Rotor blade for a wind turbine and methods of manufacturing the same
In one aspect, a method for manufacturing a rotor blade for a wind turbine is disclosed. The method may generally include assembling a blade blank comprising a shear member and a volume of core material and removing material from the blade blank to form a body having a pressure side and a suction side extending between a leading edge and a trailing edge. The shear member may have a first end disposed adjacent to the pressure side and a second end disposed adjacent to the suction side. In addition, the method may include positioning a skin around an outer perimeter of the body.
1. A method for manufacturing a rotor blade for a wind turbine, the method comprising:
assembling a blade blank comprising a shear member and a volume of core material;
removing material from the blade blank to form a body having a pressure side and a suction side extending between a leading edge and a trailing edge, the shear member having a first end disposed adjacent to the pressure side and a second end disposed adjacent to the suction side;
positioning a stiffening member adjacent to at least one of the first end or the second end of the shear member; and
positioning a skin around an outer perimeter of the body.
2. The method of claim 1 , wherein removing material from the blade blank to form a body comprises removing material from at least one of the shear member or the core material to form the body.
3. The method of claim 1 , wherein positioning a stiffening member adjacent to at least one of the first end or the second end of the shear member comprises positioning a first stiffening member at the first end of the shear member and a second stiffening member at the second end of the shear member.
4. The method of claim 3 , further comprising forming a first channel at the first end of the shear member and a second channel at the second end of the shear member.
5. The method of claim 4 , wherein positioning a first stiffening member at the first end of the shear member and a second stiffening member at the second end of the shear member positioning the first stiffening member within the first channel and the second stiffening member within the second channel.
6. The method of claim 5 , wherein positioning the first stiffening member within the first channel and the second stiffening member within the second channel comprises forming the first stiffening member within the first channel and the second stiffening member within the second channel.
7. The method of claim 6 , wherein the first and second stiffening members are formed within the first and second channels by curing a composite material installed within the first and second channels.
8. The method of claim 6 , wherein the first and second stiffening members are formed within the first and second channels by using a wet lay-up process.
9. The method of claim 4 , wherein forming a first channel at the first end of the shear member and a second channel at the second end of the shear member comprises forming the first and second channels while the material is being removed from the blade blank to form the body.
10. The method of claim 4 , wherein forming a first channel at the first end of the shear member and a second channel at the second end of the shear member comprises removing additional material from the blade blank after the body has been formed in order to form the first and second channels.
11. The method of claim 1 , further comprising positioning an edge stiffening member at or adjacent to the trailing edge.
12. The method of claim 1 , wherein assembling a blade blank comprising a shear member and a volume of core material comprises assembling the shear member between two core material segments to form the blade blank.
13. A method for manufacturing a rotor blade for a wind turbine, the method comprising:
assembling a blade blank comprising a shear member and a volume of core material;
removing material from the blade blank to form a body having a pressure side and a suction side extending between a leading edge and a trailing edge, the shear member having a first end disposed adjacent to the pressure side and a second end disposed adjacent to the suction side;
forming a first channel at the first end of the shear member and a second channel at the second end of the shear member;
positioning a first stiffening member within the first channel and a second stiffening member within the second channel; and,
positioning a skin around an outer perimeter of the body.
14. The method of claim 13 , wherein positioning the first stiffening member within the first channel and the second stiffening member within the second channel comprises forming the first stiffening member within the first channel and forming the second stiffening member within the second channel.
15. The method of claim 14 , wherein the first and second stiffening members are formed within the first and second channels by curing a composite material installed within the first and second channels.
16. The method of claim 14 , wherein the first and second stiffening members are formed within the first and second channels by using a wet lay-up process.
17. The method of claim 13 , wherein forming a first channel at the first end of the shear member and a second channel at the second end of the shear member comprises forming the first and second channels while the material is being removed from the blade blank to form the body.
18. The method of claim 13 , wherein forming a first channel at the first end of the shear member and a second channel at the second end of the shear member comprises removing additional material from the blade blank after the body has been formed to form the first and second channels.