Technical field

The present invention relates to a leading edge device for attachment to a wind turbine blade, wherein the leading edge device comprises at least an erosion shield with an in ner surface and an outer surface. The present invention also relates to a wind turbine blade with an attached leading edge device. The present invention further relates to a method of manufacturing such a leading edge device and a method of installing the leading edge device.

Background

It is well-known that the leading edge area of a wind turbine blade is subjected to vari- ous weather and environmental conditions, such as high winds, hails, dusts, salt sprays, etc. A protective coating or tape may be applied to the leading edge area.

Field experiences have shown that such erosion coating or tape will last approximately between 5 to 8 years. However, the coating or tape may rupture due to heavy erosion and thereby flutter freely in the wind. This will result in a loss of aerodynamic perfor mance and generation of added aerodynamic noise. Service operations are thus re quired to remove the ruptured erosion shield and further repairing any cracks or failures in the exposed blade surface, before applying a new erosion shield. Such extensive and complex service operations require the wind turbine to be taken out of operation, thereby increasing the downtime and loss of annual energy production (AEP).

In an attempt to increase the time between service operations, a multi-layered erosion shield can be attached to or integrated into the leading edge area of the wind turbine blade. WO 2013/09221 1 A1 discloses such a multi-layered erosion shell where the outermost layer is able to passively peel off or rupture during operation to maintain a relative smooth outer surface. WO 2017/012632 A1 discloses another multi-layered erosion shell comprising two layers of thermoplastic materials, wherein the inner layer is optimised for integration with the blade shell and the outer layer is optimised for ero sion resistance. It is further known that the aerodynamic performance of the wind turbine blade can be improved by attaching aerodynamic devices to the leading edge. The aerodynamic de vices may extend further along the pressure side and/or the suction side. These aero dynamic devices modifies the airflow over the wind turbine blade and are normally spe cifically designed for a particular purpose, such as delaying stall, improving the tip vor tex energy or enhancing the lift-to-drag ratio. Alternatively, the wind turbine blade can be manufactured with a specially designed leading edge profile integrated into the blade shell.

US 2013/0056585 A1 discloses an aircraft blade with a continuous array of tubercle shaped protrusions, between which a convex or concave surface is formed. EP 1805412 B1 discloses an array of individually spaced tubercles which can be integrat ed into the blade shell or attached to the leading edge of the blade shell.

Wind turbine blades with such integrated leading edge profiles require very time- consuming, labour-intensive, and expensive manufacturing steps as well as surface preparations in order to apply the protective coating. The integrated leading edge pro files also require the use of specially designed erosion shells due to their complex sur face profiles, thereby increasing the complexity and costs of manufacturing such ero sion shields.

US 2009/0220795 A1 discloses a multi-layered coating system suitable for application on the leading edge area of a wind turbine blade. The multi-layered coating system is optimised to reduce the amount of surface preparation required before applying the protective coating.

US 201 1/0008174 A1 discloses F-shaped elastomeric vortex generator attached to the leading edge area of an aerodynamic blade. The complexity and time for preparing the leading edge surface for attachment of such vortex generators is increased if a leading edge protection is applied first. Further, the vortex generator may weaken the leading edge protection, if erosion resistant material or gelcoat is removed before attaching the vortex generator.

Object of the invention

An object of the invention is to provide a leading edge device, a wind turbine blade and methods that solve the abovementioned problems. Another object of the invention is to provide a leading edge device, a wind turbine blade and methods that saves time and costs when manufacturing a wind turbine blade with a leading edge protection combined with a complex leading profile.

Another object of the invention is to provide a leading edge device, a wind turbine blade and methods that reduces the downtime and increases the operational lifetime.

A further object of the invention is to provide a leading edge device, a wind turbine blade and methods that increase the flexibility when upgrading existing wind turbine blades.

Another further object of the invention is to provide a leading edge device, a wind tur bine blade and methods that save time and costs when repairing wind turbine blades having a complex leading edge profile.

Detailed description of the invention

One object of the invention is further achieved by a leading edge device for a wind tur bine blade or a blade section, comprising an erosion shield extending in a longitudinal direction from a first end to a second end and further in a circumference direction from a first edge to a second edge, the erosion shield has an inner surface and an opposite facing outer surface arranged between said first and second ends, wherein the erosion shield is configured to be attached to a leading edge surface of the wind turbine blade characterised in that at least one airflow modifying element projects from said outer surface, the at least one aerodynamic element having a first profile, wherein said at least one airflow modifying element and said erosion shield are integrally formed.

In other words, the present invention relates to a leading edge device for a wind turbine blade or a blade section, comprising an erosion shield extending in a longitudinal direc tion from a first end to a second end and further in a circumference direction from a first edge to a second edge, the erosion shield has an inner surface and an opposite facing outer surface arranged between said first and second ends, wherein the erosion shield is configured to be attached to a leading edge surface of the wind turbine blade charac terised in that at least one airflow modifying element projects from said outer surface, the at least one airflow modifying element having a first profile, wherein said at least one airflow modifying element and said erosion shield are integrally formed. This provides alternative leading edge device with combined leading protection and aerodynamic effect. The present configuration allows aerodynamic elements of various types and sizes to be incorporated into the leading edge protection to form an integrat ed device. This saves manufacturing time and costs as the leading edge profile of the wind turbine can be manufactured with a basic leading edge profile. The present con figuration also allows for a more versatile upgrade of existing wind turbine blades.

In a preferred embodiment, at least one of the airflow modifying elements protrudes from the outer surface of the erosion shield. In some embodiments, all of the airflow modifying elements protrude from the outer surface of the erosion shield. The airflow modifying elements are preferably regularly spaced on the leading edge device.

It is thus preferred that the leading edge device comprises one or more raised surfaces or one or more local maxima in its outer surface, wherein the raised surfaces or local maxima are constituted by the airflow modifying elements.

According to a preferred embodiment, the airflow modifying elements are covered by a layer of material, wherein the same layer of material covers all airflow modifying ele ments. It was found that such design provides improved structural integrity while being simple and cost-effective. In some embodiments the airflow modifying elements are covered by a first layer of material, wherein the first layer of material is covered by a second layer of material.

It is preferred that the leading edge device comprises between 2 and 20 airflow modify ing elements, such as between 5 and 15, or between 5 and 10 airflow modifying ele ments.

The leading edge element is preferably formed as an erosion shield comprising a num ber of layers arranged in a stack. The erosion shield extends in a longitudinal direction from a first end to a second end and further in a circumference direction from a first edge to a second edge. The erosion shield has an inner surface configured to contact a leading edge surface of the wind turbine blade. The erosion shield further has an outer surface facing away from the wind turbine blade, when installed. The length and width, i.e. in the circumference direction, may be selected dependent of the aerodynamic pro file and geometrical dimensions of the wind turbine blade. This provides an erosion re sistant structure protecting the blade surface against cracking and failures. The first and second ends may have a curved or tapered end profile seen in length di rection, a curved or convex end profile seen in width direction, and/or integrated serra tions for reducing the negative aerodynamic effect on the spanwise local airflow.

According to one embodiment, said at least one airflow modifying element extends along the outer surface in at least the length or circumference direction, wherein said first profile has a local thickness extending from said outer surface to a local outer sur face of the at least one airflow modifying element.

The airflow modifying elements are configured to modify the airflow over the wind tur bine blade. For example, the airflow modifying elements may be shaped to improve the lift-to-drag ratio of the wind turbine blade. The airflow modifying element may have any suitable two-dimensional or three-dimensional shaped body extending in the longitudi- nal direction and/or in the circumference direction. Once installed, the aerodynamic performance of the wind turbine blade can be improved.

The airflow modifying element may have a body with a local thickness or height meas ured between the outer surface of the erosion shell and the local outer surface of the airflow modifying element. The local thickness may be constant or vary along the length and/or the width of the airflow modifying element. Alternatively, the local thick ness may taper off towards one or more local ends and/or one or more local edges.

Further, the erosion shield may have a local thickness or height measured between the outer surface and the inner surface. The local thickness may be constant or vary along the length and/or the width of the erosion shield. Alternatively, the local thickness may taper off towards the first and second ends and/or the first and second edges.

According to one embodiment, said first profile forms a substantially two-dimensional shaped body extending substantially in the circumference direction. The airflow modifying element may have a substantially two-dimensional (2D) shaped body, e.g. an elongated profile, extending substantially in a local longitudinal direction and a local thickness direction. The body may have a substantially constant width measured along its local length. This 2D shaped body may arranged relative to the cir cumference direction so that it extends parallel to the circumference or longitudinal di rection or are positioned in an inclined angle relative to the circumference or longitudi nal direction. For example, the airflow modifying element may be formed as a fence, a strip, a fin, a vane or another suitable 2D shape. For example, the airflow modifying el ement may have a straight or curved body.

This configuration may be suited for preventing spanwise airflow over the wind turbine blade. This configuration may also be suited for guiding the airflow towards the trailing edge or the tip end dependent on the spanwise position of the airflow modifying ele ment on the wind turbine blade. This configuration may in some instances also trans form the laminar airflow into a turbulent airflow and in turn delay the airflow separation.

In a special configuration, the airflow modifying element may form one part of a com bined aerodynamic element extending further along the pressure side and/or the suc tion side. This combined aerodynamic element may optionally extend along the entire circumference of the wind turbine blade. For example, a second part of the combined aerodynamic element may extend along the pressure side and a third part of the com bined aerodynamic element may extend along the suction side. The second and third parts may optionally be connected at the trailing edge to form a continuous element.

According to one embodiment, said first profile forms a substantially three-dimensional shaped body extending in the longitudinal direction and further in the circumference di rection.

Alternatively, the airflow modifying element may have a substantially three-dimensional (3D) shaped body, e.g. a complex shaped profile, extending substantially in a local lon gitudinal direction, a local width direction and a local thickness direction. The local thickness may vary as function of the local width and/or the local length. This 3D shaped body may be arranged relative to, e.g. aligned with, the leading edge of the wind turbine blade. For example, the airflow modifying element may be formed as a bump, a tubercle, a serration or another suitable 3D shape. The present invention is particularly suited for manufacturing leading edge devices hav ing complex 3D profile. Conventional lay-up processes only allows for the production of leading edge profile having a substantially 2D profile. This allows the body of these aerodynamic elements to be manufactured using a more optimal process, thereby re ducing lay-up time and manufacturing costs.

According to a special embodiment, said body is covered with a protective coating and/or covered with a laminate of layers.

The body of the airflow modifying elements may optionally be covered with a coating and/or one or more outer layers. This allows the local outer surfaces of the airflow mod ifying elements be protected against environmental erosions and impacts, thereby in creasing the service intervals and the lifetime of the leading edge device. The above coating and/or outer layers may form part of the erosion shield or form an additional erosion protection.

The body may be made of any suitable plastic or thermoplastic materials or any foam materials, such as polymer; polyamide; polyester; polypropylene; polystyrene; polyure thane; polyethylene; PVC or epoxy; elastomer or resin. For example, but not limited to, acrylonitrile butadiene styrene (ABS); polylactic acid (PLA); polyethylene (e.g. HDPE); SLS Nylon ^® ; rigid opaque plastics (e.g. Vero) or rubber-like plastics (e.g. Tango or Agi- lus). The body may also be made of a fibre-reinforced material or composite, such as fibre-reinforced Nylon ^® or fibre-reinforced polymer, wherein said fibres may be made of carbon, glass, aramid or Kevlar ^® .

Preferably, the body may be made of a resistant material which substantially absorbs erosion forces over time. This allows the body to function as an erosion resistant struc ture. The body may also be made of a flexible material which substantially absorbs im pact shock waves from particles hitting the airflow modifying device. This allows the body to function as a cushioning structure.

The coating may be a gelcoat comprising polymer, urethane, polyester or another suit able material or mixture of materials. Additionally or alternatively, the coating may comprise an ultraviolet (UV) resistant material for protection against UV radiations. The erosion shield may comprise single layer or a plurality of layers arranged in a stack. The erosion shield may for example comprise one or more inner layers and one or more outer layers and, optionally, one or more intermediate layers arranged be tween the inner layers and the outer layers. This provides a multi-layered erosion shield, wherein each layer may be optimised for a particular purpose.

The inner layer may be made of a material selected to provide a strong attachment to the fibre material and/or resin of the blade shell. Alternatively or additionally, the inner layer may be made of a flexible material, as mentioned above, for providing a cushion ing effect. An adhesive layer may optionally be provided between the leading edge sur face and the inner layer for securing a strong attachment of the leading edge device to the fibre material and/or resin of the blade shell. Alternatively, the inner layer may be formed by the body of the airflow modifying elements. Alternatively, the inner layer may extend between the individual airflow modifying elements and further along the local outer surfaces of the body of each airflow modifying element.

The outer layer may be made of an erosion resistant material, as mentioned above, for protecting at least the leading edge surface of the wind turbine blade. The outer layer may extend along the entire inner layer, wherein the body of the airflow modifying ele ments is projecting from said outer layer. Alternatively, the outer layer may extend along the inner layer between the individual airflow modifying elements and further along the local outer surfaces of each airflow modifying element. Alternatively, the out er layer may be formed by the body of the airflow modifying elements.

The intermediate layer may be made of a cushioning material, as mentioned above. The intermediate layer may extend along the entire inner and outer layers. Alternative ly, the intermediate layer may extend along the inner layer and further along the local outer surfaces of each airflow modifying elements. Alternatively, the intermediate layer may be formed by the body of the airflow modifying elements.

According to one embodiment, said at least one airflow modifying element comprises an array of airflow modifying elements arranged along the outer surface. The leading edge device may comprise a number of airflow modifying elements distrib uted along the erosion shield in the longitudinal direction and/or the circumference di rection. For example, the leading edge device may a single airflow modifying element or an array of airflow modifying elements. The number of airflow modifying elements may dependent on the length and/or width of the leading edge device. The airflow mod ifying elements may be individually spaced apart along the erosion shield by a constant or variable distance. Alternatively, the airflow modifying elements may be interconnect ed to form a continuous structure. The distance between the airflow modifying ele ments may be selected based on the dimensions thereof and/or the aerodynamic pro file and geometrical dimensions of the wind turbine blade. This allows for an optimised configuration of the airflow modifying elements.

According to a special embodiment, the first profile of said array of airflow modifying el ements varies along the longitudinal direction and/or the circumference direction.

The profile of each airflow modifying element may be uniform along the longitudinal di rection and/or the circumference direction. Alternatively, the profile of each airflow mod ifying element may vary along the longitudinal direction and/or the circumference direc tion. For example, a first airflow modifying element and at least a second airflow modi fying element may be arranged on the erosion shield. The first airflow modifying ele ment may have a first profile and the second airflow modifying element may have a second profile that differs from the first profile. Said first and second profiles may differ in length, height and/or width.

The erosion shield may have a substantially uniform local thickness in longitudinal di rection and/or the circumference direction. Alternatively, the thickness of the erosion shield may be tapered off within a peripheral edge area. The erosion shield may have a substantially outer surface that is substantially parallel to the inner surface. Alternative ly, the outer surface may have a convex profile in at least circumference direction rela tive to the inner surface so that a maximum local thickness is located at the centre of the erosion shield. This allows the erosion shield to have a minimal negative effect on the aerodynamic performance of the wind turbine blade.

In another aspect, the present invention relates to a leading edge device for a wind tur bine blade or a blade section, comprising an erosion shield extending in a length direc tion from a first end to a second end and further in a width direction from a first edge to a second edge, the leading edge device has an inner surface and an opposite facing outer surface arranged between said first and second ends, the inner surface facing a leading edge surface of the wind turbine blade, when installed, wherein said leading edge device is configured to be attached to the wind turbine blade, wherein at least one protrusion projects from said outer surface in a thickness direction, when installed, the at least one protrusion having a first profile formed by a body, wherein said at least one protrusion and said erosion shield are integrally formed, the leading edge device further has at least one layer covering at least a portion of said outer surface.

In a preferred embodiment, said body is a three-dimensional shaped body having a lo cal thickness, a local length and a local width, wherein said local thickness varies along the local length and the local width.

In another embodiment said body is an elongated body having a local length, a local width and a local thickness, wherein said elongated body extends in at least one direc tion.

In another aspect, the present invention relates to an erosion protection device config ured to be arranged on the leading edge of a rotor blade such that the erosion protec tion device extends generally in a spanwise direction along at least part of the rotor blade, wherein the erosion protection device comprises a curved outer surface extend ing between a first edge and a second edge of the erosion protection device for shield ing at least part of the leading edge of the rotor blade, wherein the outer surface is un dulated to form a plurality of peaks and valleys. In another aspect, the present inven tion relates to a rotor blade assembly comprising a rotor blade, such as a wind turbine rotor blade, having a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root, wherein the rotor blade assembly further comprises at least one of said erosion protection devices arranged on the leading edge of the ro tor blade such that the erosion protection device extends generally in a spanwise direc tion along at least part of the rotor blade. The first edge is preferably arranged at the suction side of the rotor blade, and the second edge is preferably arranged at the pres sure side of the rotor blade. The undulated outer surface of the erosion protection de vice preferably comprises, or is made up of, an outer coating. Preferably, the undulated outer surface is a unitary surface such that the entire surface is comprised of the same material. The erosion protection device usually has an inner surface, opposing the outer surface, wherein the inner surface is shaped to conform to a blade surface along its leading edge. The peaks of the undulated outer surface of the erosion protection device are advantageously configured to alter the aerodynamic characteristics of the rotor blade. The first and/or the second edge may be provided as respective straight edges. In oth er embodiments, the first and/or the second edge may be serrated. The serrations may be shaped to further improve the airflow over the first and second edges.

The erosion protection device may be arranged along 20% to 100%, preferably be tween 40% to 100%, of the blade length measured between the blade root and the blade tip. Each peak of the undulated outer surface may be formed by a core material, which may be sandwiched between one or more outer coatings or layers and one or more inner layers.

One object of the invention is also achieved by a wind turbine blade for a wind turbine, the wind turbine blade comprising at least one blade section extending in a longitudinal direction from a blade root or a tip end to an opposite end and further in a chordwise direction from a leading edge to a trailing edge, the wind turbine blade having a length of at least 35 meters measured between the blade root and the tip end, wherein the wind turbine blade has a first side surface defining a pressure side and a second side surface defining a suction side, wherein a leading edge surface is arranged between the first and second side surfaces, characterised in that a leading edge device as de scribed above is arranged at said leading edge surface.

This provides a wind turbine blade with a complex leading edge profile that is integrat ed into the leading edge protection. This saves manufacturing time and costs as the wind turbine blade is advantageously manufactured with a basic leading profile, there by simplifying the lay-up process of the layers forming the leading edge profile. This further allows for the desired leading profile to be integrally formed in the leading edge device, thereby allowing for a more controlled and optimal manufacture of the complex leading edge profile. The present leading edge device allows the aerodynamic perfor mance of the wind turbine blade to be improved. The wind turbine blade may be formed as a full-span blade or a modular blade having an inner blade section and an outer blade section. The wind turbine blade may com prise two shell parts jointed together to form the profile of the wind turbine blade. The blade shell at the leading edge area may comprise a laminate of fibre layers impreg nated with resin which is later cured.

The leading edge surface may be flushed with adjoining blade surfaces to form a con tinuous blade surface. A sealant or a filler material may be applied along the transition area between the leading edge device and the wind turbine blade to form a smooth transition between the outer surface of the erosion shield and the adjacent blade sur face. This reduces the negative aerodynamic effect of the erosion shield.

Alternatively, the leading edge surface may comprise a recess shaped to partly or fully receive the erosion shield of the leading edge device. The leading edge device may be attached to the wind turbine blade by welding or adhesion. For example, using a plastic welding process, such as laser welding; hot gas welding, e.g. heat sealing; speed tip welding; spot welding; contact welding; hot plate welding; ultrasonic welding; high fre quency welding or solvent welding. For example, by mechanical adhesion; chemical adhesion; dispersive adhesion or diffusive adhesion. Such welding and adhesion tech niques are well known and will not be described further in details.

The leading edge device may also be attached by over-lamination, wherein one or more fibre layers are laid up along the transition area. The fibre layers may be laid up in a combined recess formed by a local recess in the blade surface aligned with anoth er local recess in the outer surface of the leading edge device. The fibre layers are then impregnated with resin and cured to provide a strong attachment. Additionally or alter natively, the inner layer of the erosion shield may be attached to fibre material and/or resin of the blade shell by the above welding or adhesion. This also reduces the nega tive aerodynamic effect of the erosion shield.

The wind turbine blade has a blade length of at least 35 metres, preferably over 50 me tres. One or more leading edge devices may be arranged along a part of the leading edge. Each leading edge device may have a length of up to 10 metres, preferably up to 5 metres, e.g. between 10 centimetre and 1 metre. The leading devices may be ar ranged between 20% to 100% of the blade length measured from the blade root, pref erably between 40% to 100%, e.g. between 60% to 100%, of the blade length. One object of the invention is further achieved by a method of manufacturing a leading edge device, comprising the steps of:

- providing an erosion shield extending in a longitudinal direction from a first end to a second end and further in a circumference direction from a first edge to a second edge, the erosion shield has an inner surface and an opposite facing outer surface arranged between said first and second ends, wherein the erosion shield is configured to be at tached to a leading edge surface of the wind turbine blade,

- providing at least one airflow modifying element comprising a body with a first profile, the body having at least one local outer surface,

- integrating said erosion shield and said at least one airflow modifying element to form the leading edge device.

This provides alternative method of providing a leading edge device as the leading edge protection is manufactured with integrated aerodynamic elements. This allows for the complex leading profile of a wind turbine blade to be manufactured in a fast and simple process. The shape of the airflow modifying elements may thus be manufac tured and/or machined into a finished shape under more controlled conditions, thus al lowing for the use of an optimised process, such as 3D-printing and/or 3D-machining.

Integrating the airflow modifying elements into the erosion shell allows for a seamless attachment and saves time and costs if repairs of the complex leading profile are needed. This also allows for an improved erosion protection of the complex leading profile.

The present method eliminates the step of preparing the outer surface of the erosion shield before attaching the airflow modifying elements, as required in EP 1805412 B1 and in US 201 1/0008174 A1 . Other conventional methods, such as applying a protec tive coating as disclosed in US 2009/0220795 A1 , require the complex leading profile to be integrated into the blade shell. This complicated and labour intensive manufactur ing process is also eliminated by the present method as the complex leading profile is formed by the leading edge device.

According to one embodiment, said erosion shield and said at least one airflow modify ing element are manufactured as a single piece in a common process, or as individual pieces in separate processes. The body of the airflow modifying elements may be manufactured in an optimised pro cess and later integrated into the leading device in another process. For example, the body may be formed in an extrusion process, a vacuum forming process, an injection moulding process or in another optimised process. The elements may, if needed, be cut into the desired length to form the finished elements. This allows the airflow modify ing elements and in turn the complex leading edge profile to be manufactured in a fast and simple process, thereby saving time and costs.

The finished elements may optionally be shipped or transported to another site for final assembling the leading edge device. This allows the airflow modifying elements to be manufactured under controlled conditions and then integrated into the erosion shield in an optimised process.

Alternatively, the body of the airflow modifying elements may be manufactured and in tegrated into the leading device in a combined process. The airflow modifying elements may thus be integrated during the manufacture of the erosion shield. This allows the leading edge device to be manufactured and assembled at the same site, e.g. at a pro duction line separate from the blade moulding line.

According to a special embodiment, at least a part of the at least one airflow modifying device is manufactured by three-dimensional printing and/or by three-dimensional ma chining of a base element. According to the present invention, the base element may have wider production tolerances than known base elements for erosion shields due to the provision of the airflow modifying elements overlaying the underlying geometry. This renders the base element more cost-effective and reliable than known structures.

The airflow modifying elements may advantageously be formed directly in a 3D-printing process or in a 3D-machining process. Alternatively, the selected plastic or foam mate rial may be 3D-printed into a base element substantially having the desired profile. The base element may then be 3D-machined to form the finished elements. This also al lows the airflow modifying elements and in turn the complex leading edge profile to be manufactured in a fast and simple process, thereby saving time and costs.

According to one embodiment, the at least one airflow modifying element is sand wiched between layers of the erosion shield or attached to a layer of the erosion shield. The body of the airflow modifying elements may be arranged between different layers of the erosion shield to form an integrated device. For example, between the inner and outer layers of the erosion shield, or between a first outer layer and a second outer lay er of the erosion shield. The different layers of the leading edge device may be at tached to each other and further to the body of the airflow modifying elements. For ex ample, the attachment may be done by adhesion, welding or another suitable tech nique. This allows for a seamless attachment which reduces the risk of the airflow mod ifying elements separating under heavy erosions.

The body of the airflow modifying elements may also be attached to a layer of the ero sion shield. For example, the inner layer or the outer layer of the erosion shield. The at tachment may be done by adhesion, welding or another suitable technique.

According to one embodiment, the method further comprises at least:

- applying a protective coating over at least one of said outer surface and said at least one local outer surface, or

- laying up at least one outer layer of a protective material over at least one of said out er surface and said at least one local outer surface.

A protective coating, as mentioned above, may be applied over the outer surface of the erosion shield and further over the local outer surfaces of the airflow modifying ele ments. This provides a substantially seamless transition between the airflow modifying elements and the erosion shield. This also protects the outer surface of the airflow modifying elements.

Alternatively or additionally, one or more outer layers may be laid up over at least the local outer surfaces of the airflow modifying elements. For example, at least the outer layer and/or the intermediate layer of the erosion shield may extend along the outer surface and further over the body of the airflow modifying elements. Alternatively, all layers of the erosion shield may extend along the outer surface and further over the body of the airflow modifying elements. This allows the erosion shield to enclose or conform to the body of the airflow modifying elements while at the same time conform ing to the shape of the leading edge surface. For example, an additional outer layer of an erosion resistant material and/or an addi tional intermediate layer of a cushioning material may extend over at least the local outer surfaces of the airflow modifying elements. The additional outer layer and/or addi tional intermediate layer may be terminated, e.g. having a tapered profile, on the outer surface to form a substantially smooth transition. Alternatively, the additional outer lay er and/or additional intermediate layer may extend further along the outer surface to form an additional erosion protection.

The leading edge device may be configured to provide an enhanced leading edge pro tection, thereby increasing the service intervals. This in turn reduces the downtime and increases the AEP. The estimated amount of erosion and wear may be taken into ac count when designing the leading edge device. For example, this may be achieved by increasing the total thickness of the erosion shield between the airflow modifying ele ments and/or forming the body of the airflow modifying elements of an erosion resistant material.

One object of the invention is additionally achieved by a method of installing a leading edge device on a wind turbine blade, the method comprising the steps of:

- providing a leading edge device as described above,

- preparing a leading edge surface on at least blade section of the wind turbine blade for attachment of the leading edge device,

- positioning the leading edge device on said leading edge surface and attaching the leading edge device to said wind turbine blade.

This provides an alternative method of manufacturing a wind turbine blade with a com plex leading edge profile. This eliminates the need for integrating the leading edge pro file during manufacture of the blade shell, thereby saving time and costs. The wind tur bine blade may thus be manufactured with a basic leading edge profile which may be modifying by attachment of the present leading edge device.

The present leading edge device may be attached to the wind turbine blade in a post moulding step or before installation of the wind turbine blade. The present leading edge device may be attached by adhesion, welding, over-lamination or another suitable technique. This allows the aerodynamic performance to be improved and in turn an in creased AEP. According to one embodiment, the method further comprises the step of:

- removing an old leading edge device or an old erosion shield from the wind turbine blade prior to preparing said leading edge surface.

The present method also allows for a more versatile upgrade of existing wind turbine blades compared with conventional methods. This may be done by replacing an exist ing leading edge protection with the present leading edge device or by retrofitting the present leading edge device onto the existing wind turbine blade. This upgrade process may be done when performing a service operation on the wind turbine blade, hence the wind turbine blade can be upgraded without having to demount or replace the wind tur bine blade. This saves time and cost when upgrading existing wind turbine blades.

The present method also allows for an improved way of modifying the leading edge profile and/or the profile of the airflow modifying elements. This may be done by simply attaching the present leading edge device onto an original profile, i.e. basic profile, of the wind turbine blade. Additionally or alternatively, this may be done by replacing a leading edge device having a first profile with a leading edge device having a second profile. For example, the first and second leading edge devices may have different numbers of airflow modifying elements. For example, the airflow modifying elements of the first and second leading edge devices may have different profiles and/or dimen sions. This saves time and cost when modifying the aerodynamic profile of the wind turbine blade.

The present method may include an initial step of removing an old erosion shield or leading edge device from the leading edge surface. This may be done using any known techniques. The leading edge surface may afterwards be prepared for attachment of the present leading edge device. The preparation step may include repairing any cracks or failures in the leading edge surface, e.g. due to environmental erosion or de lamination. The preparation step may further include any suitable surface preparation, such as sanding, chemical cleaning and/or application of a primer, to achieve a good capacity of adherence of the leading edge surface. Said capacity of adherence may in example, but not limited to, be determined by glossiness, roughness and/or surface tension. Optionally, a recess may be formed in the leading edge surface for receiving the lead ing edge surface. The sides and bottom surface of the recess and/or the adjoining blade surface may be prepared for attaching the leading edge surface by adhesion, welding or over-lamination.

Description of drawings

The invention is explained in detail below with reference to embodiments shown in the drawings, in which Fig. 1 shows a wind turbine,

Fig. 2 shows an exemplary embodiment of the wind turbine blade having a base aerodynamic profile,

Fig. 3 shows a leading edge device for attachment to the wind turbine blade with a first embodiment of the first and second edges,

Fig. 4 shows the leading edge device with a second embodiment of the first and second edges,

Fig. 5 shows the leading edge device configured for attachment to the tip end, Fig. 6 shows a second embodiment of the airflow modifying element,

Fig. 7 shows a third embodiment of the airflow modifying element,

Fig. 8 shows an alternative third embodiment of the airflow modifying element,

Fig. 9 shows the wind turbine blade with a number of leading edge extending along the leading edge,

Fig. 10 shows a cross-sectional view of a first embodiment of the erosion shield and the airflow modifying elements,

Fig. 1 1 shows a cross-sectional view of a second embodiment of the erosion shield and the airflow modifying elements,

Fig. 12 shows a cross-sectional view of a third embodiment of the erosion shield and the airflow modifying elements,

Fig. 13 shows a cross-sectional view of a fourth embodiment of the erosion shield and the airflow modifying elements,

Fig. 14 shows a cross-sectional view of a fifth embodiment of the airflow modify ing elements, and

Fig. 15 shows an exemplary method of installing the leading edge device on the wind turbine blade.

List of references 1. Wind turbine

2. Wind turbine tower

3. Nacelle

4. Hub

5. Wind turbine blades

6. Pitch bearing

7. Blade root

8. Tip end

9. Leading edge

10. Trailing edge

1 1. Blade shell

12. Pressure side

13. Suction side

14. Blade root portion

15. Aerodynamic blade portion

16. Transition portion

17. Blade length of wind turbine blade

18. Chord length of wind turbine blade

19. Leading edge device

20. Erosion shield

21. Airflow modifying elements

22. First end

23. Second end

24. First edge

25. Second edge

26. Inner surface

27. Outer surface

28. Serrations

29. Further airflow modifying element

30. Body

31. Inner layer

32. Outer layer

33. Profile

34. Old erosion shield

35. Old leading edge device

36. Leading edge surface 37. Recess

The listed reference numbers are shown in abovementioned drawings where no all ref erence numbers are shown on the same figure for illustrative purposes. The same part or position seen in the drawings will be numbered with the same reference number in different figures.

Detailed description of the drawings

Fig. 1 shows a modern wind turbine 1 comprising a wind turbine tower 2, a nacelle 3 arranged on top of the wind turbine tower 2, and a rotor defining a rotor plane. The na celle 3 is connected to the wind turbine tower 2, e.g. via a yaw bearing unit. The rotor comprises a hub 4 and a number of wind turbine blades 5. Here three wind turbine blades are shown, but the rotor may comprise more or fewer wind turbine blades 5. The hub 4 is connected to a drive train, e.g. a generator, located in the wind turbine 1 via a rotation shaft.

The hub 4 comprises a mounting interface for each wind turbine blade 5. A pitch bear ing unit 6 is optionally connected to this mounting interface and further to a blade root of the wind turbine blade 5.

Fig. 2 shows a schematic view of the wind turbine blade 5 which extends in a longitudi nal direction from a blade root 7 to a tip end 8. The wind turbine blade 5 further extends in a chordwise direction from a leading edge 9 to a trailing edge 10. The wind turbine blade 5 comprises a blade shell 1 1 having two opposite facing side surfaces defining a pressure side 12 and a suction side 13 respectively. The blade shell 1 1 further defines a blade root portion 14, an aerodynamic blade portion 15, and a transition portion 16 between the blade root portion 14 and the aerodynamic blade portion 15.

The blade root portion 14 has a substantially circular or elliptical cross-section (indicat- ed by dashed lines). The blade root portion 14 together with a load carrying structure, e.g. a main laminate combined with a shear web or a box beam, are configured to add structural strength to the wind turbine blade 5 and transfer the dynamic loads to the hub 4. The load carrying structure extends between the pressure side 12 and the suc tion side 13 and further in the longitudinal direction.

The blade aerodynamic blade portion 15 has an aerodynamically shaped cross-section (indicated by dashed lines) designed to generate lift. The cross-sectional profile of the blade shell 1 1 gradually transforms from the circular or elliptical profile into the aerody namic profile in the transition portion 16.

The wind turbine blade 5 has a blade length 17 of at least 35 metres, preferably at least 50 metres, measured in the longitudinal direction. The wind turbine blade 5 further has a chord length 18 as function of the blade length 17 measured in the chordwise direc tion, wherein the maximum chord length is found between the blade aerodynamic blade portion 15 and the transition portion 16.

Fig. 3 shows a leading edge device 19 for attachment to the wind turbine blade 5 which comprises an erosion shield 20 and a number of airflow modifying elements 21. The erosion shield 20 extends from a first end 22 to a second end 23 in a longitudinal direc tion and further from a first edge 24 to a second edge 25 in a circumference direction. The erosion shield 20 has an inner surface 26 facing a leading edge surface (shown in fig. 15) of the wind turbine blade 5 and an opposite facing outer surface 27. The inner surface 26 is shaped to conform to the blade surface of the leading edge area.

The airflow modifying elements 21 project from the outer surface 27 and each have a local outer surface 27’. Each airflow modifying element 21 has a body with an aerody namic profile having a local length, a local width and a local height.

Here, the first and second edges 24, 25 are formed as straight edges extending in the longitudinal direction of the leading edge device 19.

Fig. 4 shows the leading edge device 19 with a second embodiment of the first and second edges 24’, 25’. Here, a number of serrations 28 are distributed along the longi tudinal direction and project from the first and second edges 24’, 25’, respectively, to wards the trailing edge 10. The serrations 28 are integrally formed by the erosion shield 20. The serrations 28 are shaped to improve the airflow over the first and second edg es 24, 25. The leading edge devices 19 of figs. 3 and 4 are configured to be attached to a part of the leading edge 9, preferably at a distance from the tip end 8 or the root end (shown in fig. 2). Fig. 5 shows an alternative position of the leading edge device 19. Here, the leading edge device 19 is configured to be attached to a tip end area. The leading edge device 19 may, for example, be arranged at the tip end 8 and extend towards the root end 7.

Fig. 6 shows a second embodiment of the airflow modifying element 2T of the leading edge device 19. Here, the airflow modifying element 2T extends substantially in the circumference direction from a local first edge 24 to a local second edge 25’. The local thickness of the airflow modifying element 21’ tapers off towards the local first and sec ond edges 24’, 25’, respectively.

The local first edge 24’ is optionally aligned with the first edge 24 of the erosion shield 20. The local first edge 24’ is positioned at a first chordwise length from the leading edge 9. Similarly, the local second edge 25’ is optionally aligned with the second edge 25 of the erosion shield 20. The local second edge 25’ is positioned at a second chordwise length from the leading edge 9.

Here, the local first and second edges 24’, 25’ are aligned in the chordwise direction, but may be offset relative to each other.

Fig. 7 shows a third embodiment of the airflow modifying element 21”, wherein the air flow modifying element 21” form part of a combined airflow modifying element extend ing along a portion of the pressure and suction sides 12, 13. Here, a further airflow modifying element 29 is aligned with the local first edge 24’ of the airflow modifying el ement 21”. Further, another further airflow modifying element 29 is aligned with the lo cal second edge 25’ of the airflow modifying element 21”. The airflow modifying ele ment 21” together with the further airflow modifying elements 29 form the combined air flow modifying element. Thereby, extending the airflow modifying element towards the trailing edge 10.

Here, a further airflow modifying element 29 is arranged on both the pressure and suc tion sides 12, 13. However, the further airflow modifying element 29 may be arranged on only the pressure side 12 or the suction side 13. In an alternative configuration, the further airflow modifying elements 29 form part of the airflow modifying element 21

Fig. 8 shows an alternative third embodiment of the airflow modifying element 21”, wherein the further airflow modifying element 29’ extend over the trailing edge 10 and further along a part of the pressure and suction sides 12, 13. Thereby, forming an air flow modifying element extending around the circumference of the wind turbine blade 5.

Fig. 9 shows the wind turbine blade 5 with a number of leading edge devices 19 ex tending along a portion of the leading edge 9. Here, a continuous leading edge device 19 or an array of leading edge devices 19 are positioned along the leading edge 9.

The leading edge devices 19 are arranged between 20% to 100%, preferably between 40% to 100%, of the blade length measured from the blade root 7.

Fig. 10 shows a cross-sectional view of a first embodiment of the erosion shield 20’ and the airflow modifying elements 2T”. Here, the erosion shield 20’ comprises an inner layer 31 and an outer layer 32. The inner layer 31 extends along the inner surface 26. The airflow modifying elements 2T” are formed by a body 30 having a 3D-profile, as indicated in figs. 3-5, extending in the longitudinal direction, the thickness direction and further in the circumference direction. Here, the bodies 30 are shaped to as a continu ous element forming the outer layer 32 of the erosion shield 30 wherein the body 30 forms a continuous outer surface 27”.

The body 30 may alternatively be shaped to form the inner layer 31 instead.

Fig. 1 1 shows a cross-sectional view of a second embodiment of the erosion shield 20” and the airflow modifying elements 21””. Here, the body 30’ is sandwiched between the outer layer 32’ and the inner layer 31 . The outer layers 32’ extend along the inner layer 31 between the bodies 30’ and further along the local outer surfaces 27’ of each body 30.

Here, the bodies 30’ are shaped apart by a distance to form the airflow modifying ele ments 21””. Fig. 12 shows a cross-sectional view of a third embodiment of the erosion shield 20’” and the airflow modifying elements 21””. Here, the inner layer 31 ^' and the outer layer 32’ extend both over the local outer surfaces 27’ of the bodies 30’.

The body 30’ of the airflow modifying element 21”” is here arranged on the inner sur face 26’ so that it faces the leading edge surface (shown in fig. 15).

Fig. 13 shows a cross-sectional view of a fourth embodiment of the erosion shield 20 and the airflow modifying elements 21. Here, the airflow modifying elements 21 are formed by a body 33 having a 2D-profile, as indicated in figs. 6-8, extending in the thickness direction and further in the circumference direction.

As indicated in figs. 10-14, the leading edge device 19 comprises an array of airflow modifying elements 21 formed by the body 30, 33.

The body 33 has a substantially uniform profile along its local length. For example, the body 33 may have substantially rectangular profile, as indicated in fig. 13. The body 33’ may also have a substantially round profile, e.g. semi-elliptical or semi-circular, as indi cated in fig. 13. The body 33” may also have a substantially triangular profile, as indi cated in fig. 13.

The erosion shield 20 is here formed as a multi-layered erosion shield comprising a number of layers arranged in a stack.

Here, the body of the airflow modifying element 21 is attached to the outer layer 32 of the erosion shield 20.

Fig. 14 shows a cross-sectional view of a fifth embodiment of the airflow modifying el ements 21 . Here, the dimensions of one or more of the airflow modifying elements 21 vary along the local length.

As illustrated, the local thickness of the bodies 33”, 33”’, 33”” may vary from a mini mum local thickness to a maximum local thickness. The dimensions and, optionally, the profile of the airflow modifying elements 21 are thus varied along the length of the wind turbine blade 5. Fig. 15 shows an exemplary method of installing the leading edge device 19 on the wind turbine blade 5. The wind turbine blade 5 is preferably manufactured with a basic leading edge profile, as indicated in fig. 15. Existing wind turbine blades 5 may be provided with an old leading edge protection, such as an erosion shield 34 or a leading edge device 35 with a basic profile, as indi cated in fig. 15(a). When upgrading the wind turbine blade 5, the old erosion shield 34 or leading edge device 35 is removed (indicated by arrow) in an initial step. Afterwards, any damages in the leading edge surface 36 are repaired and the leading edge surface 36 is then prepared for attachment of the leading edge device 19, as indi cated in fig. 15(b).

Finally, the leading edge device 19 is then positioned on the leading edge surface 36 and attached to the wind turbine blade 5, as indicated in fig. 15(c).

If no leading edge protection exists, then any damages in the leading edge surface 36 are repaired and the leading edge surface 36 is then prepared for attachment of the leading edge device 19, as indicated in fig. 15(b). For new wind turbine blades 5, the original leading edge surface 36’ is prepared for at tachment of the leading edge device 19 in a post-moulding process. This may include forming a recess 37 in the leading edge surface 36’. The leading edge device 19 is af terwards at least partly positioned in the recess 37 and subsequently attached to the wind turbine blade 5.

The abovementioned embodiments may be combined in any combinations without de viating from the present invention.