Spar cap for a wind turbine rotor blade formed from pre-cured laminate plates of varying thicknesses
A spar cap for a rotor blade of a wind turbine may generally include an assembly of pre-cured laminate plates stacked on one top of the other, with the assembly including an outermost pre-cured plate, an innermost pre-cured plate positioned opposite the outermost pre-cured plate and a plurality of intermediate pre-cured plates stacked directly between the outermost and innermost pre-cured plates. The outermost pre-cured plate may be configured to be positioned adjacent to an inner surface of a body shell of the rotor blade. In addition, the outermost pre-cured plate may define a plate thickness that differs from a plate thickness defined by the innermost pre-cured plate by at least 50%.
1. A spar cap for a rotor blade of a wind turbine, the rotor blade including a blade root, a blade tip and a body shell extending between the blade root and the blade tip, the spar cap comprising:
an assembly of pre-cured laminate plates stacked one on top of the other, the assembly of pre-cured laminate plates including an outermost pre-cured plate, an innermost pre-cured plate positioned opposite the outermost pre-cured plate and a plurality of intermediate pre-cured plates stacked directly between the outermost and innermost pre-cured plates, the outermost pre-cured plate configured to be positioned adjacent to an inner surface of the body shell,
wherein the outermost pre-cured plate defines a plate thickness that differs from a plate thickness defined by the innermost pre-cured plate by at least 50%, and
wherein the plurality of intermediate pre-cured plates are arranged such that a plate thickness of the plurality of intermediate pre-cured plates continuously decreases or continuously increases between adjacent pre-cured plates of the plurality of intermediate pre-cured plates as the spar cap extends between the outermost pre-cured plate and the innermost pre-cured plate.
2. The spar cap of claim 1 , wherein the plate thickness of the outermost pre-cured plate corresponds to a maximum plate thickness for the spar cap and the plate thickness of the innermost pre-cured plate corresponds to a minimum plate thickness for the spar cap.
3. The spar cap of claim 1 , wherein the plate thickness of the outermost pre-cured plate corresponds to a minimum plate thickness for the spar cap and the plate thickness of the innermost pre-cured plate corresponds to a maximum plate thickness for the spar cap.
4. The spar cap of claim 1 , wherein each of the plurality of pre-cured laminate plates corresponds to a pultruded plate.
5. A spar cap for a rotor blade of a wind turbine, the rotor blade including a blade root, a blade tip and a body shell extending between the blade root and the blade tip, the spar cap comprising:
an assembly of pre-cured laminate plates stacked one on top of the other, the assembly of pre-cured laminate plates including an outermost pre-cured plate, an innermost pre-cured plate positioned opposite the outermost pre-cured plate and a plurality of intermediate pre-cured plates stacked directly between the outermost and innermost pre-cured plates, the outermost pre-cured plate configured to be positioned adjacent to an inner surface of the body shell,
wherein the outermost pre-cured plate defines a plate thickness corresponding to one of a maximum plate thickness or a minimum plate thickness for the spar cap and the innermost pre-cured plate defines a plate thickness corresponding to the other of the maximum plate thickness or the minimum plate thickness for the spar cap, and
wherein the plurality of intermediate pre-cured plates are arranged such that a plate thickness of the plurality of intermediate pre-cured plates continuously decreases or continuously increases between adjacent pre-cured plates of the plurality of intermediate pre-cured plates as the spar cap extends between the outermost pre-cured plate and the innermost pre-cured plate.
6. The spar cap of claim 5 , wherein the plate thickness of the outermost pre-cured plate corresponds to the maximum plate thickness and the plate thickness of the innermost pre-cured plate corresponds to the minimum plate thickness.
7. The spar cap of claim 6 , wherein the plate thickness of the plurality of intermediate pre-cured plates is continuously decreased as the spar cap extends between the outermost pre-cured plate and the innermost pre-cured plate.
8. The spar cap of claim 5 , wherein the plate thickness of the outermost pre-cured plate corresponds to the minimum plate thickness and the plate thickness of the innermost pre-cured plate corresponds to the maximum plate thickness.
9. The spar cap of claim 8 , wherein the plate thickness of the plurality of intermediate pre-cured plates is continuously increased as the spar cap extends between the outermost pre-cured plate and the innermost pre-cured plate.
10. The spar cap of claim 5 , wherein the minimum plate thickness is equal to less than about 50% of the maximum plate thickness.
11. The spar cap of claim 10 , wherein the minimum plate thickness is equal to less than about 20% of the maximum plate thickness.
12. The spar cap of claim 5 , wherein each of the plurality of pre-cured laminate plates corresponds to a pultruded plate.
13. A spar cap for a rotor blade of a wind turbine, the rotor blade including a blade root, a blade tip and a body shell extending between the blade root and the blade tip, the spar cap comprising:
an assembly of pre-cured laminate plates, the assembly of pre-cured laminate plates including a plurality of first pre-cured laminate plates stacked one on top of the other along an inboard region of the spar cap and a plurality of second pre-cured laminate plates stacked one on top of the other along an outboard region of the spar cap,
wherein the plurality of first and second pre-cured laminate plates are inter-leafed such that an overlapped region is defined between each second pre-cured laminate plate and each pair of adjacent first pre-cured laminate plates along a spanwise direction of the spar cap, and
wherein, at least in the overlapped region, a plate thickness of the plurality of first pre-cured laminate plates is greater than a plate thickness of the plurality of second pre-cured laminate plates.
14. The spar cap of claim 13 , wherein the spar cap transitions from the inboard region to the outboard region at a spanwise location ranging from about 40% to about 60% of a span of the rotor blade.
15. The spar cap of claim 13 , wherein at least one of the plurality of first pre-cured laminate plates define a plate thickness corresponding to a maximum plate thickness for the spar cap and wherein at least one of the plurality of second pre-cured laminate plates define a plate thickness corresponding to a minimum plate thickness for the spar cap.