Segmented rotor blade for a wind turbine and methods for joining the same
A segmented rotor blade for a wind turbine. The segmented rotor blade including at least a first blade segment and a second blade segment extending in opposite directions from a joint. Each of the first and second blade segments including at least one shell member defining an airfoil surface. A joint assembly coupling the first blade segment to the second blade segment via a dovetail connection at the joint. The joint assembly including at least one receiving section defining a receiving cavity, a joining structure received within the at least one receiving section to establish a dovetail connection, and a securement assembly securing the joining structure within the at least one receiving section so as to secure the dovetail connection.
1 . A segmented rotor blade for a wind turbine, comprising:
at least a first blade segment and a second blade segment extending in opposite directions from a joint, each of the first and second blade segments comprising at least one shell member defining an airfoil surface; and
a joint assembly coupling the first blade segment to the second blade segment via a dovetail connection at the joint, the joint assembly comprising:
at least one receiving section defining a receiving cavity having a receiving profile,
a joining structure received within the at least one receiving section, the joining structure defining a joining profile corresponding to the receiving profile, the joining profile and the receiving profile forming a dovetail profile, wherein the joining structure and the at least one receiving section form the dovetail connection, wherein the at least one receiving section and the joining structure extend along an arc defined between a leading edge and a trailing edge of the segmented rotor blade, and
a securement assembly securing the joining structure within the at least one receiving section so as to secure the dovetail connection.
2 . The segmented rotor blade of claim 1 , wherein the at least one receiving section and the joining structure extend along a plane defined in a chordwise direction.
3 . The segmented rotor blade of claim 1 , wherein the joint has a deviation from a chordwise axis of less than or equal to 45-degrees.
4 . The segmented rotor blade of claim 1 , wherein the joining structure further comprises at least one end having a contour corresponding to a portion of a contour of the airfoil surface.
5 . The segmented rotor blade of claim 1 , wherein the joint assembly further comprises:
at least one spacer element contained within the at least one receiving section, the at least one spacer element having a spacer profile corresponding to at least a portion of the receiving cavity.
6 . The segmented rotor blade of claim 1 , wherein the securement assembly comprises at least one pre-tensioned bolt positioned within the joint assembly, the at least one pre-tensioned bolt oriented to exert a clamping force on the at least one receiving section so as to maintain contact between the joining structure and the at least one receiving section.
7 . The segmented rotor blade of claim 1 , wherein the securement assembly comprises a thermoplastic resin positioned between opposing bearing surfaces of the joining structure and the at least one receiving section.
8 . The segmented rotor blade of claim 1 , wherein the at least one receiving section is formed integrally with the first blade segment and wherein the joining structure is formed integrally with the second blade segment.
9 . The segmented rotor blade of claim 1 , wherein the at least one receiving section is a first receiving section formed integrally with the first blade segment, the segmented rotor blade further comprising:
a second receiving section formed integrally with the second blade segment, wherein the joining structure is encapsulated by the first and second receiving sections so as to establish the dovetail connection along the joint.
10 . The segmented rotor blade of claim 1 , wherein the at least one receiving section is a first plurality of receiving sections distributed along a chord of the segmented rotor blade at a first thickness location, wherein the joining structure is a first plurality of joining structures received within the first plurality of receiving sections at the first thickness location, the joint assembly further comprising:
a second plurality of receiving sections distributed along the chord at a second thickness location, each receiving section of the first and second plurality of receiving sections defining a receiving cavity having a receiving profile;
a second plurality of joining structures received within the second plurality of receiving sections at the second thickness location, each joining structure of the first and second plurality of joining structures defining a joining profile corresponding to the receiving profile of the corresponding receiving section, the joining profiles and the corresponding receiving profiles forming a plurality of dovetail profiles, wherein the first and second pluralities of joining structures and the first and second pluralities of receiving sections form a plurality of dovetail connections.
11 . A method for joining first and second blade segments of a rotor blade of a wind turbine, the first blade segment having at least one receiving section defining a receiving cavity having a receiving profile, the second blade segment having a joining structure defining a joining profile, the receiving and joining profiles having corresponding interlocking geometries, the method comprising:
placing the first and second blade segments in opposite directions from a joint;
engaging the corresponding interlocking geometries of the joining structure and the receiving section so as to form a joint assembly having a dovetail connection, wherein engaging the corresponding interlocking geometries of the joining structure and the receiving section further comprises applying a rotational force to the joining structure so as to move the joining structure along an arc defined by the at least one receiving section; and
securing the joining structure and the receiving section together via a securement assembly.
12 . The method of claim 11 , wherein the joint has a deviation from a chordwise axis of less than or equal to 45-degrees.
13 . The method of claim 11 , further comprising:
inserting at least one spacer element into the at least one receiving section, the at least one spacer element having a cross-sectional spacer profile corresponding to the cross-section of the receiving cavity and/or a portion of airfoil surface.
14 . The method of claim 11 , wherein securing the joining structure and the receiving section further comprises:
inserting at least one pre-tensioned bolt into a recess defined by the at least one receiving section; and
applying a torque to the pre-tensioned bolt so as to apply a clamping pressure onto the joining structure.
15 . The method of claim 11 , wherein securing the joining structure and the receiving section further comprises:
applying a thermoplastic resin to at least one of the joining structure or the at least one receiving section;
applying a clamping pressure to the at least one receiving section; and
curing the thermoplastic resin.
16 . The method of claim 11 , wherein the second blade segment further comprises at least one receiving section, the method further comprising:
aligning the first and second blade segments spanwise along a pitch axis, wherein engaging the corresponding interlocking geometries comprises inserting the joining structure into the receiving sections of the first and second blade segments so as to establish the dovetail connection.
17 . A wind turbine, comprising:
a tower secured atop a foundation;
a nacelle mounted atop the tower; and
a rotor mounted to the nacelle, the rotor comprising a rotatable hub having at least one segmented rotor blade coupled thereto, the at least one segmented rotor blade comprising:
at least a first blade segment and a second blade segment extending in opposite directions from a joint, each of the first and second blade segments comprising at least one shell member defining an airfoil surface, and
a joint assembly coupling the first blade segment to the second blade segment via a dovetail connection at the joint, the joint assembly comprising:
at least one receiving section defining a receiving cavity having a receiving profile,
a joining structure received within the at least one receiving section, the joining structure defining a joining profile corresponding to the receiving profile, the joining profile and the receiving profile forming a dovetail profile, wherein the joining structure and the at least one receiving cavity form the dovetail connection, wherein the at least one receiving section and the joining structure extend along an arc defined between a leading edge and a trailing edge of the segmented rotor blade, and
a securement assembly securing the joining structure within the at least one receiving section so as to secure the dovetail connection.