Rotor blades having thermoplastic components and methods for joining rotor blade components
Rotor blades and methods for joining blade components of rotor blades are provided. A method includes positioning an insert between and in contact with a first blade component and a second blade component. At least one of the first blade component or the second blade component includes a thermoplastic resin. The insert includes a thermoplastic resin and an energy absorptive pigment. The method further includes heating the thermoplastic resin of the at least one of the first blade component or the second blade component and the thermoplastic resin of the insert. The method further includes cooling the thermoplastic resin of the at least one of the first blade component or the second blade component and the thermoplastic resin of the insert. The heating step and the cooling step join the first blade component, the second blade component and the insert together.
1. A method for joining blade components of a wind turbine rotor blade, the method comprising:
positioning an insert between and in contact with a first blade component and a second blade component, at least one of the first blade component or the second blade component comprising a thermoset and a localized portion of a thermoplastic resin, the insert comprising a thermoplastic resin and an energy absorptive pigment;
applying a compressive force to the first blade component, the second blade component, and the insert;
heating the thermoplastic resin of the at least one of the first blade component or the second blade component and the thermoplastic resin of the insert; and
cooling the thermoplastic resin of the at least one of the first blade component or the second blade component and the thermoplastic resin of the insert,
wherein the heating step and the cooling step join the first blade component, the second blade component and the insert together.
2. The method of claim 1 , wherein the first blade component and the second blade component each comprise a thermoset and a localized portion of a thermoplastic resin.
3. The method of claim 1 , wherein the localized portion of the thermoplastic resin of the at least one of the first blade component or the second blade component comprises a plurality of fibers embedded in the thermoplastic resin.
4. The method of claim 1 , wherein the insert comprises a fiber reinforced thermoplastic composite, the composite comprising the thermoplastic resin, the energy absorptive pigment and a plurality of fibers embedded in the thermoplastic resin.
5. The method of claim 1 , wherein the energy absorptive pigment is carbon black.
6. The method of claim 1 , wherein the compressive force is applied to the first blade component, the second blade component, and the insert by a clamping mechanism.
7. The method of claim 1 , wherein the first blade component and the second blade component are free from energy absorptive pigment.
8. The method of claim 1 , wherein the heating step is performed by laser welding.
9. The method of claim 1 , wherein the first blade component is a first outer blade segment and the second blade component is a second outer blade segment.
10. The method of claim 1 , wherein the first blade component is a sparcap and the second blade component is an outer blade segment.
11. The method of claim 1 , wherein the first blade component is a shear web and the second blade component is a sparcap.
12. A rotor blade for a wind turbine, the rotor blade comprising:
a first blade component and a second blade component, at least one of the first blade component or the second blade component comprising a thermoset and a localized portion of a thermoplastic resin; and
an insert between and in contact with the first blade component and the second blade component, the insert comprising a thermoplastic resin and an energy absorptive pigment,
the first blade component, the second blade component and the insert joined together by a welded interface between the insert and the first blade component and a welded interface between the insert and the second blade component.
13. The rotor blade of claim 12 , wherein the welded interfaces are laser welded interfaces.
14. The rotor blade of claim 12 , wherein the localized portion of the thermoplastic resin of the at least one of the first blade component or the second blade component comprises a plurality of fibers embedded in the thermoplastic resin.
15. The rotor blade of claim 12 , wherein the insert comprises a fiber reinforced thermoplastic composite, the composite comprising the thermoplastic resin, the energy absorptive pigment and a plurality of fibers embedded in the thermoplastic resin.
16. The rotor blade of claim 12 , wherein the first blade component is a first outer blade segment and the second blade component is a second outer blade segment.
17. The rotor blade of claim 12 , wherein the first blade component is a sparcap and the second blade component is an outer blade segment.
18. The rotor blade of claim 12 , wherein the first blade component is a shear web and the second blade component is a sparcap.