A METHOD OF MANUFACTURING A SHELL OF A WIND TURBINE BLADE

Abstract

A method of manufacturing a shell of a wind turbine blade is disclosed. The method of manufacturing includes laying one or more layers of fiber on a surface of mould to form the shell. A spar element is positioned at a pre-defined position on the one or more layers of fiber, and a vacuum bag is positioned or covered around the one or more layers of fiber and the spar element. The method further includes step of infusion of resin through the one or more layers of fiber and the spar element. The resin is subsequently allowed to cure to obtain the shell of the wind turbine blade. The spar element is thus adhered to the shell through resin infusion process.

Claims

1. A method of manufacturing a shell of a wind turbine blade (28), the method comprising: laying one or more shell or spar fibers, on a surface of mould to form at least a portion of the blade shell; positioning a spar element (60a) at pre-defined position on the one or more layers of fiber; covering a vacuum bag (100) over the one or more layers of fiber and the spar element (60a) to seal the spar element (60a) and the one or more layers of fibers; and infusing resin through the one or more layers of fiber and the spar element (60a) and subsequently curing the same to obtain the shell (32a or 32b), wherein the spar element (60a) adheres to the shell (32a or 32b) upon curing the infused resin.

2. A method for joining a spar element to a wind turbine blade (28), the method comprises: positioning the spar element (60a) on a shell (32a or 32b) or spar cap of the wind turbine blade (28), wherein a portion of the spar element (60a) in contact with the shell or spar cap is defined with a flow path; and infusing resin between the spar element (60a) and the shell (32a or 32b) or the spar cap through the flow path and subsequently curing the same to adhere the spar element (60a) to the shell (32a or 32b) or spar cap of the wind turbine blade (10).

3. The method according to claim 1, wherein the spar element (60a) is a spar beam receiver section or a portion of receiver section.

4. The method according to claim 1, wherein the resin includes a polyester compound, preferably at least one of a vinyl ester or epoxy resins.

5. The method according to claim 1, wherein the one or more layers of fibers on the mould are glass fibers and the one or more layers of fibers are in form of at least one of fabrics, prefabricated structure or loose fibers.

6. The method according to claim 1 comprises positioning a shear web (102) at a substantially central portion of the shell (30 and 32), wherein the shear web (102) extends along length of the shell and up-to the spar element (60a).

7. The method according to claim 1, wherein an end of the spar element (60a) is connected to the shear web (102).

8. The method according to claim 1 comprises joining the end of spar element (60a) and the shear web (102) by resin infusion process.

9. A method for manufacturing a root end segment (32) of the wind turbine blade (10), the method comprising: forming a first shell half structure (32a) and a second shell half structure (32b) separately in a mould; joining a spar element (60a) to at least one of the first shell half structure (32a) and the second shell half structure (32b) by resin infusion process in the mould; positioning a shear web (102) at a substantially central portion of the first shell half structure (32a) and the second shell half structure (32b), wherein the shear web (102) extends in a spanwise direction up-to the spar element (60a); joining an end of the spar element (60a) and the shear web (102) by resin infusion process; and joining and sealing the first shell half structure (32a) and a second shell half structure (32b) to obtain the root end segment (32) of the wind turbine blade (10).

10. The method as claimed in claim 9, wherein a first half of the spar element (60a) is bonded to the first shell half structure (32a) and a second half of the spar element (60a) is bonded to the second shell half structure (32b).

11. The method according to claim 9 comprises adhering the first half of the spar element (60a) to the second half of the spar element (60a) before joining of the first shell half structure (32a) and the second shell half structure (32b).

12. The method according to claim 9, wherein the spar element (60a) is defined with an extending portion on an end opposite to receiving section (60), the extending portion is configured to connect to the shear web (102).

13. The method according to claim 9, wherein the first shell half structure (32a) and the second shell half structure (32b) are formed by laying plurality of layers of fiber in the mould, infusing resin and subsequently curing the resin.

14. The method according to claim 9, wherein the resin includes a polyester compound, preferably at least one of a vinyl ester or epoxy resins and/or or more layers of fibers on the mould are glass fibers.

15. A wind turbine blade (10) comprising a shell and a spar element (60a) adhered to the shell through the resin infusion process as claimed in claim 1.

Description

DESCRIPTION OF THE INVENTION

[0024] The invention is explained in detail below with reference to an embodiment shown in the drawings, in which

[0025] FIG. 1 illustrates a perspective view of one embodiment of a wind turbine,

[0026] FIG. 2 illustrates a perspective view of a wind turbine blade, in accordance with an embodiment of the disclosure,

[0027] FIG. 3 illustrates a plan view of one embodiment of a rotor blade having a first blade segment and a second blade segment,

[0028] FIG. 4 illustrates a perspective view of a section of one embodiment of tip end of the blade,

[0029] FIG. 5 illustrates a perspective view of one embodiment of a section of the root end of the blade at the chord-wise joint,

[0030] FIG. 6 illustrates an assembly of one embodiment of the rotor blade of the wind turbine having a tip end joined to with the root end segment,

[0031] FIG. 7 illustrate an exploded perspective view of one embodiment of the multiple supporting structures of the assembly of the rotor blade of the wind turbine;

[0032] FIGS. 8a-d illustrates different cross-sections of the receiving section of the spar element;

[0033] FIGS. 9 and 10 illustrates step-by-step method of joining a spar element to the shell of the wind turbine blade by resin infusion process;

[0034] FIG. 11a illustrates a perspective view of a mould used to manufacture the shell of the wind turbine blade by resin infusion process, in accordance with an embodiment of the disclosure,

[0035] FIGS. 11b and 11c is a flowchart of the method of manufacturing a wind turbine blade, in accordance with an embodiment of the present disclosure

[0036] FIG. 12 illustrates schematic view of the spar element connected to the shear web of the wind turbine blade by resin infusion process; and

[0037] FIGS. 13 and 14 illustrates various configurations for connecting the spar element to the shear web by resin infusion process.

DETAILED DESCRIPTION

[0038] Reference now will be made in detail to embodiments of the invention, one or more examples of which are illustrated in the drawings. Each example is provided by way of explanation of the invention, not limitation of the invention. In fact, will be apparent to those skilled in the art that various modifications and variations can be made in the present invention without departing from the scope or spirit if the invention. For instance, features illustrated or described as part of one embodiment can be used with another embodiment to yield a still further embodiment. Thus, it is intended that the present invention covers such modifications and variations as come within the scope of the appended claims and their equivalents.

[0039] Referring now to the drawings, FIG. 1 illustrates a perspective view of one embodiment of a wind turbine 10 according to the present invention. In the illustrated embodiment, the wind turbine 10 is a horizontal-axis wind turbine. Alternatively, the wind turbine 10 may be a vertical-axis wind turbine. In addition, as shown, the wind turbine 10 may include a tower 12 that extends from a support surface 14, a nacelle 16 mounted on the tower 12, a generator 18 positioned within the nacelle 16, a gearbox 20 coupled to the generator 18, and a rotor 22 that is rotationally coupled to the gearbox 20 with a rotor shaft 24. Further, as shown, the rotor 22 includes a rotatable hub 26 and at least one rotor blade 28 coupled to and extending outward from the rotatable hub 26. As shown, the rotor blade 28 includes a blade tip 17 and a blade root 19.

[0040] FIG. 2 shows a schematic view of a rotor blade 28. The rotor blade 28 has the shape of a conventional wind turbine blade and comprises a root region 19 closest to the hub, a profiled or an airfoil region 34 farthest away from the hub and a transition region 32d between the root region 19 and the airfoil region 32c. The blade 28 comprises a leading edge facing the direction of rotation of the blade 28, when the blade 28 is mounted on the hub, and a trailing edge facing the opposite direction of the leading edge.

[0041] The airfoil region 32c (also called the profiled region) has an ideal or almost ideal blade shape with respect to generating lift, whereas the root region 19 due to structural considerations has a substantially circular or elliptical cross-section, which for instance makes it easier and safer to mount the blade 28 to the hub. The diameter (or the chord) of the root region 19 may be constant along the entire root area. The transition region 32d has a transitional profile gradually changing from the circular or elliptical shape of the root region 19 to the airfoil profile of the airfoil region. The chord length of the transition region 32d typically increases with increasing distance r from the hub. The airfoil region has an airfoil profile with a chord extending between the leading edge and the trailing edge of the blade 28. The width of the chord decreases with increasing distance r from the hub.

[0042] A shoulder 32e of the blade 28 is defined as the position, where the blade 28 has its largest chord length. The shoulder is typically provided at the boundary between the transition region 32d and the airfoil region. FIG. 2 also illustrates the longitudinal extent L, length or longitudinal axis of the blade.

[0043] It should be noted that the chords of different sections of the blade normally do not lie in a common plane, since the blade may be twisted and/or curved (i.e. pre-bent), thus providing the chord plane with a correspondingly twisted and/or curved course, this being most often the case in order to compensate for the local velocity of the blade being dependent on the radius from the hub.

[0044] The blade is typically made from a first shell half structure and a second shell half structure that are glued to each other along bond lines at the leading edge and the trailing edge of the blade 28.

[0045] Referring now to FIG. 3, a schematic view of a cross section of one of the rotor blades 28 of FIG. 1 is illustrated. In an embodiment, the rotor blade 28 may hereinafter alternatively be referred as blade. As shown, the rotor blade 28 may include a tip end segment 30 and a root end segment 32. Further, as shown, the tip end segment 30 of the blade 28 and the root end segment 32 of the blade 28 may each extend in opposite directions from a chordwise joint 34. In addition, as shown, each of the blade segments 30, 32 may include at least one shell member defining an airfoil surface, such as a first shell half structure and a second shell half structure. The tip end segment 30 and the root end segment 32 are connected by at least an internal support structure 36 to facilitate joining of the tip end segment 30 and root end segment 32. The arrow 38 shows that the segmented rotor blade 28 in the illustrated example includes the tip end segment 30 and the root end segment 32 and are joined by inserting the internal support structure 36 into the root end segment 32. In addition, as shown, the root end segment includes multiple spar structures 66 (also referred to herein as spar caps) that extend lengthwise for connecting with the beam structure 40 of the tip end segment 30 (which is shown in more detail in FIGS. 3 and 5).

[0046] Referring now to FIG. 4, a perspective view of a section of the tip end segment 30 according to the present invention is illustrated. As shown, the tip end segment 30 includes a beam structure 40 that forms a portion of the internal support structure 36 and extends lengthwise for structurally connecting with the root end segment 32. Further, as shown, the beam structure 40 forms at least a part of a shear web 42 (i.e. shear web on the tip end segment of the blade) connected with a suction side spar cap 44 and a pressure side spar cap 46. Moreover, as shown, the tip end segment 30 may include one or more first pin joints at a receiving end 54 of the beam structure 40. In one embodiment, the pin joint may include a pin that is in a tight interference fit with a bushing. More specifically, as shown, the pin joint(s) may include at least one pin tube 52 located on the receiving end 54 of the beam structure 40. Thus, as shown, the pin tube 52 may be oriented in a span-wise direction. Further, the tip end segment 30 may also include a pin joint slot 50 located on the beam structure 40. Moreover, as shown, the pin joint slot 50 may be oriented in a chord-wise direction.

[0047] Referring now to FIG. 5, a perspective view of a section of the root end segment 32 according to the present invention is illustrated. As shown, the root end segment 32 includes a spar element 60a. The spar element 60a may be defined with a receiving section 60. The receiving section 60 of the spar element 60a may extend lengthwise to a predetermined length within the root end segment 32 for receiving the beam structure 40 of the tip end segment 30. Further, as shown, the receiving section 60 may include the spar structures 66 that extend lengthwise for connecting with the beam structure 40 of the tip end segment 30. In addition, as shown, the receiving section 60 may include a chord-wise member 48 [as can be seen in FIG. 6] having a span-wise pin joint slot 56 defined therethrough. Moreover, as shown, the receiving section 60 may include a chord-wise pin joint slot 58 defined therethrough that aligns with the pin joint slot 50 of the beam structure 40.

[0048] Referring now to FIG. 6, an assembly 70 of the rotor blade 28 having the tip end segment 30 joined with the root end segment 32 according to the present invention is illustrated. As shown, the assembly 70 illustrates multiple supporting structures beneath outer shell members of the rotor blade 28 having the tip end segment 30 joined with the root end segment 32. More specifically, as shown, the span-wise extending pin 52 of the receiving end 54 of the beam structure 40 is received within the span-wise pin joint slot 56 of the receiving section 60 so as to secure the first and second blade segments 30, 32 together. Referring now to FIG. 6, an exploded perspective view of the multiple supporting structures of the assembly 70 towards the receiving section 60 of the rotor blade 28 is illustrated. As shown, the spar structures 66 are configured to receive the beam structure 40) and may include the chord-wise pin joint slot 58 that align with the pin joint slot 50 of the beam structure 40 through which a chord-wise extending pin 62 may be inserted. Further, as shown, the chord-wise extending pin 62 may be configured to remain in a tight interference fit within the aligning pin joint slots 50, 58 such that spar structures 66 and the beam structure 40 are joined during assembly. Further. FIG. 6 also illustrates the chord-wise member 48 that includes the pin joint slot 56 configured for receiving the pin tube 52 (also referred to herein as the span-wise extending pin 52) of the beam structure 40. As such, the pin tube 52 is configured to form a tight interference fit pinned joint.

[0049] Exemplary cross-sectional shapes of spar element 60a are shown in FIGS. 8A to 8C. FIG. 8A shows a spar element 60a having a rectangular cross-section. It should be understood that also a square cross-section is comprised within the meaning of the term rectangular. According to another embodiment of the present invention shown in FIG. 8B, the spar element 60a has an elliptical cross-section. It should be understood that also a circular cross-section is comprised within the meaning of the term elliptical. An even further embodiment of the present invention is shown in FIG. 8C. Therein, the cross-sectional shape of spar element 60a is adjusted to the cross-sectional shape of the wind turbine rotor blade 28. The cross-sectional shape is basically rectangular, but the upper and lower connecting surfaces are curved so as to follow the shape of the blade shells. Although FIGS. 8A to 8C show the cross-sectional shape of spar element 60a, it should be understood that the cross-sectional shapes of beam structure 40 will be selected to correspond with the cross-sectional shape of receiving section 60. In some embodiment, the spar element 60a may be a multi-piece receiver section. As shown in FIG. 8D, the receiver section may be prefabricated into two halves. In further embodiments of the disclosure, the method of adhering the receiving section 60 to the at least one of the first shell half structure or the second shell half structure of the wind turbine blade 28 is substantiated with reference to FIGS. 9 and 10.

[0050] Referring now to FIGS. 9 and 10, which illustrates method of manufacturing the wind turbine blade 28 including the spar element 60a. In an embodiment, the first shell half structure and the second shell half structure of the wind turbine blade 28 may be manufactured by a moulding process using a mould 103. FIG. 11a illustrates a schematic side view of a mould 103 for manufacturing shell half structures of the wind turbine blade 28. In addition to the method substantiated hereinbelow, the method is also depicted in the way of flowcharts in the FIGS. 11b and 11c. The pressure and suction side shells of the wind turbine blade 28 are manufactured using the mould 103 as shown in FIG. 11a. The mould 103 may be defined with an outer surface 103a and an inner surface 103b. The inner surface of the mould 103 is aerodynamic. In an embodiment, the first shell half structure 30a and 32a, and the second shell half structure 30b and 32b for the root end segment 32 and the tip end segment 30 may be manufactured in a single mould 103. Initially, a blade gel coat or primer is typically applied to the inner surface 103b of the mould 103. Further, fiber reinforcement and/or fiber fabrics are placed into the inner surface 103b of the mould 103. A plurality of layers of fibers may be positioned on the inner surface 103b of the mould 103. In an embodiment, the plurality of layers of fibers may include aramid fiber fabrics, glass fibers, carbon fiber fabrics or hybrid fiber fabrics made of glass and carbon. Other, fiber fabrics not limiting to the above-mentioned fabrics which are known in the art may also be used. In some embodiments, the fibers used may be in any form such as but not limiting to fabrics, prefabricated structures such as pultrusion's or loose fibers.

[0051] Upon placing the plurality of layers of fibers on the mould, the spar element 60a may be positioned on the at least one of the first shell half structure 32a or the second shell half structure 32b of the root end segment 32 of the blade 28. In an embodiment, the spar element 60a may be positioned proximal to the chord-wise joint 34. The spar element 60a may be configured to receive the beam structure 40 and may also be referred to as spar beam receiver section. In a preferred embodiment, the spar element 60a may be a prefabricated structure. The spar element 60a is positioned preferably on the first shell half structure 32a of the root end segment 32. Further, a vacuum bag 100 may be used to seal and close the mould comprising the plurality of layers of fibers and the spar element 60a. A high vacuum pump may be used to remove air in a cavity created by the vacuum bag 100 and the mould [not shown] to eliminate or expel air from the cavity and consolidate the plurality of layers of fibers and the spar element 60a. Upon sealing the plurality of layers of fibers and the spar element 60a, a resin may be infused through the cavity created by the vacuum bag 100 and the mould. The resin infused may flow through the cavity and wet the plurality of layers of fibers. Also, the infused resin flows between the plurality of layers of fibers and the spar element 60a. The infused resin is allowed to cure before the vacuum bag 100 is removed from the mould. This process is herein also referred to as resin infusion process. In a preferred embodiment, the mould of the first shell half structure 32a and the second shell half structure 32b may be closed and the resin may be infused to the plurality of layer of fibers and the spar element 60a and the resin is allowed to cure. In this condition, sealing flanges of the mould when closed together may be configured to act as vacuum bag to aid in resin infusion. The above-described process ensures that the spar element 60a is formed as an integral part of the first shell half structure 32a of the root end segment 32 of the blade 28. The spar element 60a may be adhered to the first shell half structure 32a of the blade 28 without the use of conventional adhesive bonds. It should be understood that the spar element 60a may also be positioned on the second shell half structure 32b of the root end segment 32 of the blade 28 and may be adhered to the second shell half structure 32b. Positioning of the spar element 60a on the first shell half structure 32a should by no means be construed as a limitation of the present invention.

[0052] In an embodiment of the disclosure, the spar element 60a may be adhered to at least one of the first shell half structure 32a and the second shell half structure 32b on the root end segment 32 that may be prefabricated. The method of adhering the spar element 60a to the prefabricated blade 28 is substantiated hereinbelow. At least one of the first shell half structure 32a or the second shell half structure 32b of the root end segment 28 may be placed in the mould. The spar element 60a is positioned over at least one of the first shell half structure 32a or the second shell half structure 32b which is prefabricated. In the present invention and for ease of substantiating, the spar element 60a may be considered to be placed on the first shell half structure 32a of the root end segment 32 of the blade 28. A portion of the spar element 60a which may come in contact with the first shell half structure 32a may be defined with a flow path. The flow path may be configured to facilitate flow of the resin between a portion of the first shell half structure 32a at which the spar element 60a is positioned and the spar element 60a. In an embodiment, the flow path may be created by using fluid flow media such as but not limiting to fiber mats or any other suitable means. Once the spar element 60a is positioned over the first shell half structure 32a, the resin is infused through the flow path defined on the portion of the spar element 60a and is allowed to cure. The spar element 60a may be adhered to the first shell half structure 32a upon complete curing of the resin. In an embodiment, the spar element 60a may be adhered to a spar cap of the blade 28. The spar element 60a may be adhered to the spar cap by resin infusion process. The said process eliminates the use of conventional adhesive bonds which lead to high concentrated loads. In an embodiment, the resin may include a polyester compound such as but not limiting to an unsaturated polyester compound. In an embodiment, the resin used for infusion in the present disclosure is at least one of vinyl ester or epoxy resin.

[0053] In some embodiment and as illustrated in FIG. 8D, each of the two halves of the spar element 60a may be positioned on each of the first shell half structure 32a and the second shell half structure 32b [illustrated in dotted lines] of the wind turbine blade 28. For example, a first half of the spar element 60a may be positioned on the first shell half structure 32a and a second half of the spar element 60a may be positioned on the second shell half structure 32b. In an embodiment, the two halves of the spar element 60a may be positioned at a predetermined position on the first shell half structure 32a and second shell half structure 32b. The pre-determined position described herein above may be proximal to the chord-wise joint 34 on the first and second shell half structures 32a and 32b. In some embodiments, predetermined position may be spar cap region in the wind turbine blade 28. The surface of the two halves of the spar element 60a that may come in contact with the shell 32a and 32b may be defined with a flow path. Once the two halves of the spar element 60a are placed over the respective shells 32a and 32b, resin may be infused in between the shells 32a and 32b and the two halves of the spar element 60a. The resin may be infused through the flow path defined on each of the two halves of the spar element 60a. The infused resin may be subsequently allowed to cure, thereby adhering the two halves of the spar element 60a to the respective shells 32a and 32b. In another embodiment, the two halves of the spar element 60a may be positioned over spar caps. Each of the two halves of the spar element 60a may be adhered to the respective spar caps by resin infusion process. Once the resin is cured and the each of the two halves of the spar element 60a is adhered to the respective spar caps, the spar caps are positioned on the first shell half structure 32a and second shell half structure 32b at a pre-determined position. The spar caps may be adhered to the first shell half structure 32a and second shell half structure 32b by the resin infusion process. Further, the two halves of the spar element 60a may be adhered to one another by any conventional joining process including but not limiting to adhesive bonding.

[0054] In an embodiment, as shown in FIG. 12, an end opposite to the receiving section 60 of the spar element 60a may be adhered or joined to a shear web 102 on the root end segment 32 of the wind turbine blade 28. The shear web 102 may be positioned at a substantially central portion on at least one of the first shell half structure 32a or the second shell half structure 32b. The shear web 102 may extend along the length blade 28 from the root end and up-to the spar element 60a. In some embodiments, the shear web 102 may be connected to at least one of the first shell half structure 32a or the second shell half structure 32b by at least one of adhesive bond or resin infusion process. As depicted in FIG. 12. the end of the spar element 60a opposite to the receiving section may be connected to the shear web 102 of the blade 28 by the resin infusion process. The resin may be infused in a space between the end of spar element 60a and the shear web 102.

[0055] Typical ways of joining the shear web 102 with the spar element 60a are shown in FIGS. 13 (a) to 14 (d). According to some embodiments of the present invention, the spar element 60a may be defined with an extending portion on the end opposite to the receiving portion 60. The extending portion may be configured to connect to the shear web 102 of the blade 28. FIGS. 13 (a) to (d) shows the extended portion of the spar element 60a that may be connected with the shear web 102 of the root end segment 32. As shown in FIG. 13 (a), the root end segment 32 of the blade 28 may include multiple shear web 102 extending parallelly from the root region of the blade up to the spar element 60a. The parallelly running shear webs 102 are then adhered to the spar element 60a by the resin infusion process, thus forming a co-infused joint between the spar element 60a and the shear web 102. According to another embodiment of the present invention, as shown in FIGS. 13 (b) and 13 (c), the root end segment 32 of the blade 28 may include a single shear web 102 extending from the root region of the blade 28 to the spar element 60a. The single shear web may be adhered to the spar element 60a by a Y-shaped joint member as shown in FIG. 13 (b). Also, as shown in FIG. 13c, the shear web 102 may extend into a portion of the spar element 60a. In both cases i.e. embodiments according to FIGS. 13 (b) and 13 (c), the resin may be infused between the spar element 60a and the shear web 102 to form the co-infused joint. An even further embodiment of the present invention is shown in FIG. 13 (d), here the ends of the spar element 60a may be abutted against the shear web 102 and the resin may be infused between the shear web 102 and the spar element 60a. In some embodiments and as shown in FIG. 8D, the spar element 60a may be defined with a scarf region. The scarf region may be configured to be connected to the shear web 102 and the spar cap by a resin infusion process. In a preferred embodiment, the resin may be infused in the gap formed between the shear web 102 and the spar element 60a [i.e. the process of joining the shear web and the spar element according to FIGS. 12 and 13]. A flow media such as but not limiting to fiber mat may be positioned in the gap between the shear web 102 and the spar element 60a. The resin may then be infused through the flow media to the gap and may be allowed to cure. Upon curing the resin bonds both the spar element 60a and the shear web 102 together to obtain a resin infused joint.

[0056] In some embodiments, the shear web 102 may be directly connected to the end of the end of the spar element 60a as shown in FIGS. 14 (a) to (d). As shown in FIGS. 14 (a) and 14 (b), at least one corner of the end of the spar element 60a may be chamfered. The chamfered portion on the spar element 60a may accommodate the ends of the shear web 102. The ends of the shear web 102 that may be connected to the spar element 60a may also be counter chamfered. The resin may be infused in the space between the chamfered portion of the shear web 102 and the spar element 60a to adhere the shear web 102 to the spar element 60a. According to another embodiment of the present invention as shown in FIGS. 14 (c) and 14 (d), the shear web 102 of the root end segment 32 may be abutted against the end of the spar element 60a. The resin may be infused in space between the shear web 102 and the spar element 60a, thereby adhering the spar element 60a to the shear web 102 upon curing of the resin. However, the above methods should not be construed as a limitation to the present invention.

[0057] Upon positioning the spar element 60a, shear web 102 and other blade components on the at least one of the first shell half structure 32a, the second shell half structure 32b may be adhered to the first shell half structure 32a. In an embodiment, before adhering the second shell half structure 32b to the first shell half structure 32a, the surfaces of the spar element 60a, and other blade components facing the second shell half structure 32b may be applied with adhesives. Subsequently, before lowering the second half shell structure 32b on to the first half shell structure 32a, adhesive is applied over the leading edge and the trailing edge. Once the adhesive is applied on the leading edge and the trailing edge the second half shell structure 32b may be lowered over the first shell half structure 32a. Upon bonding the first shell half structure 32a and second shell half structure 32b, the adhesive may be allowed to cure to obtain the root end segment 32 of the blade 28. Further, the blade 28 is removed from the mould and the excess material may be trimmed. In some embodiments, the spar elements 60a, shear web 102 and other blade components may be adhered by the resin infusion process on at least one of the shells 32a and 32b which undergoes more pressure during operation. In an embodiment, the said resin infusion method may also be used to adhere beam structure 40 in the tip end segment of the blade 30.

[0058] In an embodiment, the use of resin infusion process for adhering the spar element 60a may reduce the concentrated load at the chord-wise joint 34 of blade 28 unlike the conventional adhesive bond process. The structural properties of blade at the chord-wise joint doesn't change by the use of resin infusion process which is not in case of the conventional adhesive bonds. The resin infused joints may significantly increase potential strength of tip end segment 30 of the blade 28. Also, the elimination of adhesive bonds reduces the blade mass, cost and significantly increases the robustness and reliability. Also, use of resin infusion process does not limit the design feature unlike the adhesive bonds.

[0059] The invention is not limited to the embodiments described herein and may be modified or adapted without departing from the scope of the present invention.

[0060] Exemplary embodiments of the present disclosure are set out in the following items: [0061] 1. A method of manufacturing a shell of a wind turbine blade (28), the method comprising: [0062] laying one or more shell or spar fibers, on a surface of mould to form at least a portion of the blade shell; [0063] positioning a spar element (60a) at pre-defined position on the one or more layers of fiber; [0064] covering a vacuum bag (100) over the one or more layers of fiber and the spar element (60a) to seal the spar element (60a) and the one or more layers of fibers; and [0065] infusing resin through the one or more layers of fiber and the spar element (60a) and subsequently curing the same to obtain the shell (32a or 32b), wherein the spar element (60a) adheres to the shell (32a or 32b) upon curing the infused resin. [0066] 2. The method according to claim 1, wherein the spar element (60a) is a spar beam receiver section or a portion of receiver section. [0067] 3. The method according to any of claims 1-2, wherein the resin includes a polyester compound, preferably at least one of a vinyl ester or epoxy resins. [0068] 4. The method according to any of claims 1-3, wherein the one or more layers of fibers on the mould are glass fibers and the one or more layers of fibers are in form of at least one of fabrics, prefabricated structure or loose fibers. [0069] 5. The method according to any of claims 1-4 comprises positioning a shear web (102) at a substantially central portion of the shell (30 and 32), wherein the shear web (102) extends along length of the shell and up-to the spar element (60a). [0070] 6. The method according to claim 5, wherein an end of the spar element (60a) is connected to the shear web (102). [0071] 7. The method according to claim 6 comprises joining the end of spar element (60a) and the shear web (102) by resin infusion process. [0072] 8. A method for joining a spar element to a wind turbine blade (28), the method comprises: [0073] positioning the spar element (60a) on a shell (32a or 32b) or spar cap of the wind turbine blade (28), wherein a portion of the spar element (60a) in contact with the shell or spar cap is defined with a flow path; and [0074] infusing resin between the spar element (60a) and the shell (32a or 32b) or the spar cap through the flow path and subsequently curing the same to adhere the spar element (60a) to the shell (32a or 32b) or spar cap of the wind turbine blade (10). [0075] 9. The method according to claim 8, wherein the resin includes a polyester compound, preferably at least one of a vinyl ester or epoxy resins. [0076] 10. The method according to any of claims 8-9 comprises positioning a shear web (102) at a substantially central portion shell, wherein the shear web (102) extends along length of the shell and up-to the spar element (60a). [0077] 11. The method according to claim 10, wherein an end of the spar element (60a) is connected to the shear web (102). [0078] 12. The method according to claim 11 comprises joining the spar element (60a) and the shear web (102) of the wind turbine blade by resin infusion process. [0079] 13. A method for manufacturing a root end segment (32) of the wind turbine blade (10), the method comprising: [0080] forming a first shell half structure (32a) and a second shell half structure (32b) separately in a mould; [0081] joining a spar element (60a) to at least one of the first shell half structure (32a) and the second shell half structure (32b) by resin infusion process in the mould; [0082] positioning a shear web (102) at a substantially central portion of the first shell half structure (32a) and the second shell half structure (32b), wherein the shear web (102) extends in a spanwise direction up-to the spar element (60a); [0083] joining an end of the spar element (60a) and the shear web (102) by resin infusion process; and [0084] joining and sealing the first shell half structure (32a) and a second shell half structure (32b) to obtain the root end segment (32) of the wind turbine blade (10). [0085] 14. The method according to claim 13, wherein a first half of the spar element (60a) is bonded to the first shell half structure (32a) and a second half of the spar element (60a) is bonded to the second shell half structure (32b). [0086] 15. The method according to any of claims 13-14 comprises adhering the first half of the spar element (60a) to the second half of the spar element (60a) before joining of the first shell half structure (32a) and the second shell half structure (32b). [0087] 16. The method according to any of claims 13-15, wherein the spar element (60a) is defined with an extending portion on an end opposite to receiving section (60), the extending portion is configured to connect to the shear web (102). [0088] 17. The method according to any of claims 13-16, wherein the first shell half structure (32a) and the second shell half structure (32b) are formed by laying plurality of layers of fiber in the mould, infusing resin and subsequently curing the resin. [0089] 18. The method according to any of claims 13-17, wherein the resin includes a polyester compound, preferably at least one of a vinyl ester or epoxy resins. [0090] 19. The method according to any of claims 17-18, wherein the one or more layers of fibers on the mould are glass fibers. [0091] 20. A wind turbine blade (10) comprising a shell and a spar element (60a) adhered to the shell through the resin infusion process as claimed in any of the previous claims.

LIST OF REFERENCE NUMERALS

[0092] 10 Wind turbine [0093] 12 Tower [0094] 14 Support surface [0095] 16 nacelle [0096] 17 Blade tip [0097] 18 Generator [0098] 19 Blade root end [0099] 20 Gear box [0100] 22 Rotor [0101] 24 Rotor shaft [0102] 26 Rotatable hub [0103] 28 Wind turbine blade or Rotor blade [0104] 30 Tip end segment [0105] 32 Root end segment [0106] 32a First shell half structure of root end segment [0107] 32b Second shell half structure of root end segment [0108] 32c Airfoil region [0109] 32d Transition region [0110] 32e shoulder [0111] 34 Chord wise joint [0112] 36 Internal support structures [0113] 38 Arrow [0114] 40 Beam structure [0115] 42 Shear web on tip end segment [0116] 44 and 46 Spar cap [0117] 48 Chord wise member [0118] 50 Pin Joint slot [0119] 52 Span-wise extending pin [0120] 54 Receiving end [0121] 56 Span-wise pin joint slot [0122] 58 Chord-wise pin joint slot [0123] 60 Receiving section [0124] 60a Spar element [0125] 60b Extended portion of the spar element [0126] 62 Chord-wise extending pin [0127] 66 Spar structures [0128] 100 Vacuum bag [0129] 102 Shear web for root end segment and configuration of shear web [0130] 103 Mould [0131] 103a and 103b outer and inner surface of the mould respectively