ROTOR BLADE WITH BELTS COMPRISING PULTRUDED PRODUCTS
20210379842 ยท 2021-12-09
Inventors
Cpc classification
Y02P70/50
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F03D1/0675
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C70/44
PERFORMING OPERATIONS; TRANSPORTING
Y02E10/72
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
B29C70/34
PERFORMING OPERATIONS; TRANSPORTING
B29C70/44
PERFORMING OPERATIONS; TRANSPORTING
B29D99/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for producing a component of a rotor blade, by providing a production mould (2) with a curved support surface (1), at least one flexible pultrudate (4) being laid onto the support surface (1), the at least one flexible pultrudate (4) being covered with a vacuum film (6), a vacuum being generated and the at least one flexible pultrudate (4) being pressed entirely onto the curved support surface (1) of the production mould (2) by the vacuum.
Claims
1. A method for producing a component of a rotor blade, by providing a production mould (2) with a curved support surface (1), at least one flexible pultrudate (4) being laid onto the support surface (1), the at least one flexible pultrudate (4) being covered with a vacuum film (6), a vacuum being generated and the at least one flexible pultrudate (4) being pressed entirely onto the curved support surface (1) of the production mould (2) by the vacuum.
2. The method according to claim 1, characterised in that if the at least one flexible pultrudate (4) is initially straight in a cross-section and while it is pressed by the formation of the vacuum onto the curved support surface (1), it is kept continuously at a temperature below the glass transition temperature (Tg).
3. The method according to claim 1, characterised in that the component is infused with resin (8) and the resin (8) and the at least one pultrudate (4) are cured.
4. The method according to claim 1, characterised in that the at least one pultrudate (4) is curved along a cross-section and along a longitudinal section.
5. The method according to claim 1, characterised in that the at least one pultrudate (4) is heated to a temperature below a glass transition temperature (Tg) and at that temperature is pressed onto the curved support surface (1).
6. The method according to claim 1, characterised in that two to five pultrudates (4) are laid alongside one another and up to ten pultrudates (4) are laid one above the other on the curved support surface (1) and an infusion process is carried out and a girder is produced.
7. Arrangement for producing a component of a rotor blade with a production mould (2) having a curved support surface (1) and at least one flexible pultrudate (4) which lies entirely on the support surface (1) and has a glass transition temperature (Tg) and is at a temperature below the glass transition temperature (Tg).
8. Arrangement according to claim 7, characterised in that a vacuum film (6) is laid over the at least one uncured pultrudate (4).
Description
[0025] The invention is described with reference to an exemplary embodiment in three drawings, in which:
[0026]
[0027]
[0028]
[0029] A curved support surface 1 of a production mould 2 for a girder of a rotor blade is shown in
[0030] The girders according to the invention have a number of pultrudates 4 which can be arranged in the longitudinal direction alongside one another and one above the other. The cross-section of a pultrudate 4 for producing the girder is shown in
[0031] The production mould 2 illustrated in
[0032] Since the rotor blade shell is curved both in cross-section and also in longitudinal section along the support surface of the pultrudate 4, the pultrudate 4 must already incorporate the curvatures in its own shape in order to lie as entirely as possible, at least over a large area on the inner wall of the rotor blade half-shell. Therefore the support surfaces 1 of the production mould 2 of the girder which are illustrated in
[0033] Pultrudates 4 are usually produced in a pultrusion process. For this purpose rovings, which are carbon fibre and/or glass fibre bundles stored on coils, are unrolled alongside one another and one above the other and are drawn alongside one another in the longitudinal direction through a resin bath or surrounded by a liquid resin, which is then heated together with the rovings in a furnace. During the heating the resin cures, and a solid pultrudate 4 is produced which is flexible with difficulty. However, the pultrudates according to the invention are more easily flexible by comparison with the conventional pultrudates. For this purpose, during the process of producing the pultrudate 4, first of all in a conventional manner rovings are unwound from coils, arranged alongside one another and covered with liquid resin. The rovings with the resin are moved through a furnace, wherein, however, the residence time and/or the temperature of the furnace are shortened or lowered respectively by comparison with the conventional curing step, so that the resulting pultrudate is not completely cured. Because the complete pultrudate is not completely cured, thus it is more flexible and softer, it can be used for the production method according to the invention.
[0034]
[0035] According to the invention the incompletely cured pultrudates 4 according to
[0036] The production mould 2 can be heated during the infusion process, so that as a result an additional softening of the pultrudate 4 is possible.
[0037] After the vacuum is produced or simultaneously, resin 8 is infused into the pultrudate structure and the pultrudates 4 are adhered to one another. During subsequent heating the resin 8 is completely cured, and a girder is produced for a rotor blade half-shell, wherein the pultrudates 4 of the girder are optimally adapted to the curvature of the support surface 1 and nevertheless no internal tension is built up in the pultrudates 4 during the infusion process, since the soft pultrudates 4 can curve easily, i.e. without a great application of force against the support surface 1 and no tension or opposing force has to be overcome.
[0038] A longitudinal section through the production mould of
[0039] It is also conceivable that the entire girder is not completely cured, that is to say during the infusion process, by comparison with conventional infusion processes, the temperature of the production mould 2 is raised for a shorter time and/or to a lower curing temperature, so that after the infusion process the girder is not completely cured, but remains soft and, in an analogous manner to the above-mentioned pultrudate 4, is laid into the rotor blade half-shell where in an infusion process it is drawn onto the support surface 1 of the rotor blade half-shell.
LIST OF REFERENCE NUMERALS
[0040] 1 support surface [0041] 2 production mould [0042] 4 pultrudates [0043] 6 vacuum film [0044] 7 space [0045] 8 resin [0046] L longitudinal direction [0047] Tg glass transition temperature