EP1337738B1 - Component, in particular hydraulic component, made of composite material and method for making same - Google Patents
Component, in particular hydraulic component, made of composite material and method for making same Download PDFInfo
- Publication number
- EP1337738B1 EP1337738B1 EP01997621A EP01997621A EP1337738B1 EP 1337738 B1 EP1337738 B1 EP 1337738B1 EP 01997621 A EP01997621 A EP 01997621A EP 01997621 A EP01997621 A EP 01997621A EP 1337738 B1 EP1337738 B1 EP 1337738B1
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- EP
- European Patent Office
- Prior art keywords
- metal
- layer
- fibres
- reinforcing
- fibers
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/026—Impact turbines with buckets, i.e. impulse turbines, e.g. Pelton turbines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/04—Heavy metals
- F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
- F05C2201/0463—Cobalt
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/04—Heavy metals
- F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
- F05C2201/0466—Nickel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
- F05D2230/11—Manufacture by removing material by electrochemical methods
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/12—Light metals
- F05D2300/121—Aluminium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/172—Copper alloys
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/172—Copper alloys
- F05D2300/1723—Nickel-Copper alloy, e.g. Monel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/611—Coating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/614—Fibres or filaments
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/70—Treatment or modification of materials
- F05D2300/702—Reinforcement
Definitions
- the invention relates to a part, such as a component hydraulics, composite material with organic matrix and reinforcing fibers, and to a method of manufacturing such piece.
- Hydraulic component means any organ likely to interact with a water flow and, by example, a Pelton turbine bucket, a director for a flow, a Kaplan turbine blade or a Francis type turbine wheel.
- the invention relates to a part, in particular a hydraulic component made of composite material organic matrix and reinforcing fibers, this piece being at least locally coated with a protective layer metallic or metal-based, characterized in that includes metal or metal-based fibers, the layer of protection or reinforcement being formed by deposit electrolytic on these metal or metal-based fibers.
- the invention it is possible to have a hanging intimacy between the material of the protective layer or reinforcement and the fiber material as far as the couple of material chosen, for the metal fibers or metal base on the one hand and the protective layer on the other on the other hand, is compatible with electrolytic deposition.
- electrolytic deposition probably allows to obtain a chemical bond between the material of the reinforcing fibers and the material of the protective layer, which avoids the risk of inadvertent stalling of the protective layer.
- the rigidity of the fastening obtained does not depend no curvature radii of the room in areas where is affixed the protective or reinforcing layer, which allows to consider deposits on sharp edges, such as median edges of the buckets of a Pelton turbine. of the bending tests have shown that breaking a piece according to the invention takes place by separating the matte or reinforcing fiber fabric and organic matter before the separation between the protective layer and the substrate on which it is affixed.
- the bucket 1 shown in Figures 1 to 3 is intended to be mounted on the rim, not shown, of a turbine wheel Pelton.
- This bucket 1 consists of a first skin 11 forming its intrados and a second skin 12 forming its extrados, these skins being made of composite materials with a matrix based on epoxy resin, polyester, vinylester, urethane, polyamide or poly-ether-ether-ketone and carbon-based reinforcing fibers, for example, on most of their surface. These fibers are presented under form of a fabric impregnated with resin.
- the geometry of the skins 11 and 12 is such that they define between them a volume in which stiffening ribs 13 are arranged.
- a protective layer 15 and reinforcing the edge 14 is provided on the skin 11.
- the layer 15 is formed by electrolytic deposition located on the skin 11.
- skin 11 includes, at level of the edge 14, reinforcing fibers 21 copper then that, in the rest of its surface, the skin 11 is reinforced by carbon fibers.
- the copper reinforcing fibers 21 are woven between them and form a fabric 23 constituting the layer upper or outer skin 11 in the area of the ridge 14, while fabrics 24 of carbon fibers are superimposed in the rest of the skin thickness 11 and under the tissue 23 at the edge 14.
- the fibers 21 are grouped in the vicinity of the outer surface S of the skin 11, in the area of the ridge 14.
- all the reinforcing fibers used at the edge 14 could be copper fibers, in which case several layers of the type of fabric 23 would be superimposed.
- non-woven fiber mats could be used at the place fabrics 23 and 24.
- the metal fibers 21 extend in a single direction of the fabric 23, for example, that they constitute the sons of chain over part of its width, whereas the wires of weft are constituted by carbon threads.
- the sons of carbon weft 22 extend both on a 23A portion of the fabric 23 in which they are woven with threads of chain 21 of copper and 23B parts of the fabric 23 in which they are woven with warp yarns 26 in carbon.
- the outer layer of the skin 11 of the bucket 1 is it continuous, only part of it being suitable for electrolytic deposition.
- the width of Part 23A is determined by width of the layer 15.
- the continuous nature of the fabric 23 ensures a good anchoring of the threads 21 in the structure of the skin 11.
- This bath is maintained at a temperature of about 60 ° C.
- a counter-electrode made of nickel is used and the elements are degrading and a current is applied with a density of approximately 4 A / dm 2 , which makes it possible to obtain on the fabric 23 the formation of the layer 15 essentially with nickel. the resulting layer having a Vickers hardness of the order of 150 HV.
- metal fibers 21 and, on the other hand, the electrolyte bath, that is to say the layer protection or reinforcement 15.
- the invention is not limited to a turbine trough Pelton and can be implemented with a turbine blade Kaplan, with a director, particularly at the level of their respective leading edges, and with a turbine wheel Francis, especially at the leading edges of the blades and at the exposed edges of the belt and ceiling.
- the areas to be protected are areas with low radii of curvature, which is not a problem given the intimate bonding obtained by electrolytic deposition.
- the hanging intimate obtained between the protective layer or reinforcement and the substrate allows to consider supporting elements reported on this layer by deposit said "to plasma ", plasma spray type, PVD (" Power Vapor Deposition “ or physical deposition), CVD ("Chemical Vapor Deposition” or chemical deposit), etc ... Indeed, the elevation localized temperature allowing the deposit is compatible with the nature of the material of the layer, without risk of damage of the piece made of composite materials. This deposit additional with plasma increases the protection thermal, protection against erosion or corrosion, even the mechanical protection.
Abstract
Description
L'invention a trait a une pièce, telle qu'un composant hydraulique, en matière composite à matrice organique et fibres de renfort, et à un procédé de fabrication d'une telle pièce.The invention relates to a part, such as a component hydraulics, composite material with organic matrix and reinforcing fibers, and to a method of manufacturing such piece.
Par composant hydraulique, on entend tout organe susceptible d'interagir avec un écoulement d'eau et, par exemple, un auget de turbine de type Pelton, une directrice pour un écoulement, une pale de turbine de type Kaplan ou une roue de turbine de type Francis.Hydraulic component means any organ likely to interact with a water flow and, by example, a Pelton turbine bucket, a director for a flow, a Kaplan turbine blade or a Francis type turbine wheel.
Il est connu, par exemple de WO-A-99/49 213 ou de EP-A-0 900 283 de réaliser les augets d'une roue de turbine Pelton en matériau plastique composite. En effet, les matériaux composites à matrice organique possèdent de bonnes propriétés mécaniques dues, pour l'essentiel, au tissage des fibres de renfort. Toutefois, ces matériaux sont difficilement exploitables lorsqu'ils travaillent dans un environnement où ils sont soumis à de l'abrasion, à des chocs ou à de l'érosion par des éléments solides présents, par exemple, dans le flux dans lequel ils baignent. Par exemple, dans le cas d'une turbine Pelton utilisée dans une chute dont l'eau est fortement chargée en matières minérales, l'endommagement de la matrice organique et des fibres de renfort en carbone est très rapide, de sorte que la durée de vie des augets est faible.It is known, for example from WO-A-99 / 49,213 or from EP-A-0 900 283 to make the buckets of a Pelton turbine wheel made of composite plastic material. Indeed, the materials Organic matrix composites have good properties mechanical forces due, for the most part, to the weaving of reinforcement. However, these materials are difficult to exploit when they work in an environment where they are subjected to abrasion, shock or erosion by solid elements present, for example, in the flow in which they bathe. For example, in the case of a turbine Pelton used in a fall whose water is strongly loaded with mineral matter, the damage of the matrix organic and carbon fiber reinforcements is very fast, so that the lifespan of the buckets is low.
Des problèmes analogues se posent avec d'autres pièces qui sont soumises à des conditions d'utilisation difficiles.Similar problems arise with other parts which are subject to difficult conditions of use.
Il est connu de tenter de protéger de telles pièces ou composants en appliquant une couche de protection ou de renforcement à base de métal sur de telles pièces. Les dépôts obtenus ont une adhérence résultant, pour l'essentiel, de la différence d'énergie de surface entre le matériau constitutif de la pièce et celui constitutif de la couche de protection. En pratique, ceci s'avère insuffisant et un risque important de désolidarisation intempestive de la couche de protection par rapport à la pièce sur laquelle elle est appliquée existe, avec des risques d'endommagement d'une installation industrielle et une usure alors très rapide de la pièce en matière composite. En particulier, un tel type de dépôt n'est pas applicable à des composants hydrauliques.It is known to attempt to protect such pieces or components by applying a protective layer or metal-based reinforcement on such parts. Deposits obtained have an adhesion resulting, for the most part, from the difference in surface energy between the constituent material of the part and that constituting the protective layer. In practice, this is insufficient and a significant risk inadvertent disconnection of the protective layer relative to the part on which it is applied exists, with the risk of damage to an industrial plant and a very fast wear of the piece of material composite. In particular, such a type of deposit is not applicable to hydraulic components.
C'est à ces problèmes qu'entend plus particulièrement remédier l'invention en proposant une pièce en matière composite qui est protégée efficacement contre les chocs et l'abrasion.It is these problems that are particularly remedy the invention by proposing a piece of composite that is effectively protected against shocks and abrasion.
Dans cet esprit, l'invention concerne une pièce, notamment un composant hydraulique, en matière composite à matrice organique et fibres de renfort, cette pièce étant revêtue au moins localement d'une couche de protection métallique ou à base de métal, caractérisée en ce qu'elle comprend des fibres métalliques ou à base de métal, la couche de protection ou de renforcement étant formée par dépôt électrolytique sur ces fibres métalliques ou à base de métal.In this spirit, the invention relates to a part, in particular a hydraulic component made of composite material organic matrix and reinforcing fibers, this piece being at least locally coated with a protective layer metallic or metal-based, characterized in that includes metal or metal-based fibers, the layer of protection or reinforcement being formed by deposit electrolytic on these metal or metal-based fibers.
Grâce à l'invention, il est possible d'avoir un accrochage intime entre la matière de la couche de protection ou de renforcement et la matière des fibres dans la mesure où le couple de matériau choisi, pour les fibres métalliques ou à base de métal d'une part et la couche de protection d'autre part, est compatible avec un dépôt électrolytique. En fait, le dépôt électrolytique permet probablement d'obtenir une liaison chimique entre le matériau des fibres de renfort et le matériau de la couche de protection, ce qui évite les risque de décrochage intempestif de la couche de protection. En particulier, la rigidité de l'accrochage obtenue ne dépend pas des rayons de courbure de la pièce dans les zones où est apposée la couche de protection ou de renforcement, ce qui permet d'envisager des dépôts sur des arêtes vives, telles que des arêtes médianes des augets d'une turbine Pelton. Des essais de flexion ont permis de montrer que la rupture d'une pièce conforme à l'invention a lieu par désolidarisation du mat ou tissu de fibres de renfort et de la matière organique avant la séparation entre la couche de protection et le substrat sur lequel elle est apposée.Thanks to the invention, it is possible to have a hanging intimacy between the material of the protective layer or reinforcement and the fiber material as far as the couple of material chosen, for the metal fibers or metal base on the one hand and the protective layer on the other on the other hand, is compatible with electrolytic deposition. In fact, electrolytic deposition probably allows to obtain a chemical bond between the material of the reinforcing fibers and the material of the protective layer, which avoids the risk of inadvertent stalling of the protective layer. In particular, the rigidity of the fastening obtained does not depend no curvature radii of the room in areas where is affixed the protective or reinforcing layer, which allows to consider deposits on sharp edges, such as median edges of the buckets of a Pelton turbine. of the bending tests have shown that breaking a piece according to the invention takes place by separating the matte or reinforcing fiber fabric and organic matter before the separation between the protective layer and the substrate on which it is affixed.
Selon des aspects avantageux de l'invention, la pièce incorpore une ou plusieurs des caractéristiques suivantes :
- Les fibres métalliques ou à base de métal sont disposées, pour l'essentiel, au voisinage de la surface de la pièce destinée à être revêtue de la couche de protection de renforcement. En effet, c'est au niveau de la surface de la pièce qui constitue le substrat que doit avoir lieu l'accrochage.
- Le matériau des fibres métalliques ou à base de métal comprend du cuivre, de l'alumimium, ou un alliage de ces métaux et/ou d'autres éléments métalliques.
- Le matériau de la couche de protection ou de renforcement comprend du nickel, du cobalt, du cuivre, d'autres éléments métalliques et/ou des alliages de ces éléments.
- La pièce en question est un composant hydraulique.
- The metal or metal-based fibers are essentially disposed in the vicinity of the surface of the part to be coated with the reinforcing protective layer. Indeed, it is at the surface of the part that constitutes the substrate that must occur the attachment.
- The material of the metal or metal-based fibers comprises copper, alumimium, or an alloy of these metals and / or other metallic elements.
- The material of the protective or reinforcing layer comprises nickel, cobalt, copper, other metallic elements and / or alloys of these elements.
- The part in question is a hydraulic component.
L'invention concerne également un procédé de fabrication d'une pièce telle que précédemment décrite et, plus spécifiquement un procédé qui comprend des étapes consistant à :
- utiliser, dans certaines zones au moins de la pièce, des fibres métalliques ou à base de métal et
- procéder à un dépôt électrolytique de la couche de protection ou de renforcement sur ces fibres métalliques ou à base de métal.
- use, in at least some areas of the room, metal or metal-based fibers and
- electrolytically depositing the protective or reinforcing layer on these metal or metal-based fibers.
Selon des aspects avantageux de l'invention, le procédé incorpore une ou plusieurs des caractéristiques suivantes :
- Il consiste à isoler les fibres de renfort de la pièce située dans des zones autres que celles incluant des fibres métalliques ou à base de métal avant de procéder au dépôt électrolytique. Ceci permet de définir avec une bonne précision la géométrie de la couche de protection ou de renforcement. On peut en particulier prévoir d'isoler les fibres, autres que les fibres métalliques ou à base de métal, par application d'un vernis isolant.
- On applique, par un dépôt de type "à plasma", un élément métallique sur la couche de protection ou de renforcement après son dépôt. Cet aspect de l'invention tire parti du fait que l'accrochage obtenu entre la couche précitée et la pièce ou substrat est suffisamment intense pour permettre de supporter des éléments rapportés.
- On utilise, pour le bain électrolytique, une solution de composés métalliques incluant du nickel à une température d'environ 60°C avec une contre-électrode à base de nickel et une densité de courant de l'ordre de 4 A/dm2, alors que les fibres de renfort sur lesquelles on effectue le dépôt sont réalisées dans un matériau comprenant du cuivre.
- It consists of isolating the reinforcing fibers from the part located in areas other than those including metal or metal-based fibers before electrolytic deposition. This makes it possible to define with good accuracy the geometry of the protective layer or reinforcement. In particular, it is possible to isolate the fibers, other than the metal or metal-based fibers, by applying an insulating varnish.
- A "plasma" type deposit is applied to a metal element on the protective or reinforcing layer after it has been deposited. This aspect of the invention takes advantage of the fact that the hooking obtained between the aforementioned layer and the part or substrate is sufficiently intense to allow to support inserts.
- For the electrolytic bath, a solution of metal compounds including nickel at a temperature of about 60 ° C with a nickel-based counter electrode and a current density of about 4 A / dm 2 is used . while the reinforcing fibers on which the deposition is performed are made of a material comprising copper.
L'invention sera mieux comprise et d'autres avantages de celle-ci apparaítront plus clairement à la lumière de la description qui va suivre de deux modes de réalisation d'un composant hydraulique conforme à son principe, donnée uniquement à titre d'exemple et faite en référence aux dessins annexés dans lesquels :
- la figure 1 est une vue en perspective éclatée d'un auget de turbine Pelton conforme à l'invention ;
- la figure 2 est une vue éclatée et à plus grande échelle du détail II à la figure 1, lors d'une première étape de fabrication de l'auget de la figure 1 ;
- la figure 3 est une coupe selon la ligne III-III à la figure 1, lors d'une seconde étape de fabrication de cet auget et
- la figure 4 est une vue en plan d'un tissu de fibres de renfort utilisé dans un auget conforme à un second mode de réalisation de l'invention.
- Figure 1 is an exploded perspective view of a Pelton turbine bucket according to the invention;
- Figure 2 is an exploded view and on a larger scale of the detail II in Figure 1, during a first step of manufacturing the bucket of Figure 1;
- FIG. 3 is a section along the line III-III in FIG. 1, during a second manufacturing step of this bucket and
- Figure 4 is a plan view of a reinforcing fiber fabric used in a bucket according to a second embodiment of the invention.
L'auget 1 représenté aux figures 1 à 3 est destiné à être
monté sur la jante non représentée d'une roue de turbine
Pelton. Cet auget 1 est constitué d'une première peau 11
formant son intrados et d'une seconde peau 12 formant son
extrados, ces peaux étant réalisées en matériaux composites
avec une matrice à base de résine epoxyde, polyester,
vinylester, uréthane, polyamide ou poly-ether-ether-cétone et
des fibres de renfort à base de carbone, par exemple, sur
l'essentiel de leur surface. Ces fibres se présentent sous
forme d'un tissu imprégné de résine. La géométrie des peaux
11 et 12 est telle qu'elles définissent entre elles un volume
dans lequel sont disposées des nervures de rigidification 13.The
On note 14 l'arête médiane de l'auget 1 qui est formée
par la peau 11. Cette arête est soumise à des efforts de
friction intenses et variables selon la qualité de l'eau
utilisée pour faire tourner la turbine Pelton. Cette arête est
également soumise à des chocs car l'eau peut être chargée en
débris de taille relativement importante.We note 14 the median edge of the
Conformément à l'invention, une couche 15 de protection
et de renforcement de l'arête 14 est prévue sur la peau 11.According to the invention, a
La couche 15 est formée par un dépôt électrolytique
localisé sur la peau 11.The
Pour que ce dépôt conduise à un accrochage intime de la
couche 15 sur l'arête 14, et comme il ressort plus particulièrement
des figures 2 et 3, où l'écartement des fibres est
exagéré par rapport à la réalité, la peau 11 comprend, au
niveau de l'arête 14, des fibres de renfort 21 en cuivre alors
que, dans le reste de sa surface, la peau 11 est renforcée par
des fibres de carbone.For this deposit to lead to an intimate collision of the
En fait, les fibres de renfort en cuivre 21 sont tissées
entre elles et forment un tissu 23 constituant la couche
supérieure ou externe de la peau 11 dans la zone de l'arête
14, alors que des tissus 24 de fibres de carbone sont superposés
dans le reste de l'épaisseur de la peau 11 et sous le
tissu 23 au niveau de l'arête 14. Ainsi, les fibres 21 sont
regroupées au voisinage de la surface externe S de la peau 11,
dans la zone de l'arête 14.In fact, the
Selon une variante non représentée de l'invention,
l'ensemble des fibres de renfort utilisé au niveau de l'arête
14 pourrait être des fibres de cuivre, auquel cas plusieurs
couches du type du tissu 23 seraient superposées.According to a not shown variant of the invention,
all the reinforcing fibers used at the
Selon une autre variante non représentée de l'invention,
des mats de fibres non tissées pourraient être utilisés à la
place des tissus 23 et 24.According to another variant not shown of the invention,
non-woven fiber mats could be used at the
Comme représenté à la figure 4 pour un second mode de
réalisation, il est également possible de prévoir que les
fibres métalliques 21 s'étendent selon une seule direction du
tissu 23, par exemple, qu'elles en constituent les fils de
chaíne sur une partie de sa largeur, alors que les fils de
trame sont constitués par des fils de carbone. Les fils de
trame en carbone 22 s'étendent à la fois sur une partie 23A
du tissu 23 dans laquelle ils sont tissés avec des fils de
chaíne 21 en cuivre et sur des parties 23B du tissu 23 dans
lesquelles ils sont tissés avec des fils de chaíne 26 en
carbone. Ainsi, la couche externe de la peau 11 de l'auget 1
est-elle continue, une partie seulement de celle-ci étant
adaptée au dépôt électrolytique. Dans ce cas, la largeur de
la partie 23A est déterminée en fonction de la largeur
souhaitée de la couche 15. Le caractère continu du tissu 23
assure un bon ancrage des fils 21 dans la structure de la peau
11.As shown in FIG. 4 for a second mode of
realization, it is also possible to foresee that the
A la figure 4, l'écartement des fibres est également exagéré pour améliorer la compréhension du dessin.In FIG. 4, the fiber spacing is also exaggerated to improve understanding of the drawing.
Lorsque la peau 11 a été moulée, on dépose sur les
parties 16 de cette peau ne comprenant que des fibres de
carbone 22, à savoir les bandes 24A dans le premier mode de
réalisation ou les parties 23B dans le second, une couche 25
de vernis isolant, avant de nettoyer et de dégraisser les
couches de tissus 23 comprenant des fibres 21 et de plonger
la peau 11 dans un bain de composés métalliques avec la
répartition suivante :
Ce bain est maintenu à une température d'environ 60°C.
On utilise une contre-électrode en nickel et des éléments
dépassivants et on applique un courant avec une densité
d'environ 4 A/dm2, ce qui permet d'obtenir sur le tissu 23 la
formation de la couche 15 essentiellement avec du nickel, la
couche obtenue ayant une dureté Vickers de l'ordre de 150 HV.This bath is maintained at a temperature of about 60 ° C. A counter-electrode made of nickel is used and the elements are degrading and a current is applied with a density of approximately 4 A / dm 2 , which makes it possible to obtain on the
Des résultats satisfaisants ont également été obtenus avec des ions cobalt en solution dans le bain précité, auquel cas le dépôt obtenu est de type Ni-Co.Satisfactory results were also obtained with cobalt ions in solution in the aforementioned bath, to which case the deposit obtained is Ni-Co type.
Bien entendu, d'autres couples de métaux peuvent être
envisagés pour, d'une part, les fibres métalliques 21 et,
d'autre part, le bain d'électrolyte, c'est-à-dire la couche
de protection ou de renfort 15.Of course, other pairs of metals can be
considered for, on the one hand,
On peut notamment prévoir d'utiliser les matériaux suivants :
- pour les fibres métalliques : cuivre, aluminium, alliages de ces métaux ou d'autres éléments métalliques
- pour la couche de protection ou de renforcement : cuivre, nickel, cobalt ou autres éléments métalliques ou alliages de ces éléments.
- for metal fibers: copper, aluminum, alloys of these metals or other metallic elements
- for the protective or reinforcing layer: copper, nickel, cobalt or other metallic elements or alloys of these elements.
L'invention n'est pas limitée à un auget de turbine Pelton et peut être mise en oeuvre avec une pale de turbine Kaplan, avec une directrice, notamment au niveau de leurs bords d'attaque respectifs, et avec une roue de turbine Francis, notamment au niveau des bords d'attaque des aubes et au niveau des bords exposés de la ceinture et du plafond. Dans tous les cas, les zones à protéger sont des zones avec de faibles rayons de courbure, ce qui n'est pas gênant compte tenu de l'accrochage intime obtenu par dépôt électrolytique.The invention is not limited to a turbine trough Pelton and can be implemented with a turbine blade Kaplan, with a director, particularly at the level of their respective leading edges, and with a turbine wheel Francis, especially at the leading edges of the blades and at the exposed edges of the belt and ceiling. In In all cases, the areas to be protected are areas with low radii of curvature, which is not a problem given the intimate bonding obtained by electrolytic deposition.
D'autres pièces mécaniques peuvent être réalisées grâce à l'invention, telles que par exemple des ailettes de turbine.Other mechanical parts can be realized thanks to to the invention, such as for example turbine blades.
Quel que soit le type de la pièce considérée, l'accrochage intime obtenu entre la couche de protection ou de renforcement et le substrat permet d'envisager de supporter des éléments rapportés sur cette couche par dépôt dit "à plasma", de type plasma spray, PVD ("Power Vapor Deposition" ou dépôt par voie physique), CVD ("Chemical Vapor Deposition" ou dépôt par voie chimique), etc ... En effet, l'élévation localisée de température permettant le dépôt est compatible avec la nature du matériau de la couche, sans risque d'endommagement de la pièce en matériaux composites. Ce dépôt supplémentaire avec plasma permet d'augmenter la protection thermique, la protection contre l'érosion ou la corrosion, voire la protection mécanique.Whatever the type of the part considered, the hanging intimate obtained between the protective layer or reinforcement and the substrate allows to consider supporting elements reported on this layer by deposit said "to plasma ", plasma spray type, PVD (" Power Vapor Deposition " or physical deposition), CVD ("Chemical Vapor Deposition" or chemical deposit), etc ... Indeed, the elevation localized temperature allowing the deposit is compatible with the nature of the material of the layer, without risk of damage of the piece made of composite materials. This deposit additional with plasma increases the protection thermal, protection against erosion or corrosion, even the mechanical protection.
Claims (10)
- Part, especially a hydraulic component, made of a composite comprising an organic matrix and reinforcing fibres, the said part being plated at least locally with a metal or metal-based protective layer, characterized in that it comprises metal or metal-based fibres (21), the said layer (15) being formed by electroplating on the said metal or metal-based fibres.
- Part according to Claim 1, characterized in that the said metal or metal-based fibres (21) are placed, for the most part, near that surface (S) of the said part (1) which is intended to be plated with the said layer (15).
- Part according to one of the preceding claims, characterized in that the material of the said metal or metal-based fibres (21) comprises copper or aluminium, or an alloy of these metals and/or of other metallic elements.
- Part according to one of the preceding claims, characterized. in that the material of the said layer (15) comprises nickel, cobalt or copper, or other metallic elements and/or alloys of these elements.
- Part according to one of the preceding claims, characterized in that it is a hydraulic component (1).
- Process for manufacturing a part, such as a hydraulic component, the said part being of a composite comprising an organic matrix and reinforcing fibres and plated, at least locally, with a metal or metal-based protective or reinforcing layer, characterized in that it comprises the steps consisting in:using, at least in certain regions (14) of the said part (1), metal or metal-based fibres (21); andelectroplating the said metal or metal-based fibres with the said layer (15).
- Process according to Claim 6, characterized in that it comprises a step consisting in insulating the reinforcing fibres (22) of the said part (1) which are in regions (16) other than that or those (14) including metal or metal-based fibres (21), before they are electroplated with the said layer (15).
- Process according to Claim 7, characterized in that it comprises a step consisting in insulating the said fibres (22) other than the metal or metal-based fibres (21) by applying an insulating varnish (25).
- Process according to one of Claims 6 to 8, characterized in that it comprises a step consisting in applying, by "plasma"-type deposition, a metallic element on. the said layer (15) after the electroplating with the said. layer.
- Process according to one of Claims 6 to 9,. characterized in that it consists in using, for the electrolytic bath, a solution of nickel-containing metal compounds at a temperature of about 60°C, with a nickel counterelectrode and a current-density of around 4 A/dm2, while the reinforcing fibres (21) on which the deposit is formed are made of a copper-containing material.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0015292 | 2000-11-27 | ||
FR0015292A FR2817284B1 (en) | 2000-11-27 | 2000-11-27 | PIECE, IN PARTICULAR HYDRAULIC COMPONENT, IN COMPOSITE MATERIAL AND METHOD FOR MANUFACTURING SUCH A PART |
PCT/FR2001/003733 WO2002042609A2 (en) | 2000-11-27 | 2001-11-26 | Component, in particular hydraulic component, made of composite material and method for making same |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1337738A2 EP1337738A2 (en) | 2003-08-27 |
EP1337738B1 true EP1337738B1 (en) | 2004-05-26 |
Family
ID=8856914
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01997621A Expired - Lifetime EP1337738B1 (en) | 2000-11-27 | 2001-11-26 | Component, in particular hydraulic component, made of composite material and method for making same |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP1337738B1 (en) |
AU (1) | AU2002222051A1 (en) |
FR (1) | FR2817284B1 (en) |
NO (1) | NO20032365L (en) |
PE (1) | PE20020878A1 (en) |
PT (1) | PT1337738E (en) |
WO (1) | WO2002042609A2 (en) |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1219715B (en) * | 1988-06-14 | 1990-05-24 | Riva Calzoni Spa | PELTON TYPE HYDRAULIC TURBINE IMPELLER, AT REDUCED PRODUCTION COSTS |
PT900283E (en) | 1995-12-12 | 2002-09-30 | Akzo Nobel Nv | 11ALFA-HYDROXYLACAO MICROBIAL STEROIDS |
FR2776341B1 (en) * | 1998-03-23 | 2000-06-09 | Gec Alsthom Neyrpic | TURBINE WHEEL AND PELTON-TYPE TURBINE EQUIPPED WITH SUCH A WHEEL |
-
2000
- 2000-11-27 FR FR0015292A patent/FR2817284B1/en not_active Expired - Fee Related
-
2001
- 2001-11-26 EP EP01997621A patent/EP1337738B1/en not_active Expired - Lifetime
- 2001-11-26 AU AU2002222051A patent/AU2002222051A1/en not_active Abandoned
- 2001-11-26 PT PT01997621T patent/PT1337738E/en unknown
- 2001-11-26 WO PCT/FR2001/003733 patent/WO2002042609A2/en not_active Application Discontinuation
- 2001-11-27 PE PE2001001183A patent/PE20020878A1/en not_active Application Discontinuation
-
2003
- 2003-05-26 NO NO20032365A patent/NO20032365L/en not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
NO20032365D0 (en) | 2003-05-26 |
NO20032365L (en) | 2003-07-18 |
PT1337738E (en) | 2004-10-29 |
FR2817284B1 (en) | 2003-02-14 |
EP1337738A2 (en) | 2003-08-27 |
AU2002222051A1 (en) | 2002-06-03 |
WO2002042609A2 (en) | 2002-05-30 |
FR2817284A1 (en) | 2002-05-31 |
WO2002042609A3 (en) | 2003-01-09 |
PE20020878A1 (en) | 2002-09-27 |
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