REVERSIBLE SYSTEM FOR DIVIDING AEROGENERATOR BLADES INTO SEVERAL PARTS

Abstract

Aerogenerator blades of several sections or sectors are joined by specifically designed inserts that allow assembly to be carried out at a wind farm, particularly, at the base of a tower. These inserts are disposed both inside and outside of the original blades, in a single piece or several pieces and joined to the blades by any mechanical, physical or material fusion connection. Adhesives and other type of joints can also be used for this purpose.

Description

STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT

Not applicable.

NAMES OF PARTIES TO A JOINT RESEARCH AGREEMENT

Not applicable.

REFERENCE TO AN APPENDIX SUBMITTED ON COMPACT DISC

Not applicable.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention is encompassed within the aerogenerator technology sector, more specifically, the industrial sector that manufactures and assembles aerogenerator blades, and relates to an alternative for assembling aerogenerator blades based on the manufacture of said blades in sections, in such a manner that the final assembly is carried out by means of inserts specifically designed for such a purpose.

2. Description of Related Art Including Information Disclosed Under 37 CFR 1.97 and 37 CFR 1.98.

To date, all blades are formed by joining different components during the workshop manufacturing process but emerging in a single piece from the large molds used for final curing of the assembly. The process for manufacturing and curing the matrix material and adhesives used determines the manufacturing time of the parts. Once the blade is manufactured, the difficulty in storage and transport thereof arises due to its large size. Likewise, the mounting thereof onto the bushing, and the bushing onto the generator axle, is carried out by moving large-sized assemblies, with the ensuing difficulty of assembly and fixing thereof.

The present invention aims to offer a new solution to the previously expounded problems. Different works with the same intention are known, although none of these nor the inventions registered to date have demonstrated their use or capacity to manufacture the blades in several parts and assemble them onsite.

BRIEF SUMMARY OF THE INVENTION

The foundation of the invention is based on the manufacture of blades in sections and assembly thereof, joining the sections at the wind farm at the base of the tower, by means of specifically designed inserts, with all the advantages that this entails.

The main advantages of the present invention are, on one hand, planning the production of the different sectors involved in the manufacture of the blades, without having to depend on the time required to form the whole blade, but rather its constituent parts. On the other hand, it allows storage of the smaller parts, in addition to planning the transport and use of transport means of shorter length and width, considerably expediting the permit process and reducing the terms and costs derived from transporting the blades from the point of manufacture to that of installation. The present invention allows great ease of handling and assembly at the wind farm itself, given that smaller parts must be moved and joined together, which also implies that the blade parts are joined together in a simpler and faster manner, thereby guaranteeing joint correctness. As the joint is detachable, the damaged parts of a blade can be substituted with other new ones without having to replace the whole blade, as at present.

The invention guarantees the use of current molds for the manufacture of blades, allowing the manufacturer's original blade design to be maintained, adding specific components to the blade laminate during the manufacturing process in order to obtain the correct joint between the blade sector and the insert. Specific molds designed to obtain the necessary geometry so that the joint between the insert and the blade sectors is adequate for correct stress transmission may also be introduced.

The joint between the insert and the blade sector may be resolved by means of traditional mechanical, physical or material fusion (solders with and without addition of material) joints or by means of adhesive or other types of joints designed for such purpose.

The blades and inserts may be designed with different apertures, angles, lengths, geometries, thicknesses and with different material qualities and treatments of all kinds (thermal, anti-corrosive, mechanical, superficial, etc.) which may be applied to these in order to fulfill their function. They may also be designed using different materials (metals, alloys, steels, polyamides, technical plastics, aluminum, combinations of these and/or any material both reinforced with fibers or particles of any kind or not reinforced, which may be applied to fulfill their function) in addition to different characteristics such as ductility, malleability, plasticity, elasticity, superficiality, resistance, etc., proposed to improve said function. Likewise, the inserts may be disposed inside or outside of the original blades and may be made of a single piece or of different components and inserts having more than one part disposed for such purpose.

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

For the purpose of complementing the preceding description and helping to better understand the characteristics of the invention, a detailed description of a preferred embodiment, based on a set of drawings that accompany this specification, will be carried out, wherein the following have been represented in a merely indicative and non-limiting manner.

FIG. 1 shows a front elevation view of an aerogenerator blade.

FIG. 2 shows a sectional view along line II-II of FIG. 1.

FIG. 3 shows an exploded perspective view of the insert in one of the blade sectors.

FIG. 4 shows a sectional view along line IV-IV of FIG. 2 during assembly.

FIG. 5 shows a sectional view along line IV-IV of FIG. 2 after assembly.

In the preceding figures, the numerical references correspond to the following parts and elements:

• 1. Sector 1 of blade
• 2. Sector 2 of blade
• 3. Blade
• 4. Insert
• 5. Floating nut
• 6. Inner blade cavity
• 7. External access
• 8. Threaded positioning rod

DETAILED DESCRIPTION OF THE INVENTION

The invention consists, as can be observed in FIGS. 1 and 3, of joining two sectors 1 (1) and 2 (2) of the blade (3), each of said sectors being designed to absorb the cut, flexional, traction and torsion stresses to which they are subjected. The joint is made by means of a central insert (4) specifically designed for said function which offers the adequate characteristics of rigidity, weight and mechanical resistance for blade operation.

As can be observed in FIGS. 2 and 3, the insert (4) must adapt to the inner cavity (6) of the blade, taking the loads that it must bear into account, for which purpose a floating nut (5) is inserted in said insert (4), wherethrough a threaded positioning rod (8) is introduced which, on being rotated in one direction reduces the cross-sectional area of the insert (4), as can be observed in FIG. 4, deforming the insert (4) in such a manner that it may be introduced in the specific inner cavity (6). This same effect can be obtained by means of other systems aimed at reducing the size of the insert to allow introduction thereof into the central core of the blade. Once the insert (4) has been introduced into the corresponding cavity (6), the threaded rod is rotated from the external access (7) of the blade sectors, in such a manner that, by manipulating it in the opposite direction, this insert, having a specific tooth form design, returns to its original position, as can be observed in FIG. 5. The toothing of the insert (4) is coupled to the toothing of the blade sectors, favoring the necessary and adequate rigidity, weight and resistance for blade operation.

This phase of the process could have variations if it is wished to make permanent joints (not detachable), joining the central insert to the blade sectors by means of adhesives, rivets, screws of any type, inner conical seatings and/or any other known means. Likewise, variations could occur in the event of using an element for connection to the blade.

After introducing the central insert, the assembly is reinforced by means of simple inserts at the ends of the specifically designed blade sector joints, as can be observed in FIG. 2 and, finally, the small superficial marks remaining on the blade surface are sealed to enhance aerodynamic behavior.

There are other variants of inserts and blades, as in the case of designs with different apertures, angles, lengths, geometries, thicknesses and different materials, material qualities and characteristics, and treatments of all kinds, disposing the inserts inside or outside of the original blades and made of a single piece or of different components or inserts having more than one part disposed for such purpose, observing the essentiality of the invention, which can be considered as being evident to a person skilled in the art.

The main joint, according to the design of the blade, could occur in areas that do not correspond with the central cavity and, in all cases, could be made both inside and outside of the blade.

Claims

1. Insert for joining together aerogenerator blade sectors, comprising: a tooth profile; anda plurality of floating nuts an interior of said tooth profile.

2. Insert for joining together aerogenerator blade sectors, according to claim 1, being comprised of metal components, alloys, steels, polyamides, technical plastics, composites, aluminiums or combinations thereof.

3. Reversible method for joining together aerogenerator blade sectors, the method comprising the steps of: forming a joint using at least one insert defined in claim 1;deforming the insert to reduce cross-sectional area thereof and disposing the insert inside a blade;inserting the insert within a specific inner cavity of the blade; androtating a threaded rod of the blade from an external access of the blade sectors, wherein manipulating the rod in an opposite direction returns the insert to an original position.

4. Reversible method for joining together aerogenerator blade sectors, according to claim 3, wherein the insert is comprised of a central insert and at least one insert at one of the ends.

5. Reversible method for joining together aerogenerator blade sectors, according to claim 4, wherein a central insert and two inserts at the ends of the joints of the blade sectors are used.

6. Reversible method for joining together aerogenerator blade sectors, according to claim 3, wherein the sectors are cross-sections of the aerogenerator blades.