EP1537950A1 - Protection mask for the surface treatment of blades for turbine engines - Google Patents

Protection mask for the surface treatment of blades for turbine engines Download PDF

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Publication number
EP1537950A1
EP1537950A1 EP04300818A EP04300818A EP1537950A1 EP 1537950 A1 EP1537950 A1 EP 1537950A1 EP 04300818 A EP04300818 A EP 04300818A EP 04300818 A EP04300818 A EP 04300818A EP 1537950 A1 EP1537950 A1 EP 1537950A1
Authority
EP
European Patent Office
Prior art keywords
mask
mask according
foot
blades
blade
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.)
Granted
Application number
EP04300818A
Other languages
German (de)
French (fr)
Other versions
EP1537950B1 (en
Inventor
Lhocine Oussaada
Thierry Labrousse
Thierry Belkheir
Claude Colas
Habib Mehdaoui
Christian Polis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA Moteurs SA
SNECMA SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SNECMA Moteurs SA, SNECMA SAS filed Critical SNECMA Moteurs SA
Priority to EP07113930A priority Critical patent/EP1911549B1/en
Publication of EP1537950A1 publication Critical patent/EP1537950A1/en
Application granted granted Critical
Publication of EP1537950B1 publication Critical patent/EP1537950B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24CABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
    • B24C1/00Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods
    • B24C1/04Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods for treating only selected parts of a surface, e.g. for carving stone or glass
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/01Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B12/00Arrangements for controlling delivery; Arrangements for controlling the spray area
    • B05B12/16Arrangements for controlling delivery; Arrangements for controlling the spray area for controlling the spray area
    • B05B12/20Masking elements, i.e. elements defining uncoated areas on an object to be coated

Definitions

  • the invention relates to the protection of turbomachine blade surfaces prior to a partial surface with a character abrasive or simply to surfaces not to be treated. She also relates to the application of a surface protection for any part mechanics to be subjected to a similar surface treatment,
  • a turbine engine blade 10 here compressor or welding turbojet, is a pay 11 having an intrados face and an extrados face 19, a stilt 12 and a foot 13 slotting into an axial cavity formed in the axis of the central disc of the support (not shown).
  • a platform 14 separates the blade 11 from the stilt 12.
  • the central disk thus carries a certain number of vanes whose blades are all kept equidistant from each other, in particular by fins 15 located on a median portion of each face of the blades and of which, for two adjacent fins of two neighboring blades, the ends are in contact.
  • the surface treatment of blade 10 comprises a first treatment E1 of the surface by sandblasting to increase the roughness, in preparation for a second said metallization step E2 with thermal spray deposition.
  • a first treatment E1 of the surface by sandblasting to increase the roughness in preparation for a second said metallization step E2 with thermal spray deposition.
  • a plasma torch either of a copper alloy, for example Cu - Ni - In (copper - nickel - indium), whose ductility makes it possible to dampen the vibrations of the motor by operation at the blade contacts with the central disk, either of tungsten carbide, for example WC-Co (tungsten carbide-cobalt) whose hardness makes it possible to avoid the wear caused by the friction between adjacent fins.
  • the plasma torch projects the alloy coating at high speed and (more than 2500 ° K.) on the surface to be treated for get his hang.
  • Steps E1 are very abrasive and steps E2 are undesirable in outside the surfaces to be treated. They require in the case of the treatment fins, to interpose a protection between the tools of sandblasting and / or the plasma torches and the faces 19 of the blades 10 so as to subtract these from their effects. More specifically, only surfaces 17 of the ends of fins 15 to be put into contact with those 17 of the other fins of the neighboring blades, are submitted, during manufacture, to the surface treatments above. In in addition to the two faces 19 of the blade 11 have helical surfaces, very precise geometry, which must be protected.
  • the operators of these operations are subject to particularly due to the sustained attention required for their execution; they are also at risk of musculoskeletal disorders (TMS) consecutive to the realization of repetitive actions.
  • TMS musculoskeletal disorders
  • the applicant proposes a protective mask for the surface treatment of surfaces of a turbomachine blade having a foot and possibly fins, disposed around said surfaces while resisting the effects of surface treatment, while constituting a dismountable tool and reusable, characterized in that said surfaces being located either on the foot of the dawn is at the end of the fin, it is composed of minus a piece matching the shape of the foot or fins respectively, and having lights revealing said surfaces to be treated,
  • the surface treatment comprises a sandblasting step and / or a step of metallization.
  • Tooling means a part or a set of parts at least partly rigid whose shape and materials are suitable for masking parts of surfaces to be protected. Tooling materials are also able to withstand the operational environment of operations E1 and E2. Thanks to the tooling of the invention, all operations are eliminated. manual application of adhesive tape, and the masking is perfectly repetitive.
  • the protective mask is provided to withstand the thermal effects of surface treatment, here a plasma deposit.
  • step E2 requiring mechanical treatment beforehand
  • the protective mask of step E1 is of a material resistant to the abrasive action of sanding.
  • the protective mask is made of stainless steel or silicone material or polymer material.
  • the mask can be used both for sanding and for plasma deposit, and can be reused for a series of turbomachinery.
  • Figure 2 shows the lower part of a compressor blade of which we see the blade 11, the platform 14 and the foot 13. It is here in shape dovetail and rectilinear (non-exhaustive case, quoted example).
  • a 13R coating located in areas that are in contact with flanks of the cell.
  • a mask 100 which espouses the shape of the dawn stake in part, and can be set up by simple embedding.
  • the mask 100 advantageously made of stainless steel, has a determined thickness.
  • a 100R window is provided in this mask, on each side of the foot. The shape and dimensions of windows depend on those of the 13R coating that is to be applied by the plasma torch. This 13R coating is located on both pile surfaces. who will be in contact with the disk on the turbine engine.
  • the walls of the window are also perpendicular to this surface.
  • the window allows the passage of molten metal particles during the metallization operation with the plasma torch.
  • This arrangement has the advantage that the particles molten metal from the plasma torch that are not directed the axis of the window are deposited on the mask in the bordering area window 100R without being reflected inward. These particles do not so do not disturb the formation layer by rebound. After of a layer of desired thickness, the mask is removed.
  • the 13R coating has exactly the shape defined by that of the window it It is not necessary to carry out a retouching operation.
  • the mask is put back into service for the treatment of other blades if the Metallic area at the edge of the window is not too thick.
  • the mask can be so used several times before requiring a fitness by "demetallization" of the area bordering the window.
  • a such operation of restoring the mask is advantageously carried out by chemical techniques known to man of the job.
  • Such a mask also has the advantage of allowing the treatment of several blades at the same time.
  • a groove 110 is provided in the bottom wall of the mask to allow then to apply a alignment bar 43.
  • FIG. 3 shows a mounting for the treatment of some dawns. We assemble the blades equipped with their mask protection 100 on a single tool 40.
  • the tool 40 comprises a frame 42 on which the blades have been fixed, blade in down, so as to present the masks on the top. 100R windows are visible.
  • a bar 43 connects the masks 100 by the grooves 110. Thanks to this bar you can precisely align the masks one by one compared to others.
  • Flanges 41 are placed along the row of masks so as to cover and protect the platforms of the blades.
  • FIGS. 4A and 4B show a masking device adapted to blades with a curvilinear foot, such as blades of blower size.
  • a mask 100 ' protection device comprising, fixed on a base 132, a frame 125 of material silicone or polymer material arranged to be able to be mounted in fitting the foot 13 of the blade 11 while allowing to appear, through lights 124 surfaces 18 to be treated.
  • the frame comprises two half-shells 121 matching the shapes of the above surface, made according to the same plans that made it possible the realization.
  • These two half-shells 121 are assembled by locks 123 removable, for example fitting themselves in the two half-shells 121, and can therefore be dismantled to remain fit for a new editing and remain available for the treatment of another dawn.
  • a mask 100 "'of protection comprising, fixed on a base 132 ", four supports 127 arranged to support two spacers 126, all made of stainless steel, now payroll 11 and two masks 128, stainless steel, now and covering the foot 13 of the blade 11, on either side of the foot, while revealing, through lights 131 surfaces 18 to be treated.
  • the periphery lights 131 is lined with tabs 129 limiting this extent to will.
  • the position of the tabs 129 is adjustable by sliding on the masks 128 and is held there by clamping screws 130.
  • the tabs 129 limit only the length lights 131 but the same device is possible also in width, both devices can easily be simultaneously.
  • FIG. 5 shows an embodiment of the invention corresponding to the treatment of the fins of the dawn.
  • a mask 239 of protection comprising two half-shells 233, matches the shape of the fins according to a chimney 234 and faces 19 adjacent thereto. These forms are directly deduced from the plane of dawn 10.
  • the two half-shells 233 are assembled together on the surface to be protected by the means of four clips 236, for example stainless spring blades embedding in holes (not visible in the figure) provided for this purpose in the mask 239.
  • the mask in this case is made of silicone material, this material is both resistant to sanding mechanics and heat treatment of metallization.
  • the two half-shells 233 reveal the surfaces of the ends of fins 17 to be treated through lights 235 so that these ends remain sufficiently clear of the mask of some height "e".
  • the mask 239 is used both for sandblasting and for plasma deposition. is still reused a number of times,
  • the present invention is not limited to the embodiments represented. It encompasses all variants available to humans of career.

Abstract

Mask protecting turbine blade surfaces during treatment by sand blasting and plasma-metallization. The surfaces to be protected are surfaces either on transverse fins (15, 17) of the turbine blade (10) or surfaces (18) at its root. The mask comprises a section (100) following the appropriate contours and including apertures opening over surfaces to be treated.

Description

L'invention concerne la protection de surfaces d'aubes de turbomachines en préalable à un de surface partiel présentant un caractère abrasif ou simplement aux surfaces à ne pas traiter. Elle concerne aussi l'application d'une protection de surface pour toute pièce mécanique devant être soumise à un traitement de surface similaire,The invention relates to the protection of turbomachine blade surfaces prior to a partial surface with a character abrasive or simply to surfaces not to be treated. She also relates to the application of a surface protection for any part mechanics to be subjected to a similar surface treatment,

En référence à la figure 1, une aube 10 de turbomachine, ici de compresseur ou de soudante de turboréacteur, se d'une paie 11 comportant une face intrados et une face extrados 19, d'une échasse 12 et d'un pied 13 s'emmanchant dans une alvéole axiale ménagée dans l'axe du disque central de la la supportant (non représentés). Une plate forme 14 sépare la pale 11 de l'échasse 12.With reference to FIG. 1, a turbine engine blade 10, here compressor or welding turbojet, is a pay 11 having an intrados face and an extrados face 19, a stilt 12 and a foot 13 slotting into an axial cavity formed in the axis of the central disc of the support (not shown). A platform 14 separates the blade 11 from the stilt 12.

Le disque central porte ainsi un certain d'aubes dont les pales sont toutes maintenues équidistantes les unes des autres notamment par des nageoires 15 situées sur une partis médiane de chaque face des pales et dont, pour deux nageoires adjacentes de deux pales voisines, les extrémités sont en contact.The central disk thus carries a certain number of vanes whose blades are all kept equidistant from each other, in particular by fins 15 located on a median portion of each face of the blades and of which, for two adjacent fins of two neighboring blades, the ends are in contact.

Le traitement de surface de l'aube 10, généralement en titane ou en alliage de titane, comporte un premier traitement E1 de la surface par sablage pour en augmenter la rugosité, en préparation d'une deuxième étape E2 dite de métallisation avec dépôt par projection thermique. C'est le cas notamment de la projection au moyen d'une torche à plasma, soit d'un alliage de cuivre, par exemple Cu - Ni - In (cuivre - nickel - indium), dont la ductilité permet d'amortir les vibrations du moteur en fonctionnement au niveau des contacts des aubes avec le disque central, soit de carbure de tungstène, par exemple WC-Co (carbure de tungstène-cobalt) dont la dureté permet d'éviter l'usure occasionnée par les frottements entre les nageoires adjacentes.The surface treatment of blade 10, generally made of titanium or titanium alloy, comprises a first treatment E1 of the surface by sandblasting to increase the roughness, in preparation for a second said metallization step E2 with thermal spray deposition. It is the case in particular of the projection by means of a plasma torch, either of a copper alloy, for example Cu - Ni - In (copper - nickel - indium), whose ductility makes it possible to dampen the vibrations of the motor by operation at the blade contacts with the central disk, either of tungsten carbide, for example WC-Co (tungsten carbide-cobalt) whose hardness makes it possible to avoid the wear caused by the friction between adjacent fins.

La torche à plasma projette le revêtement d'alliage à grande vitesse et à élevée (plus de 2 500°K.) sur la surface à traiter pour y obtenir son accrochage. The plasma torch projects the alloy coating at high speed and (more than 2500 ° K.) on the surface to be treated for get his hang.

Les étapes E1 sont très abrasives et les étapes E2 sont indésirables en dehors des surfaces à traiter. Elles nécessitent dans le cas du traitement des nageoires, d'interposer une protection entre les outils de sablage et/ou les torches à plasma et les faces 19 des aubes 10 de façon à soustraire ces dernières à leurs effets. Plus précisément, seules les surfaces 17 des extrémités de nageoires 15 destinées à être mises en contact avec celles 17 des autres nageoires des aubes voisines, sont soumises, lors de la fabrication, aux traitements de surface ci-dessus. En outre les deux faces 19 de la pale 11 présentent des surfaces en hélice, de géométrie très précise, qu'il faut protéger.Steps E1 are very abrasive and steps E2 are undesirable in outside the surfaces to be treated. They require in the case of the treatment fins, to interpose a protection between the tools of sandblasting and / or the plasma torches and the faces 19 of the blades 10 so as to subtract these from their effects. More specifically, only surfaces 17 of the ends of fins 15 to be put into contact with those 17 of the other fins of the neighboring blades, are submitted, during manufacture, to the surface treatments above. In in addition to the two faces 19 of the blade 11 have helical surfaces, very precise geometry, which must be protected.

Dans le cas du traitement du pied, les seules surfaces 18 de contact, situées de part et d'autre 13 du pied de l'aube 10 sont à revêtir. Les autres zones 12 et 13 du pied doivent être protégées au moins durant le traitement E2.In the case of foot treatment, the only contact surfaces 18, located on both sides of the foot of the blade 10 are to be coated. The other areas 12 and 13 of the foot must be protected at least during E2 treatment.

Actuellement, pour cela, l'opérateur applique manuellement des rubans adhésifs ayant une résistance mécanique et thermique suffisante autour des surfaces à traiter.Currently, for this, the operator manually applies ribbons Adhesives with sufficient mechanical and thermal resistance around surfaces to be treated.

Ces opérations manuelles sont longues et fastidieuses à cause de la complexité des formes des aubes, de la précision requise et du peu d'accessibilité des surfaces à protéger. Elles n'assurent pas une qualité de niveau constant puisqu'elles ne sont pas parfaitement répétitives et qu'une mauvaise adhésion des rubans adhésifs présente un risque de masquage voire de décollement du revêtement déposé. En outre lors de la métallisation, on constate que des particules atteignent la couche en formation après avoir rebondi sur la surface de protection. La qualité de l'accrochage ou de l'homogénéité de ces particules n'est alors pas suffisante, et les zones correspondantes sont moins résistantes aux sollicitations appliquées sur turbomachines.These manual operations are long and tedious because of the complexity of the blade shapes, the precision required and the lack of accessibility of the surfaces to be protected. They do not provide a quality constant level since they are not perfectly repetitive and poor adhesion of adhesive tapes presents a risk of masking or even detachment of the deposited coating. In addition when the metallization, it is found that particles reach the layer in formation after bouncing off the protective surface. The quality of the snagging or homogeneity of these particles is then not sufficient, and the corresponding areas are less resistant to stresses applied on turbomachines.

Il existe donc un besoin pour améliorer la productivité et la qualité de ces opérations.There is therefore a need to improve the productivity and quality of these operations.

Par ailleurs les opérateurs sur ces opérations sont soumis à des tensions nerveuses dues notamment à l'attention soutenue nécessaire pour leur exécution; ils sont aussi exposés à des risques de troubles musculo-squelettiques (TMS) consécutifs à la réalisation d'actions répétitives. In addition, the operators of these operations are subject to particularly due to the sustained attention required for their execution; they are also at risk of musculoskeletal disorders (TMS) consecutive to the realization of repetitive actions.

Pour remédier à tous ces inconvénients, la demanderesse propose un masque de protection pour le traitement de surface de surfaces d'une aube de turbomachine comportant un pied et éventuellement des nageoires, disposé autour desdites surfaces en résistant aux effets du traitement de surface, tout en constituant un outillage démontable et réutilisable, caractérisé par le fait que lesdites surfaces étant situées soit sur le pied de l'aube soit en extrémité de nageoire, il est composé d'au moins une pièce épousant la forme du pied ou des nageoires respectivement, et comportant des lumières laissant apparaítre lesdites surfaces à traiter,To remedy all these drawbacks, the applicant proposes a protective mask for the surface treatment of surfaces of a turbomachine blade having a foot and possibly fins, disposed around said surfaces while resisting the effects of surface treatment, while constituting a dismountable tool and reusable, characterized in that said surfaces being located either on the foot of the dawn is at the end of the fin, it is composed of minus a piece matching the shape of the foot or fins respectively, and having lights revealing said surfaces to be treated,

Le traitement de surface comprend une étape de sablage et/ou une étape de métallisation.The surface treatment comprises a sandblasting step and / or a step of metallization.

Par outillage, on désigne pièce ou un ensemble de pièces au moins en partie rigides dont la forme et les matériaux sont adaptés au masquage des parties de surfaces à protéger. Les matériaux de l'outillage sont aussi en capacité de résister à l'environnement opératoire des opérations E1 et E2. Grâce à l'outillage de l'invention, on supprime toute opération d'application manuelle de ruban adhésif, et le masquage est parfaitement répétitif."Tooling" means a part or a set of parts at least partly rigid whose shape and materials are suitable for masking parts of surfaces to be protected. Tooling materials are also able to withstand the operational environment of operations E1 and E2. Thanks to the tooling of the invention, all operations are eliminated. manual application of adhesive tape, and the masking is perfectly repetitive.

De préférence, l'étape E2 entraínant une élévation de température, le masque de protection est dispose pour résister aux effets thermiques du traitement de surface, ici un dépôt plasma.Preferably, the step E2 causing a rise in temperature, the protective mask is provided to withstand the thermal effects of surface treatment, here a plasma deposit.

De préférence encore, l'étape E2 nécessitant un traitement mécanique préalable, le masque de protection de l'étape E1 est d'un matériau résistant à l'action abrasive d'un sablage.More preferably, step E2 requiring mechanical treatment beforehand, the protective mask of step E1 is of a material resistant to the abrasive action of sanding.

Avantageusement, le masque de protection est en acier inoxydable ou en matériau silicone ou en matériau polymère.Advantageously, the protective mask is made of stainless steel or silicone material or polymer material.

Eventuellement, le masque peut servir à la fois pour le sablage et pour le dépôt plasma, et peut être réutilise pour une série d'aubes de turbomachines. Optionally, the mask can be used both for sanding and for plasma deposit, and can be reused for a series of turbomachinery.

L'invention sera mieux comprise à l'aide de la description suivante d'un masque de protection pour deux applications de l'invention et du dessin annexé dans lequel :

  • la figure 1 représente une vue perspective d'une aube de compresseur;
  • la figure 2 représente une vue de cote d'une première application de l'invention consistant en un conformé pour permettre le traitement du pied d'une aube,
  • la figure 3 représente un montage permettant le traitement simultané de plusieurs aubes,
  • les figures 4A et 4B représentent des vues perspectives d'une autre application de l'invention, consistant en des masques pour la protection des surfaces d'une aube contre le sablage et le dépôt plasma sur les surfaces à traiter de son pied; et
  • la figure 5 représente une vue perspective d'une seconde application de l'invention, consistant en un masque pour la protection des surfaces d'une aube contre le sablage et le dépôt plasma sur les surfaces à traiter de ses nageoires ;
The invention will be better understood with the aid of the following description of a protective mask for two applications of the invention and the appended drawing in which:
  • Figure 1 shows a perspective view of a compressor blade;
  • FIG. 2 represents a side view of a first application of the invention consisting of a shape for allowing the treatment of the root of a blade,
  • FIG. 3 represents a mounting allowing the simultaneous treatment of several blades,
  • FIGS. 4A and 4B show perspective views of another application of the invention, consisting of masks for protecting the surfaces of a blade against sanding and plasma deposition on the surfaces to be treated of its foot; and
  • FIG. 5 represents a perspective view of a second application of the invention, consisting of a mask for protecting the surfaces of a blade against sanding and plasma deposition on the surfaces to be treated with its fins;

La figure 2 représente la partie inférieure d'une aube de compresseur dont on voit la pale 11, la plate-forme 14 et le pied 13. Il est ici en forme de queue d'aronde et rectiligne (cas non exhaustif, cité à titre d'exemple). Afin d'assurer un amortissement des vibrations de l'aube dans son alvéole pendant le fonctionnement du moteur, on applique un revêtement 13R localisé dans les zones qui sont en contact avec les flancs de l'alvéole. Pour pouvoir appliquer ce revêtement par torche à plasma, on dispose conformément à l'invention, un masque 100 qui épouse la forme du pieu de l'aube en partie, et peut être mis en place par simple enchâssement. Le masque 100, avantageusement réalisé en inox, présente une épaisseur déterminée. Une fenêtre 100R est ménagée dans ce masque, de chaque côté du pied. La forme et les dimensions des fenêtres dépendent de celles du revêtement 13R qu'il s'agit d'appliquer par la torche à plasma. Ce revêtement 13R est localisé sur les deux surfaces du pieu. qui seront en contact avec le disque sur la turbomachine.Figure 2 shows the lower part of a compressor blade of which we see the blade 11, the platform 14 and the foot 13. It is here in shape dovetail and rectilinear (non-exhaustive case, quoted example). In order to ensure a damping of the vibrations of the dawn in its cell during the operation of the engine, apply a 13R coating located in areas that are in contact with flanks of the cell. To apply this coating by torch according to the invention, a mask 100 which espouses the shape of the dawn stake in part, and can be set up by simple embedding. The mask 100, advantageously made of stainless steel, has a determined thickness. A 100R window is provided in this mask, on each side of the foot. The shape and dimensions of windows depend on those of the 13R coating that is to be applied by the plasma torch. This 13R coating is located on both pile surfaces. who will be in contact with the disk on the turbine engine.

Dans la mesure où la torche à plasma T est placée préférentiellement perpendiculairement à la surface à traiter, les parois de la fenêtre sont aussi perpendiculaires à cette surface. La fenêtre permet le passage des particules de métal en fusion pendant l'opération de métallisation avec la torche à plasma. Cette disposition présente l'avantage que les particules de métal en fusion issues de la torche à plasma qui ne sont pas dirigées l'axe de la fenêtre se déposent sur le masque dans la zone bordant la fenêtre 100R sans être réfléchies vers l'intérieur. Ces particules ne viennent donc pas perturber la couche en formation par rebond. Après d'une couche d'épaisseur voulue, on retire le masque. Le revêtement 13R a exactement la forme définie par celle de la fenêtre , il n est pas nécessaire de procéder à une opération de retouche.Since the plasma torch T is preferentially placed perpendicular to the surface to be treated, the walls of the window are also perpendicular to this surface. The window allows the passage of molten metal particles during the metallization operation with the plasma torch. This arrangement has the advantage that the particles molten metal from the plasma torch that are not directed the axis of the window are deposited on the mask in the bordering area window 100R without being reflected inward. These particles do not so do not disturb the formation layer by rebound. After of a layer of desired thickness, the mask is removed. The 13R coating has exactly the shape defined by that of the window it It is not necessary to carry out a retouching operation.

On remet en service le masque pour le traitement d'autres aubes si la zone métallisée en bordure de la fenêtre n'est pas trop épaisse. Le masque peut être ainsi utilisé plusieurs fois avant de nécessiter une remise en forme par "démétallisation" de la zone bordant la fenêtre. Une telle opération de restauration du masque est avantageusement effectuée par chimique selon les techniques connues de l'homme du métier.The mask is put back into service for the treatment of other blades if the Metallic area at the edge of the window is not too thick. The mask can be so used several times before requiring a fitness by "demetallization" of the area bordering the window. A such operation of restoring the mask is advantageously carried out by chemical techniques known to man of the job.

Si une opération préalable de préparation de la surface est nécessaire, on utilise le même masque pour protéger les surfaces qui ne doivent pas recevoir le sablage.If a preliminary operation of surface preparation is necessary, uses the same mask to protect surfaces that should not receive sanding.

Un tel masque présente aussi l'avantage de permettre le traitement de plusieurs aubes en même temps. Dans ce but on a prévu une rainure 110 dans la paroi de fond du masque pour permettre d'appliquer ensuite une barre d'alignement 43.Such a mask also has the advantage of allowing the treatment of several blades at the same time. For this purpose a groove 110 is provided in the bottom wall of the mask to allow then to apply a alignment bar 43.

On a représente sur la figure 3 un montage pour le traitement de quelques aubes. On assemble les aubes équipées de leur masque de protection 100 sur un seul outillage 40.FIG. 3 shows a mounting for the treatment of some dawns. We assemble the blades equipped with their mask protection 100 on a single tool 40.

L'outillage 40 comporte un bâti 42 sur lequel on a fixé les aubes, pale en bas, de manière à présenter les masques sur le dessus. Les fenêtres 100R sont visibles. Une barre 43 relie les masques 100 par les rainures 110. Grâce à cette barre on peut aligner avec précision les masques les uns par rapport aux autres. Des flasques 41 sont placés le long de la rangée de masques de manière à recouvrir et protéger les plates-formes des aubes. Une fois le montage effectué, on place l'outil de traitement en direction de la première fenêtre et on le déplace à vitesse déterminée parallèlement aux fenêtres. Par cette disposition on permet le traitement de sablage suivi de métallisation ou bien de métallisation d'un ensemble N d'aubes en assurant une qualité constante.The tool 40 comprises a frame 42 on which the blades have been fixed, blade in down, so as to present the masks on the top. 100R windows are visible. A bar 43 connects the masks 100 by the grooves 110. Thanks to this bar you can precisely align the masks one by one compared to others. Flanges 41 are placed along the row of masks so as to cover and protect the platforms of the blades. Once the editing is done, we place the treatment tool in the direction from the first window and move it at a fixed speed in parallel at the windows. By this arrangement sandblasting treatment is allowed followed by metallization or metallization of a set N of blades ensuring a constant quality.

On a représenté sur les figures 4A et 4B, un dispositif de masquage adapté à des aubes dont le pied est curviligne, telles que des aubes de soufflante de taille.FIGS. 4A and 4B show a masking device adapted to blades with a curvilinear foot, such as blades of blower size.

Pour une étape E1. de sablage des surfaces 18 du pied 13 de la pale 11 d'une aube 10, il est prévu, en référence à la figure 4A, un masque 100' de protection comportant, fixé sur un socle 132, un bâti 125 en matériau silicone ou matériau polymère agencé pour pouvoir être monte en emboítant le pied 13 de la pale 11 tout en laissant apparaítre, au travers de lumières 124 les surfaces 18 à traiter.For a step E1. sandblasting surfaces 18 of the foot 13 of the blade 11 of a blade 10, there is provided, with reference to FIG. 4A, a mask 100 ' protection device comprising, fixed on a base 132, a frame 125 of material silicone or polymer material arranged to be able to be mounted in fitting the foot 13 of the blade 11 while allowing to appear, through lights 124 surfaces 18 to be treated.

Pour cela, le bâti comporte deux demi-coques 121 épousant les formes de la surface ci-dessus, réalisées selon les plans même qui en ont permis la réalisation.For this, the frame comprises two half-shells 121 matching the shapes of the above surface, made according to the same plans that made it possible the realization.

Ces deux demi-coques 121 sont assemblées par des verrous 123 amovibles, par exemple s'emboítant eux-mêmes dans les deux demi-coques 121, et peuvent donc être démontées pour rester apte à un nouveau montage et rester disponible pour le traitement d'une autre aube.These two half-shells 121 are assembled by locks 123 removable, for example fitting themselves in the two half-shells 121, and can therefore be dismantled to remain fit for a new editing and remain available for the treatment of another dawn.

Pour une étape E2 de dépôt plasma des surfaces 18 du pied 13 de la pale 11, il est prévu, en référence à la figure 4B, un masque 100"' de protection comportant, fixés sur un socle 132", quatre supports 127 agencés pour pouvoir supporter deux entretoises 126, tous en inox, maintenant la paie 11 et deux masques 128, en inox, maintenant et recouvrant le pied 13 de la pale 11, de part et d'autre du pied, tout en laissant apparaítre, au travers de lumières 131 les surfaces 18 à traiter.For a step E2 plasma deposition of the surfaces 18 of the foot 13 of the blade 11, there is provided, with reference to FIG. 4B, a mask 100 "'of protection comprising, fixed on a base 132 ", four supports 127 arranged to support two spacers 126, all made of stainless steel, now payroll 11 and two masks 128, stainless steel, now and covering the foot 13 of the blade 11, on either side of the foot, while revealing, through lights 131 surfaces 18 to be treated.

ici, pour régler exactement l'étendue de la surface à traiter, la périphérie des lumières 131 est garnie de pattes 129 limitant cette étendue à volonté. La position des pattes 129 est réglable par coulissement sur les masques 128 et y est maintenus par des vis de serrage 130. here, to exactly regulate the extent of the surface to be treated, the periphery lights 131 is lined with tabs 129 limiting this extent to will. The position of the tabs 129 is adjustable by sliding on the masks 128 and is held there by clamping screws 130.

Dans l'exemple de la figure les pattes 129 limitent seulement la longueur des lumières 131 mais le même dispositif est possible aussi en largeur, les deux dispositifs pouvant facilement être simultanément.In the example of the figure the tabs 129 limit only the length lights 131 but the same device is possible also in width, both devices can easily be simultaneously.

On a représenté sur la figure 5 un mode de réalisation de l'invention correspondant au traitement des nageoires de l'aube. Un masque 239 de protection comportant deux demi-coques 233, épouse la forme des nageoires selon une cheminée 234 et des faces 19 voisines de celles-ci. Ces formes sont directement déduites du plan de l'aube 10. Les deux demi-coques 233 sont assemblées entre elles sur la surface à protéger par le moyen de quatre pinces 236, par exemple des lames de ressort en inox s'incrustant dans des trous (non visibles sur la figure) ménagés à cet effet dans le masque 239.FIG. 5 shows an embodiment of the invention corresponding to the treatment of the fins of the dawn. A mask 239 of protection comprising two half-shells 233, matches the shape of the fins according to a chimney 234 and faces 19 adjacent thereto. These forms are directly deduced from the plane of dawn 10. The two half-shells 233 are assembled together on the surface to be protected by the means of four clips 236, for example stainless spring blades embedding in holes (not visible in the figure) provided for this purpose in the mask 239.

Le masque dans ce cas est en matériau silicone, Ce matériau est à la fois résistant au mécanique de sablage et au traitement thermique de métallisation.The mask in this case is made of silicone material, this material is both resistant to sanding mechanics and heat treatment of metallization.

Les deux demi-coques 233 laissent apparaítre les surfaces des extrémités de nageoires 17 à traiter au travers de lumières 235 de façon à ce que ces extrémités restent suffisamment dégagées du masque d'une certaine hauteur « e ».The two half-shells 233 reveal the surfaces of the ends of fins 17 to be treated through lights 235 so that these ends remain sufficiently clear of the mask of some height "e".

Le masque 239 sert à la fois pour le sablage et pour le dépôt plasma, il est encore réutilisé un certain nombre de fois,The mask 239 is used both for sandblasting and for plasma deposition. is still reused a number of times,

La présente invention n'est pas limitée aux modes de réalisation représentés. Elle englobe toutes les variantes à la disposition de l'homme du métier.The present invention is not limited to the embodiments represented. It encompasses all variants available to humans of career.

Claims (8)

Masque de protection pour le traitement de surface de surfaces (17, 18) d'une aube (10) de turbomachine comportant un pied et éventuellement des nageoires, disposé autour desdites surfaces en résistant aux effets du traitement de surface, tout en constituant un outillage démontable et réutilisable, caractérise par le fait que lesdites surfaces étant situées soit sur le pied de l'aube soit en extrémité de nageoire, il est composé d'au moins une pièce (100, 100', 100", 239) épousant la forme du pied ou des nageoires respectivement, et comportant des lumières laissant apparaítre lesdites surfaccs à traiter.Protective mask for the surface treatment of surfaces (17, 18) of a turbomachine blade (10) comprising a foot and possibly fins, disposed around said surfaces while resisting the effects of the surface treatment, while constituting a tooling removable and reusable, characterized in that said surfaces being located either on the root of the blade or at the end of the fin, it is composed of at least one piece (100, 100 ', 100 ", 239) conforming to the shape foot or fins respectively, and having lights revealing said surfacs to be treated. Masque selon la revendication 1, comportant au moins deux demi-coques (121, 233) maintenus ensemble par des verrous ou des pinces (123,236).Mask according to claim 1, comprising at least two half-shells (121, 233) held together by bolts or clamps (123.236). Masque selon l'une des revendications 1 et 2, constitué en un matériau résistant aux effets thermiques d'un dépôt plasma.Mask according to one of claims 1 and 2, consisting of a material resistant to the thermal effects of a plasma deposit. Masque selon l'une des revendications 1 à 3, constitue en un matériau résistant aux effets thermiques d'un sablage.Mask according to one of claims 1 to 3, constitutes a material resistant to the thermal effects of sanding. Masque selon l'une des revendications 1, 3 et 4, épousant la forme du pied de l'aube et constitué en inox.Mask according to one of claims 1, 3 and 4, conforming to the shape of the foot of dawn and made of stainless steel. Masque selon la revendication 5, pouvant être en place par simple enchâssement.Mask according to claim 5, which can be in place simply entrenchment. Masque selon l'une des revendications 1 à 4, constitué en matériau silicone ou polymère.Mask according to one of claims 1 to 4, made of material silicone or polymer. Masque selon la revendication 7 dans lequel, les aubes de turbomachines comportent des nageoires (15) dont les extrémités sont à traiter, jésuites extrémités restent dégagées du masque d'une certaine hauteur « e ».Mask according to claim 7 wherein the blades of turbomachines comprise fins (15) whose ends are treat, Jesuit ends remain clear of the mask of some height "e".
EP04300818A 2003-12-04 2004-11-26 Protection mask for the surface treatment of blades for turbine engines Expired - Fee Related EP1537950B1 (en)

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EP07113930A EP1911549B1 (en) 2003-12-04 2004-11-26 Protective mask for surface treatment of turbomachine vanes

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FR0314256 2003-12-04
FR0314256A FR2863191B1 (en) 2003-12-04 2003-12-04 PROTECTIVE MASK FOR SURFACE TREATMENT OF TURBOMACHINE BLADES

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DE (2) DE602004008015T2 (en)
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NO20045322L (en) 2005-06-06
US7066799B2 (en) 2006-06-27
RU2369443C2 (en) 2009-10-10
DE602004008015D1 (en) 2007-09-20
DE602004008015T2 (en) 2008-04-24
DE602004025058D1 (en) 2010-02-25
TW200530488A (en) 2005-09-16
CN1626696A (en) 2005-06-15
ES2291837T3 (en) 2008-03-01
ES2336499T3 (en) 2010-04-13
EP1911549A1 (en) 2008-04-16
US20050227589A1 (en) 2005-10-13
RU2004135414A (en) 2006-05-10
EP1911549B1 (en) 2010-01-06
NO336270B1 (en) 2015-07-06
TWI331184B (en) 2010-10-01
FR2863191B1 (en) 2007-04-20
CN100569988C (en) 2009-12-16
MXPA04012145A (en) 2005-09-21
FR2863191A1 (en) 2005-06-10
EP1537950B1 (en) 2007-08-08

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