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 PDFInfo
- 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
Links
- 238000004381 surface treatment Methods 0.000 title claims description 10
- 239000000463 material Substances 0.000 claims description 10
- 230000001681 protective effect Effects 0.000 claims description 7
- 230000000694 effects Effects 0.000 claims description 6
- 239000010935 stainless steel Substances 0.000 claims description 5
- 229910001220 stainless steel Inorganic materials 0.000 claims description 5
- 229920001296 polysiloxane Polymers 0.000 claims description 4
- 229920000642 polymer Polymers 0.000 claims 1
- 238000011282 treatment Methods 0.000 abstract description 15
- 238000001465 metallisation Methods 0.000 abstract description 8
- 238000005488 sandblasting Methods 0.000 abstract description 7
- 239000011248 coating agent Substances 0.000 description 7
- 238000000576 coating method Methods 0.000 description 7
- 238000000151 deposition Methods 0.000 description 4
- 230000008021 deposition Effects 0.000 description 4
- 230000000873 masking effect Effects 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 230000003252 repetitive effect Effects 0.000 description 3
- 241000272165 Charadriidae Species 0.000 description 2
- 239000002390 adhesive tape Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000002861 polymer material Substances 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 208000023178 Musculoskeletal disease Diseases 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910009043 WC-Co Inorganic materials 0.000 description 1
- IZBSGLYEQXJERA-UHFFFAOYSA-N [In].[Ni].[Cu] Chemical compound [In].[Ni].[Cu] IZBSGLYEQXJERA-UHFFFAOYSA-N 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000001311 chemical methods and process Methods 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
- 238000009718 spray deposition Methods 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24C—ABRASIVE OR RELATED BLASTING WITH PARTICULATE MATERIAL
- B24C1/00—Methods for use of abrasive blasting for producing particular effects; Use of auxiliary equipment in connection with such methods
- B24C1/04—Methods 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
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/01—Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B12/00—Arrangements for controlling delivery; Arrangements for controlling the spray area
- B05B12/16—Arrangements for controlling delivery; Arrangements for controlling the spray area for controlling the spray area
- B05B12/20—Masking 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
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
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
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
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
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
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 ;
- 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
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
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
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
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
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
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-
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-
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
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
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
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
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-
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
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)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP07113930A EP1911549B1 (en) | 2003-12-04 | 2004-11-26 | Protective mask for surface treatment of turbomachine vanes |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0314256 | 2003-12-04 | ||
FR0314256A FR2863191B1 (en) | 2003-12-04 | 2003-12-04 | PROTECTIVE MASK FOR SURFACE TREATMENT OF TURBOMACHINE BLADES |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07113930A Division EP1911549B1 (en) | 2003-12-04 | 2004-11-26 | Protective mask for surface treatment of turbomachine vanes |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1537950A1 true EP1537950A1 (en) | 2005-06-08 |
EP1537950B1 EP1537950B1 (en) | 2007-08-08 |
Family
ID=34451723
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07113930A Active EP1911549B1 (en) | 2003-12-04 | 2004-11-26 | Protective mask for surface treatment of turbomachine vanes |
EP04300818A Expired - Fee Related EP1537950B1 (en) | 2003-12-04 | 2004-11-26 | Protection mask for the surface treatment of blades for turbine engines |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07113930A Active EP1911549B1 (en) | 2003-12-04 | 2004-11-26 | Protective mask for surface treatment of turbomachine vanes |
Country Status (10)
Country | Link |
---|---|
US (1) | US7066799B2 (en) |
EP (2) | EP1911549B1 (en) |
CN (1) | CN100569988C (en) |
DE (2) | DE602004008015T2 (en) |
ES (2) | ES2291837T3 (en) |
FR (1) | FR2863191B1 (en) |
MX (1) | MXPA04012145A (en) |
NO (1) | NO336270B1 (en) |
RU (1) | RU2369443C2 (en) |
TW (1) | TWI331184B (en) |
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EP2309016A1 (en) * | 2009-10-06 | 2011-04-13 | Siemens Aktiengesellschaft | Method and arrangement for a spray coating process |
EP2371459A3 (en) * | 2010-03-31 | 2014-05-28 | United Technologies Corporation | Masking apparatus |
EP2289666A3 (en) * | 2009-08-27 | 2014-08-20 | United Technologies Corporation | Abrasive finish mask and method of masking a component |
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2003
- 2003-12-04 FR FR0314256A patent/FR2863191B1/en not_active Expired - Fee Related
-
2004
- 2004-11-26 DE DE602004008015T patent/DE602004008015T2/en active Active
- 2004-11-26 TW TW093136500A patent/TWI331184B/en not_active IP Right Cessation
- 2004-11-26 DE DE602004025058T patent/DE602004025058D1/en active Active
- 2004-11-26 ES ES04300818T patent/ES2291837T3/en active Active
- 2004-11-26 EP EP07113930A patent/EP1911549B1/en active Active
- 2004-11-26 EP EP04300818A patent/EP1537950B1/en not_active Expired - Fee Related
- 2004-11-26 ES ES07113930T patent/ES2336499T3/en active Active
- 2004-11-29 US US10/997,863 patent/US7066799B2/en active Active
- 2004-12-03 MX MXPA04012145A patent/MXPA04012145A/en active IP Right Grant
- 2004-12-03 NO NO20045322A patent/NO336270B1/en not_active IP Right Cessation
- 2004-12-03 CN CNB2004101001671A patent/CN100569988C/en not_active Expired - Fee Related
- 2004-12-03 RU RU2004135414/02A patent/RU2369443C2/en not_active IP Right Cessation
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Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1762303A1 (en) * | 2005-09-09 | 2007-03-14 | Siemens Aktiengesellschaft | Method for preparing turbine blades for spray coating and device for holding such blades |
US7717058B2 (en) | 2005-09-09 | 2010-05-18 | Siemens Aktiengesellschaft | Method of preparing turbine blades for spray coating and mounting for fixing such a turbine blade |
EP2053142A2 (en) * | 2007-10-24 | 2009-04-29 | United Technologies Corporation | A method of spraying a turbine engine component |
EP2053142A3 (en) * | 2007-10-24 | 2012-01-25 | United Technologies Corporation | A method of spraying a turbine engine component |
US8173218B2 (en) | 2007-10-24 | 2012-05-08 | United Technologies Corporation | Method of spraying a turbine engine component |
EP2289666A3 (en) * | 2009-08-27 | 2014-08-20 | United Technologies Corporation | Abrasive finish mask and method of masking a component |
EP2309016A1 (en) * | 2009-10-06 | 2011-04-13 | Siemens Aktiengesellschaft | Method and arrangement for a spray coating process |
CN102031476A (en) * | 2009-10-06 | 2011-04-27 | 西门子公司 | Method and arrangement for a spray coating process |
CN102031476B (en) * | 2009-10-06 | 2015-08-19 | 西门子公司 | For method and the device of spraying coating process |
EP2371459A3 (en) * | 2010-03-31 | 2014-05-28 | United Technologies Corporation | Masking apparatus |
Also Published As
Publication number | Publication date |
---|---|
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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