Rotor blades having structural skin insert and methods of making same
The present disclosure is directed to a method of manufacturing a rotor blade for a wind turbine. The method includes providing a blade mold of the rotor blade. Another step includes placing an outer skin layer in the blade mold. The method also includes placing one or more structural inserts in the blade mold atop the outer skin layer as a function of a load of the rotor blade. Further, each of the structural inserts includes a plurality of cells arranged in a predetermined pattern. Further, the cells have varying cell sizes. The method also includes placing an inner skin layer atop the one or more structural inserts and securing the outer skin layer, the one or more structural inserts, and the inner skin layer together to form the rotor blade.
1. A method of manufacturing a rotor blade for a wind turbine, the method comprising:
providing a blade mold of the rotor blade;
placing an outer skin layer in the blade mold;
placing a structural panel in the blade mold atop the outer skin layer, the structural panel comprising a plurality of cells arranged in a predetermined pattern, the plurality of cells comprising varying cell sizes within the structural panel when the structural panel is placed in the blade mold;
placing an inner skin layer atop the structural panel; and,
securing the structural panel between the outer and inner skin layers so as to form the rotor blade.
2. The method of claim 1 , further comprising filling the plurality of cells with a filler material, wherein the filler material comprises a low-density foam material.
3. The method of claim 1 , wherein the outer and inner skin layers comprise at least one of a dry fabric or a pre-preg material.
4. The method of claim 1 , wherein the predetermined pattern comprises at least one of a dragon fly pattern, a hexagonal pattern, a square pattern, a rectangular pattern, a flex core pattern, or a random pattern.
5. The method of claim 1 , further comprising forming structural panel via three-dimensional (3D) printing.
6. The method of claim 1 , wherein the structural panel is constructed of at least one of a glass fiber reinforced polymer (GFRP), a thermoset material, a thermoplastic material, or a metal.
7. The method of claim 1 , further comprising placing a plurality of structural panels in the blade mold atop the outer skin layer, each of the plurality of structural panels comprising a different predetermined pattern.
8. The method of claim 7 , wherein the plurality of cells of at least one of the plurality of structural panels is larger than the plurality of cells of another structural panel.
9. The method of claim 7 , wherein at least one of the plurality of structural panels comprises a varying thickness along a length thereof.
10. The method of claim 1 , further comprising placing a plurality of structural panels in the blade mold atop the outer skin layer, each of the plurality of structural panels comprises matching predetermined patterns.
11. The method of claim 1 , further comprising placing a plurality of structural panels in the blade mold atop the outer skin layer, the plurality of structural panels comprising a combination of different and matching predetermined patterns.
12. The method of claim 1 , wherein securing the structural panel between the outer and inner skin layers further comprises at least one of infusing the structural panel between the outer and inner skin layers via vacuum infusion, heat curing the structural panel between the outer and inner skin layers, or mechanically fastening the structural panel between the outer and inner skin layers.
13. A method of manufacturing a rotor blade for a wind turbine, the method comprising:
providing a blade mold of the rotor blade;
placing at least one skin layer in the blade mold;
placing a structural panel in the blade mold adjacent to the skin layer, the structural panel comprising a plurality of cells arranged in a predetermined pattern, the plurality of cells comprising varying cell sizes within the structural panel when the structural panel is placed in the blade mold; and,
securing the skin layer and the structural panel together to form the rotor blade.
14. The method of claim 13 , wherein securing the skin layer and the structural panel together to form the rotor blade further comprises at least one of infusing the structural panel to the skin layer via vacuum infusion, heat curing the structural panel to the skin layer, or mechanically fastening the structural panel to the skin layer.