Trailing edge bonding cap for wind turbine rotor blades
A trailing edge bonding cap for use with a rotor blade of a wind turbine is disclosed. The trailing edge bonding cap may include a body projecting outwardly from a blade shell of the rotor blade. The body may have a first outer surface and a second outer surface. The first outer surface may intersect the second outer surface to define a trailing edge of the rotor blade. Additionally, the first and second outer surfaces may have a profile configured to correspond to an aerodynamic profile of the blade shell.
1. A trailing edge bonding cap for use with a rotor blade of a wind turbine, the trailing edge bonding cap comprising:
a body configured to project outwardly from a blade shell of the rotor blade, said body being formed from a metal matrix composite material and having a first outer surface and a second outer surface, said first outer surface configured to intersect said second outer surface to define a trailing edge of the rotor blade,
wherein said first and second outer surfaces have a profile configured to correspond to an aerodynamic profile of said blade shell and wherein said body is segmented along a length of the trailing edge bonding cap.
2. The trailing edge bonding cap of claim 1 , wherein said metal matrix composite material comprises an aluminum alloy matrix reinforced with carbon or boron fibers.
3. The trailing edge bonding cap of claim 1 , wherein said metal matrix composite material comprises an electrically conductive metal.
4. The trailing edge bonding cap of claim 1 , wherein said body has a hollow cross-section.
5. The trailing edge bonding cap of claim 1 , wherein said body comprises at least one bonding surface configured to be secured to said blade shell.
6. The trailing edge bonding cap of claim 5 , wherein said at least one bonding surface comprises a first bonding surface and a second bonding surface, said first and second bonding surfaces configured to extend within the rotor blade and engage trailing ends of said blade shell.
7. The trailing edge bonding cap of claim 6 , wherein said first and second bonding surfaces are concavely shaped.
8. The trailing edge bonding cap of claim 1 , wherein the profile of said first outer surface is configured to correspond to the aerodynamic profile of a first shell component of said blade shell and the profile of said second outer surface is configured to correspond to the aerodynamic profile of a second shell component of said blade shell.
9. The trailing edge bonding cap of claim 1 , wherein the intersection of said first and second outer surfaces defines a sharp trailing edge.
10. A rotor blade for a wind turbine, the rotor blade comprising:
a root portion;
a blade tip;
a blade shell extending between said root portion and said blade tip, said blade shell having an aerodynamic profile and comprising a first shell component and a second shell component; and,
a trailing edge bonding cap partially disposed between trailing ends of said first and second shell components, said trailing edge bonding cap being formed from a metal matrix composite material and having a first outer surface and a second outer surface, said first outer surface intersecting said second outer surface to define a trailing edge of the rotor blade,
wherein said first and second outer surfaces have a profile configured to correspond to the aerodynamic profile of said blade shell and wherein said trailing edge bonding cap is segmented along a length of the rotor blade.
11. The rotor blade of claim 10 , wherein said metal matrix composite material comprises an aluminum alloy matrix reinforced with carbon or boron fibers.
12. The trailing edge bonding cap of claim 10 , wherein said metal matrix composite material comprises an electrically conductive metal.
13. The rotor blade of claim 10 , wherein said trailing edge bonding cap has a hollow cross-section.
14. The rotor blade of claim 10 , wherein said trailing edge bonding cap comprises at least one bonding surface secured to said blade shell.
15. The rotor blade of claim 14 , wherein said at least one bonding surface comprises a first bonding surface and a second bonding surface, said first and second bonding surfaces extending within the rotor blade and engaging said trailing ends of said first and second shell components.
16. The rotor blade of claim 15 , wherein said first and second bonding surfaces are concavely shaped.
17. The rotor blade of claim 10 , wherein the profile of said first outer surface is configured to correspond to the aerodynamic profile of said first shell component, the profile of said second outer surface being configured to correspond to the aerodynamic profile of said second shell component.
18. The rotor blade of claim 10 , wherein the intersection of the first and second outer surfaces defines a sharp trailing edge.
19. The rotor blade of claim 10 , wherein a ratio of a chord length of the trailing edge bonding cap to a chord length of the rotor blade is about 1:20.