bonded and fixed to the connecting segment (8), and the vertical portions (10) of the first and second segments (1, 2) abut each other and are bonded and fixed with a structural adhesive layer (4).
8. The spanwise block connection structure for wind turbine blades according to claim 4, wherein the outer skin (14) of the splicing surface (3) on the first and second segments (1, 2) extends horizontally near one end of the inner skin (15) and fits with the inner skin (15) to form a horizontal butting portion (11), and the horizontal butting portions (11) of the first and second segments (1, 2) abut each other to form a horizontal portion (9) for fixing the connecting segment (8).
9. The spanwise block connection structure for wind turbine blades according to claim 6, wherein the first and second segments (1, 2) adopt fiberglass butt joint (12) or core material butt joint (13) at the interface (16).
Description
DESCRIPTION OF THE DRAWINGS
[0019] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the accompanying drawings to be used in the description of the embodiments or prior art will be briefly described below. It is obvious that the accompanying drawings in the following description are only some of the embodiments recorded in the present invention, and other accompanying drawings can be obtained according to these accompanying drawings without creative work for those of ordinary skill in the art.
[0020]
[0021]
[0022]
[0023]
[0024]
[0025]
[0026]
[0027]
[0028]
[0029]
[0030] Reference signs: 1. First segment; 2. Second segment; 3. Splicing surface; 4. Structural adhesive layer; 5. Biaxial fabric reinforcement layer; 6. Slope recess; 7. Reinforcement layer; 8. Connecting segment; 9. Horizontal portion; 10. Vertical portion; 11. Horizontal butting portion; 12. Fiberglass butt joint; 13. Core material butt joint; 14. Outer skin; 15. Inner skin; 16. Interface.
DESCRIPTION OF THE EMBODIMENTS
[0031] The technical solutions in the embodiments of the present invention will be described clearly and completely in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a portion of the embodiments of the present invention, rather than all the embodiments.
[0032] It should be noted that when an element is referred to as being fixed to another element, it can be directly on the element or an intermediate element may also be present. It should be noted that when an element is referred to as being connected to another element, it can be directly on the element or an intermediate element may also be present. The terms vertical, horizontal, left, right and similar expressions used herein are for illustrative purposes only and do not mean that they are the only modes of implementation.
[0033] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by those skilled in the art of the present invention. The terms used herein are for the purpose of describing specific embodiments only and are not intended to limit the invention. The term and/or used herein includes any and all combinations of one or more of the related listed items.
Embodiment 1
[0034]
[0035] In the present invention, the weight of the blade is reduced and the production cost is reduced through the bonding and fixing of the first and second segments 1, 2. The splicing surface 3 in form of the slope structure provided at the segments of the wind turbine blade along the length direction (span direction) increases the bonding area, reduces the stress concentration on the splicing surface 3, and ensures bonding reliability of the first and second segments 1, 2. In addition, the biaxial reinforcing layer at the skin interface 16 of the splicing surface 3 ensures the uniformity of the force on the blade shell structure, thereby improving the stability of the overall structure of the blade.
[0036] After the biaxial reinforcement layer is bonded and cured, an end of the biaxial fabric reinforcement layer 5 smoothly transitions to an outer skin 14 through a grinding process, which reduces stress concentration and influence on aerodynamic performance.
[0037] In order to meet the profile tolerance requirements, the interface 16 of the outer skin 14 of the splicing surface 3 is provided with a slope recess 6 for laying a reinforcement layer 7 therein, and the strength of the interface 16 is improved through the reinforcement layer 7.
Embodiment 2
[0038] The difference between this embodiment and Embodiment 1 is that two splicing surfaces 3 are adopted in the present embodiment, and the rest of the structure is the same, which will not be repeated here.
[0039] As shown in
[0040] Specifically, the provision of the two splicing surfaces 3 facilitates the control of the accuracy of the connection between the first and second segments 1, 2 to reduce profile tolerances, ensuring the stability of the blade and improving the overall load bearing capacity of the blade.
Embodiment 3
[0041] The difference between this embodiment and Embodiment 2 lies in the shape of the connecting segment 8 and the butt joint structure of the outer skin 14, and the rest of the structures is the same, which will not be repeated here.
[0042] As shown in
[0043] Specifically, the connection section 8 in the form of triangular structure ensures the accuracy of the connection between the first and second segments 1, 2 and at the same time improves the stability at the interface 16.
[0044] Since the tip of the triangular structure faces the inner skin 15 so that the inner skin 15 is bent and butt towards the outer skin 14, it results in a smaller thickness of the core material at the butt joint. In order to increase the connection strength of the inner skin 15, the first and second segments 1, 2 adopt fiberglass butt joint 12 at the interface 16.
Embodiment 4
[0045] The difference between this embodiment and Embodiments 2-3 lies in that a butting surface is added between the two splicing surfaces 3, and the rest of the structure is the same, which will not be repeated here.
[0046] When the first and second segments 1, 2 are relatively thick, a butting surface including a horizontal portion 9 and a vertical portion 10 is provided between the two splicing surfaces 3, as shown in
[0047] Specifically, the two symmetrical splicing surfaces 3 and the horizontal portion 9 form a recess into which the connecting segment 8 is overlapped. The connection between the first segment 1 and the second segment 2 is realized by butt joint of the vertical portion 10. The bonding area between the connecting segment 8 and the first and second segments 1, 2 is increased to ensure the strength of the connecting segment 8, thereby improving the overall load bearing capacity of the segmented blades.
[0048] The core material at the butt joint of the vertical portion 10 has a certain thickness. In order to simplify the process and facilitate the control of the bonding width, the first segment 1 and the second segment 2 adopt the core material butt joint 13 at the interface 16.
Embodiment 5
[0049] The difference between this embodiment and Embodiment 4 lies in the thickness of the core material at the butt joint and in the form of butt joint. As shown in
[0050] Specifically, the outer skin 14 of the first and second segments 1, 2 fits with the inner skin 15, and fiberglass butt joint 12 is adopted at the interface. The two symmetrical splicing surfaces 3 and the horizontal portion 9 form a recess into which the connecting segment 8 is overlapped to increase the bonding area between the connecting segment 8 and the first and second segments 1, 2, ensuring the strength of the connecting segment 8, thereby improving the overall load bearing capacity of the segmented blades.
[0051] Those skilled in the industry should understand that the present invention is not limited by the foregoing embodiments. The foregoing embodiments and descriptions only illustrate the principles of the present invention. Without departing from the spirit and scope of the present invention, the present invention will have various changes and improvements, which fall within the scope of the claimed invention. The scope of protection claimed by the present invention is defined by the appended claims and their equivalents.