Patent Application
20230407838
The present invention relates to the field of wind turbine blade technology, in particular to a spanwise segment connection structure for wind turbine blades.
Wind turbine blades are the basic components of wind turbines that convert wind energy into electrical energy. The blade has the cross-sectional profile of a wing. During operation, the air flowing through the blade creates a pressure difference between its two sides, so that the lift from the pressure side to the suction side acts on the blade, and the lift generates torque on the main rotor shaft, which is connected by gears to a generator that can generate electricity.
In order to make full use of wind energy resources, wind turbines are gradually becoming larger and their blade lengths are also increasing. Rich wind resources are almost located in remote areas, desert areas, offshore or seaside areas and other uninhabited areas with poor transportation conditions, making it quite difficult to transport long blades. At present, some wind turbine blades are segmented along the length direction. However, nowadays, wind turbine blades are becoming increasingly larger and thicker, and segmented along their length direction alone cannot meet transportation conditions.
In the existing modular wind turbine blades, several segments are provided along the length direction, and two adjacent segments are provided with a splicing surface and a connecting structure which passes through the splicing surface for mechanical connection/or hybrid connection with adhesive. However, mechanical and hybrid connections involve metal connections, which can increase the weight of the blades. At the same time, considering lightning protection design, it will inevitably increase the cost beyond the connection.
In view of the above-mentioned problems, the inventor actively carried out research and innovation based on the rich practical experience and professional knowledge in the engineering applications of such products for many years, in order to create a spanwise segment connection structure for wind turbine blades that is more practical.
The technical problem to be solved by the present invention is to provide a spanwise segment connection structure for wind turbine blades in order to achieve the goal of reducing blade weight and cost.
To this end, the present invention provides a spanwise segment connection structure for wind turbine blades, comprising: a first segment and a second segment provided along the length direction of the wind turbine blade, wherein at least one splicing surface, in form of a slope structure, 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.
Further, an end of the biaxial fabric reinforcement layer smoothly transitions to an outer skin.
Further, the splicing position of the outer skin of the splicing surface is provided with a slope recess for laying a reinforcing layer therein.
Further, two splicing surfaces are provided between the first and second segments, wherein the two splicing faces are symmetrically arranged and diffuse along the direction toward the outer skin, and a connecting segment is provided between the first and second segments, wherein the connecting segment is bonded and fixed on the splicing surfaces of the first and second segments.
Further, the connecting segment is in form of a trapezoidal structure whose outer side is spliced with the outer skin of the first and second segments, and its inner side is spliced with an inner skin.
Further, the connecting segment is in form of a triangular structure whose outer surface is spliced with the outer skin of the first and second segments.
Further, a butting surface including a horizontal portion and a vertical portion is provided between the two splicing surfaces, wherein the horizontal portion is bonded and fixed to the connecting segment, and the vertical portions of the first and second segments abut each other and are bonded and fixed with a structural adhesive layer.
Further, the outer skin of the splicing surface on the first and second segments extends horizontally near one end of the inner skin and fits with the inner skin to form a horizontal butting portion, and the horizontal butting portions of the first and second segments abut each other to form a horizontal portion for fixing the connecting segment.
Further, the first and second segments adopt fiberglass butt joint or core material butt joint at the interface.
The advantageous effect of the present invention is that 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 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 of the first and second segments, and ensures bonding reliability of the first and second segments. In addition, the biaxial reinforcing layer at the skin interface of the splicing surface ensures the uniformity of the force on the blade shell structure, thereby improving the stability of the overall structure of the blade.
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.
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.
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.
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.
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.
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.
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.
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.
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.
As shown in
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.
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.
As shown in
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.
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.
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.
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
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.
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.
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
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.
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.
| Number | Date | Country | Kind |
|---|---|---|---|
| 202111328543.2 | Nov 2021 | CN | national |
| Number | Date | Country | |
|---|---|---|---|
| Parent | PCT/CN2022/114464 | Aug 2022 | US |
| Child | 18225524 | US |
