EP2798095B1 - Pressure masking systems and methods for using the same - Google Patents
Pressure masking systems and methods for using the same Download PDFInfo
- Publication number
- EP2798095B1 EP2798095B1 EP12818755.6A EP12818755A EP2798095B1 EP 2798095 B1 EP2798095 B1 EP 2798095B1 EP 12818755 A EP12818755 A EP 12818755A EP 2798095 B1 EP2798095 B1 EP 2798095B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- target surface
- pressurized masking
- cleaning
- fluid
- passageway
- 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.)
- Active
Links
Images
Classifications
-
- 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
- C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- 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
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- 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
Definitions
- Embodiments of the subject matter disclosed herein relate to masking systems. Other embodiments relate to to pressure masking systems for cleaning articles with passageways.
- gas turbine engines such as aircraft engines for example
- air is drawn into the front of the engine, compressed by a shaft-mounted rotary-type compressor, and mixed with fuel.
- the mixture is burned, and the hot exhaust gases are passed through a turbine mounted on a shaft.
- the flow of gas turns the turbine, which turns the shaft and drives the compressor and fan.
- the hot exhaust gases flow from the back of the engine, driving it and the aircraft forward.
- the temperatures of combustion gases may exceed 3000°F (about 1650°C), considerably higher than the melting temperatures of the metal parts of the engine which are in contact with these gases. Operation of these engines at gas temperatures that are above the metal part melting temperatures is a well-established art, and depends in part on supplying a cooling air to the outer surfaces of the metal parts through various methods.
- the metal parts of these engines that are particularly subject to high temperatures, and thus require particular attention with respect to cooling, are the metal parts forming combustors and parts located aft of the combustor.
- the metal temperatures can be maintained below melting levels by using passageways such as cooling holes incorporated into some engine components.
- a thermal barrier coatings may also be applied to the component by a pressure coating process (e.g., a thermal spray process).
- a pressure coating process e.g., a thermal spray process
- the thermal spray process and other cleaning processes e.g., grit blasting, shot peening, water jet washing
- overspray that partially or completely blocks the component's cooling holes.
- present coating e.g., thermal spray
- cleaning processes involve a multi-step, highly labor intensive process of applying a partial layer of TBC coating, allowing the component and the TBC to sufficiently cool to a temperature at which the component can easily be handled, removing the component from an application fixture on which the thermal spraying takes place, and removing any masking, which is then followed by separately removing the well-cooled, solidified coating from the cooling holes using a water jet or other cleaning methods.
- a fraction of the desired TBC thickness is applied prior to cleaning. As a result, the entire process must typically be repeated several times until the desired TBC thickness is reached.
- EP 1645363 A1 discloses a smoothing process that smooths the surface of a component such as a turbine blade by jet treatment with a high pressure fluid jet containing solid particles. While the component is being treated by the high pressure fluid jet, it is kept in a fluid-filled container.
- the fluid container has a fluid input and a solid particle input.
- a method in accordance with the invention as hereinafter claimed of pressure cleaning a target surface of an article comprising one or more passageways comprises the steps of claim 10 below.
- a pressurized masking system in accordance with the invention as hereinafter claimed for cleaning a target surface of an article comprising passageways comprises the features of claim 1 below.
- Pressurized masking systems disclosed herein generally comprise a pressure masker, and a part cleaner to clean the target surface of an article comprising passageways. While the part cleaner projects cleaning material towards the target surface, pressurized masking fluid is fluidly connected to the passageways and passed there through to prevent the permanent altering of a cross sectional area of the passageways by the cleaning material. Pressurized masking systems, and methods of pressure cleaning a target surface of an article, will be discussed in more detail herein.
- a pressurized masking system 100 comprising a part cleaner 20 and a pressure masker 30 for cleaning an article 10.
- the article 10 comprises one or more passageways 12 passing through the article 10 from a first side 18 to a second side 19.
- the article 10 can comprise a variety of different parts such as a combustor liner or other component of a gas turbine engine.
- the article 10 can comprise a turbine component such as a hot gas path component or a combustion component.
- the passageways 12 can comprise any passage through the article 10 (passing from the first side 18 to the second side 19) that is intended to remain open (such that air can pass through) when the article 10 is in use.
- the passageways 12 may comprise cooling holes.
- the second side 19 of the article 10 comprises a target surface 11 that is to be cleaned.
- the target surface 11 may be cleaned prior to first use, during routine or repair maintenance, or as otherwise necessary depending on the life of the article 10.
- cleaned refers to stripping, washing and/or treating the target surface such as through grit blasting, shot peening, water jet washing or the like as will become appreciated herein.
- the target surface 11 of the article 10 may comprise a coating 22 or other debris that is to be removed prior to applying a fresh coating.
- the target surface 11 of the article 10 may have or will have a thermal barrier coating ("TBC") disposed thereon.
- TBC thermal barrier coating
- the TBC can comprise one or more layers of metal and/or ceramic coating material applied to the target surface 11 of the article 10 to impede the transfer of heat from hot combustion gases to the article 10, thus insulating the component from the hot combustion gas.
- the presence of the TBC on the surface permits the combustion gas to be hotter than would otherwise be possible with the particular material and fabrication process of the component.
- Any suitable composition of TBC may be applied.
- the TBC can comprise a bond layer of MCrAlY, wherein M is preferably Ni, Co, or a combination thereof, followed by a layer of yttria stabilized zirconia (YSZ).
- the article 10 may be disposed on a support stand 15 prior to or during the pressure cleaning as will become appreciated herein.
- the support stand 15 may be stationary or mobile (e.g., rotatable) and position the article 10 relative to the part cleaner 20 and the pressure masker 30 when cleaning the target surface 11 of the article 10.
- the pressurized masking system 100 further comprises the part cleaner 20.
- the part cleaner 20 comprises any device that projects a cleaning material 25 towards the target surface 11 of the article 10.
- the part cleaner 20 can comprise a grit blaster.
- the cleaning material 25 can comprise pressurized air with aluminum oxide, walnut shells, dry ice, charcoal, or any other particulates dispersed therein.
- the part cleaner 20 can comprise a shot peening device.
- the cleaning material 25 can comprise pressurized air with metallic, glass or ceramic particles dispersed therein.
- the part cleaner 20 may comprise a pressure washer.
- the cleaning material 25 may comprise water with or without an additional abrasive material.
- the part cleaner 20 may be disposed at any position relative to the article 10 that allows for the cleaning of the target surface 11.
- the article 10 may be disposed on a support stand 15 adjacent the part cleaner 20.
- the support stand 15 may then be able to rotate or otherwise displace the article 10 with respect to the part cleaner 20 and/or the part cleaner 20 may be able to articulate with respect to the article 10.
- the part cleaner 20 may then be used to project the cleaning material 25 towards the target surface 11 of the article 10.
- some of the cleaning material 25 may enter one or more of the passageways 12 from the second side 19 of the article 10.
- some of the cleaning material 25, and more particularly any particulates e.g., sand, shot, abrasives, etc.
- the part cleaner 20 may be used for a variety of applications to clean the target surface 11 of the article 10.
- the part cleaner 20 may be used to remove dirt or other contaminants prior to applying a new coat.
- the part cleaner 20 may be used to remove a previously applied coating that has since been worn and/or damaged.
- the part cleaner 20 may be used to remove part or all of a TBC on the target surface 11 before reapplying or rejuvenating the TBC.
- the part cleaner 20 may be used to remove one or more metallic coatings, contamination layers (e.g., rust, dirt, oxidation, etc.), diffused layers or other unwanted layers. While specific embodiments have been presented herein, it should be appreciated that these are exemplary only and any other application of the part cleaner 20 as part of the pressurized masking system 100 may also be realized.
- the pressurized masking system 100 further comprises a pressure masker 30.
- the pressure masker 30 comprises a fluid connection 31 that fluidly connects a source of masking fluid 35 to at least one passageway 12 of the article 10.
- fluid connection refers to a connection that allows the pressurized masking fluid 35 to pass from the pressure masker 30 to the passageway 12 with negligent loss to the outside environment.
- the fluid connection can comprise, for example, flexible tubes, hoses, pipes or any other conduit that directs the passage of the pressurized masking fluid 35 to the one or more passageways 12.
- the fluid connection 31 may comprise a tube that directly connects the output of the pressure masker 30 to the first side 18 of the passageway 12.
- the fluid connection 31 may comprise a single tube between the pressure masker 30 and a single passageway 12 (such as that illustrated in FIG. 2 ).
- the fluid connection may comprise a single tube leaving the pressure masker 30 that breaks off into segments that connect to a plurality of passageways 12 (such as that illustrated in FIG. 1 ).
- the fluid connection 31 may comprise a plurality of tubes leaving the pressure masker 30 that connects to a single or a plurality of passageways 12.
- the fluid connection 31 may comprise a plurality of channels of similar or dissimilar pressurized masking fluids 35 that connect to two or more passageways.
- the plurality of channels may comprise different pressures, temperatures, directions or mixtures of pressurized masking fluids 35.
- the fluid connection 31 of the invention comprises a multi-outlet manifold connection 40 comprising an internal passage 41 that can receive pressurized masking fluid 35 from the pressure masker 30 and fluidly distribute it to one or more passageways.
- the multi-outlet manifold connection 40 can thereby attach directly to the first side 18 of the article 10 and distribute the pressurized masking fluid 35 to a wide area about the article 10. Any passageways 12 within that area will thereby have pressurized masking fluid 35 fluidly pass there through.
- the pressurized masking fluid 35 can comprise any medium that can pass through the passageway 12 with a positive energy and prevent the permanent altering of a cross sectional area of the at least one passageway by the cleaning material 25 (or particulates thereof).
- "prevent the permanent altering of a cross sectional area" refers to removing and/or preventing substantially all of the cleaning material 25 that may enter the passageway 12 so that the cross sectional area of the passageway is not substantially reduced by a permanent obstruction 32 or increased due to erosion, deformation or the like.
- obstructions that would permanently alter the cross sectional area of the passageway 12 include, for example, large particulates lodged against a wall, a clumping of cleaning material 25 or the like.
- the pressurized masking fluid 35 may thereby comprise any material that can be forced through the one or more passageways 12 at a masking pressure to impact on and remove potential obstructions 32 from the cleaning material 25 that would alter the cross sectional area.
- the pressurized masking fluid 35 may comprise a gas such as inert gas or nitrogen.
- a gas such as inert gas or nitrogen.
- the pressurized masking fluid 35 may comprise water with or without abrasives distributed therein.
- the part cleaner 20 comprises a water jet or similar device. While specific embodiments of pressurized masking fluid and part cleaners have been presented herein, it should be appreciated that additional and alternative pressurized masking fluids and part cleaners may also be realized.
- the pressurized masking fluid 35 may comprise a masking pressure that is greater than, equal to, or less than a cleaning pressure of the cleaning material so long as the pressurized masking fluid 35 has enough energy to remove obstructions 32 from the passageways 12.
- the masking pressure may comprise a negative pressure (such as via a vacuum or suction element on the second side 19 of the article 10 such that the negative pressure pulls the pressurized masking fluid 35 through the passageway 12.
- the masking pressure may comprise a variable pressure that fluctuates during the masking process.
- the pressure masker 30 thereby passes the pressurized masking fluid 35 through the at least one passageway 12 at a masking pressure from the first side 18 to the second side 19 (wherein the second side 19 comprises the target surface 11 of the article 10 that is to be cleaned).
- the part cleaner cleans the target surface 11 of the article 10 by projecting cleaning material 25 towards the target surface.
- some of the cleaning material 25 may enter one or more passageways 12 and form one or more obstructions 32.
- the obstructions 32 may comprise a grouping of particulates from the cleaning material that would decrease the cross sectional area of the passageway 12 and reduce the amount of air that could flow there through.
- the pressurized masking fluid 35 will contact the obstruction 32 and push it back out of the passageway 12.
- the pressurized masking fluid 35 may prevent any obstructions 32 from even entering the passageways 12 via the pressurized masking fluid 35 exiting the passageway 12 on the second side 19 of the article 10.
- a method 200 for pressure cleaning a target surface 11 of an article 10 comprising one or more passageways 12.
- the method 200 first comprises fluidly connecting the pressure masker 30 to a first side 18 of at least one passageway 12 of the article 10 in step 210.
- the fluid connection 31 comprises a multi-outlet manifold connection 40 and connect the pressure masker 30 to any number of passageways 12.
- the pressure masker 30 then passes pressurized masking fluid 35 through the at least one passageway from the first side 18 to the second side 19 in step 220.
- the part cleaner 20 cleans the target surface 11 on the second side 19 of the article 10 by projecting cleaning material 25 towards the target surface 11 in step 230.
- passing pressurized masking fluid 35 through the at least one passageway 12 in step 220 and cleaning the target surface 11 in step 230 may start and end simultaneously in or with relative delay.
- the pressurized masking fluid 35 may be passing through the passageway 12 in step 20 prior to the initiation of cleaning the target surface 11 in step 230.
- Such embodiments may prevent a buildup of obstructions 32 prior to activation of the pressure masker 30.
- the pressurized masking fluid 35 may continue to pass through the passageway 12 in step 220 after the article 10 is cleaned in step 230. Such embodiments may help ensure any obstacles 32 remaining in the passageways 12 after cleaning is complete in step 230 are still removed by the pressurized masking fluid 35.
- Another embodiment relates to a method of pressure cleaning a target surface of an article comprising one or more passageways.
- the method comprises fluidly connecting a pressure masker comprising pressurized masking fluid to a first side of at least one passageway, and passing the pressurized masking fluid through the at least one passageway from the first side to a second side comprising the target surface.
- the method further comprises cleaning the target surface by projecting a cleaning material towards the target surface.
- the pressurized masking fluid passing through the at least one passageway prevents the cleaning material from permanently altering a cross sectional area of the at least one passageway.
- the fluid connection comprises a multi-outlet manifold connection that connects to the first side and comprises an internal passage.
- the internal passage receives the pressurized masking fluid and fluidly distributes it to one or more passageways.
- the pressurized masking fluid comprises a gas, e.g., nitrogen.
- the method comprises cleaning the target surface by projecting the cleaning material towards the target surface.
- a grit blaster or shot peening device cleans the target surface using the cleaning material.
- the passageway comprises a cooling hole.
- the pressurized masking fluid comprises a liquid.
- the liquid comprises abrasives.
- the method comprises cleaning the target surface by projecting the cleaning material towards the target surface.
- a water jet cleans the target surface using the cleaning material.
- the method comprises cleaning the target surface by projecting the cleaning material towards the target surface.
- the pressurized masking fluid continues to pass through the at least one passageway after cleaning the target surface is complete.
- the method comprises cleaning the target surface by projecting the cleaning material towards the target surface.
- the pressurized masking fluid passes through the at least one passageway at a masking pressure that is less than a cleaning pressure of the cleaning material.
- the pressurized masking system comprises a pressure masker configured to fluidly connect to a first side of at least one passageway of the article and to pass a pressurized masking fluid through the passageway from the first side to a second side.
- the second side comprises the target surface.
- the system further comprises a part cleaner configured to project a cleaning material towards the target surface.
- the pressurized masking fluid prevents the cleaning material from permanently altering a cross sectional area of the at least one passageway.
- the fluid connection comprises a multi-outlet manifold connection that connects to the first side of the article and comprises an internal passage.
- the internal passage receives the pressurized masking fluid and fluidly distributes it to one or more passageways.
- the pressurized masking fluid comprises a gas or a liquid, e.g., the liquid comprising abrasives.
- the part cleaner comprises a grit blaster.
- the part cleaner comprises a shot peening device.
- the part cleaner comprises a water jet.
- the pressurized masking fluid passes through the at least one passageway at a masking pressure that is less than a cleaning pressure of the cleaning material.
- the target surface comprises a thermal barrier coating.
- the at least one passageway comprises a cooling hole.
- the article comprises a turbine component.
- pressurized masking systems may be used to clean the target surface of an article while preventing the permanent altering of a cross sectional area of one or more passageways.
- a fluid connection comprising a multi-outlet manifold connection between the pressure masker and the one or more passageways can prevent the need for physical masking barriers such as tape, wax, or the like, potentially providing a more efficient cleaning system.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Plasma & Fusion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Physics & Mathematics (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Details Or Accessories Of Spraying Plant Or Apparatus (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Coating By Spraying Or Casting (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Cleaning In General (AREA)
Description
- Embodiments of the subject matter disclosed herein relate to masking systems. Other embodiments relate to to pressure masking systems for cleaning articles with passageways.
- In gas turbine engines, such as aircraft engines for example, air is drawn into the front of the engine, compressed by a shaft-mounted rotary-type compressor, and mixed with fuel. The mixture is burned, and the hot exhaust gases are passed through a turbine mounted on a shaft. The flow of gas turns the turbine, which turns the shaft and drives the compressor and fan. The hot exhaust gases flow from the back of the engine, driving it and the aircraft forward.
- During operation of gas turbine engines, the temperatures of combustion gases may exceed 3000°F (about 1650°C), considerably higher than the melting temperatures of the metal parts of the engine which are in contact with these gases. Operation of these engines at gas temperatures that are above the metal part melting temperatures is a well-established art, and depends in part on supplying a cooling air to the outer surfaces of the metal parts through various methods. The metal parts of these engines that are particularly subject to high temperatures, and thus require particular attention with respect to cooling, are the metal parts forming combustors and parts located aft of the combustor.
- The metal temperatures can be maintained below melting levels by using passageways such as cooling holes incorporated into some engine components. Sometimes, a thermal barrier coatings ("TBC") may also be applied to the component by a pressure coating process (e.g., a thermal spray process). However, the thermal spray process and other cleaning processes (e.g., grit blasting, shot peening, water jet washing) often results in overspray that partially or completely blocks the component's cooling holes.
- As a result, present coating (e.g., thermal spray) and cleaning processes involve a multi-step, highly labor intensive process of applying a partial layer of TBC coating, allowing the component and the TBC to sufficiently cool to a temperature at which the component can easily be handled, removing the component from an application fixture on which the thermal spraying takes place, and removing any masking, which is then followed by separately removing the well-cooled, solidified coating from the cooling holes using a water jet or other cleaning methods. To prevent the cooling holes from becoming obstructed beyond a level from which they can be satisfactorily cleaned, only a fraction of the desired TBC thickness is applied prior to cleaning. As a result, the entire process must typically be repeated several times until the desired TBC thickness is reached. This complex process results in low productivity, high cycle time, and increases costs by a factor of five to ten times that of applying the same TBC to a similar non-holed part. Even when coatings are not applied, the pressure cleaning methods used to clean the target surfaces of articles can similarly overflow and obstruct the article's cooling holes.
-
EP 1645363 A1 discloses a smoothing process that smooths the surface of a component such as a turbine blade by jet treatment with a high pressure fluid jet containing solid particles. While the component is being treated by the high pressure fluid jet, it is kept in a fluid-filled container. The fluid container has a fluid input and a solid particle input. - Accordingly, alternative pressure masking systems would be welcomed in the art.
- A method in accordance with the invention as hereinafter claimed of pressure cleaning a target surface of an article comprising one or more passageways comprises the steps of
claim 10 below. - A pressurized masking system in accordance with the invention as hereinafter claimed for cleaning a target surface of an article comprising passageways comprises the features of claim 1 below.
- These and additional features provided by the embodiments discussed herein will be more fully understood in view of the following detailed description, in conjunction with the drawings.
- The embodiments set forth in the drawings are illustrative and exemplary in nature and not intended to limit the inventions defined by the claims. The following detailed description of the illustrative embodiments can be understood when read in conjunction with the following drawings, where like structure is indicated with like reference numerals and in which:
-
FIG. 1 is a schematic illustrated of a pressure masking system according to one or more embodiments shown or described herein; -
FIG. 2 is a perspective view of a pressure masking system according to one or more embodiments shown or described herein; -
FIG. 3 is a perspective view of another pressure masking system according to one or more embodiments shown or described herein; -
FIG. 4 is a flowchart illustrating a method of pressure cleaning an article using a pressure masking system according to one or more embodiments shown or described herein. - One or more specific embodiments of the present invention will be described below. In an effort to provide a concise description of these embodiments, all features of an actual implementation may not be described in the specification. It should be appreciated that in the development of any such actual implementation, as in any engineering or design project, numerous implementation-specific decisions must be made to achieve the developers' specific goals, such as compliance with system-related and business-related constraints, which may vary from one implementation to another. Moreover, it should be appreciated that such a development effort might be complex and time consuming, but would nevertheless be a routine undertaking of design, fabrication, and manufacture for those of ordinary skill having the benefit of this disclosure.
- When introducing elements of various embodiments of the present invention, the articles "a," "an," "the," and "said" are intended to mean that there are one or more of the elements. The terms "comprising," "including," and "having" are intended to be inclusive and mean that there may be additional elements other than the listed elements.
- Pressurized masking systems disclosed herein generally comprise a pressure masker, and a part cleaner to clean the target surface of an article comprising passageways. While the part cleaner projects cleaning material towards the target surface, pressurized masking fluid is fluidly connected to the passageways and passed there through to prevent the permanent altering of a cross sectional area of the passageways by the cleaning material. Pressurized masking systems, and methods of pressure cleaning a target surface of an article, will be discussed in more detail herein.
- Referring now to
FIGS. 1-3 , a pressurizedmasking system 100 is illustrated comprising apart cleaner 20 and apressure masker 30 for cleaning anarticle 10. Thearticle 10 comprises one ormore passageways 12 passing through thearticle 10 from afirst side 18 to asecond side 19. As discussed above, thearticle 10 can comprise a variety of different parts such as a combustor liner or other component of a gas turbine engine. In some embodiments, thearticle 10 can comprise a turbine component such as a hot gas path component or a combustion component. Thepassageways 12 can comprise any passage through the article 10 (passing from thefirst side 18 to the second side 19) that is intended to remain open (such that air can pass through) when thearticle 10 is in use. For example, in some embodiments thepassageways 12 may comprise cooling holes. - As best illustrated in
FIGS. 2-3 , thesecond side 19 of thearticle 10 comprises atarget surface 11 that is to be cleaned. Thetarget surface 11 may be cleaned prior to first use, during routine or repair maintenance, or as otherwise necessary depending on the life of thearticle 10. As used herein, "cleaned" refers to stripping, washing and/or treating the target surface such as through grit blasting, shot peening, water jet washing or the like as will become appreciated herein. For example, in some embodiments thetarget surface 11 of thearticle 10 may comprise acoating 22 or other debris that is to be removed prior to applying a fresh coating. - In some embodiments, such as when the
article 10 comprises a metal hot gas path component, thetarget surface 11 of thearticle 10 may have or will have a thermal barrier coating ("TBC") disposed thereon. The TBC can comprise one or more layers of metal and/or ceramic coating material applied to thetarget surface 11 of thearticle 10 to impede the transfer of heat from hot combustion gases to thearticle 10, thus insulating the component from the hot combustion gas. The presence of the TBC on the surface permits the combustion gas to be hotter than would otherwise be possible with the particular material and fabrication process of the component. Any suitable composition of TBC may be applied. For example, in some embodiments the TBC can comprise a bond layer of MCrAlY, wherein M is preferably Ni, Co, or a combination thereof, followed by a layer of yttria stabilized zirconia (YSZ). - In some embodiments, the
article 10 may be disposed on a support stand 15 prior to or during the pressure cleaning as will become appreciated herein. The support stand 15 may be stationary or mobile (e.g., rotatable) and position thearticle 10 relative to thepart cleaner 20 and thepressure masker 30 when cleaning thetarget surface 11 of thearticle 10. - Still referring to
FIGS. 1-3 , the pressurizedmasking system 100 further comprises thepart cleaner 20. Thepart cleaner 20 comprises any device that projects acleaning material 25 towards thetarget surface 11 of thearticle 10. For example, in some embodiments, the part cleaner 20 can comprise a grit blaster. In such embodiments, thecleaning material 25 can comprise pressurized air with aluminum oxide, walnut shells, dry ice, charcoal, or any other particulates dispersed therein. In other embodiments, thepart cleaner 20 can comprise a shot peening device. In such embodiments, the cleaningmaterial 25 can comprise pressurized air with metallic, glass or ceramic particles dispersed therein. In even other embodiments, thepart cleaner 20 may comprise a pressure washer. In such embodiments, the cleaningmaterial 25 may comprise water with or without an additional abrasive material. - The
part cleaner 20 may be disposed at any position relative to thearticle 10 that allows for the cleaning of thetarget surface 11. For example, as illustrated inFIG. 1 , in some embodiments thearticle 10 may be disposed on asupport stand 15 adjacent thepart cleaner 20. The support stand 15 may then be able to rotate or otherwise displace thearticle 10 with respect to thepart cleaner 20 and/or thepart cleaner 20 may be able to articulate with respect to thearticle 10. Thepart cleaner 20 may then be used to project the cleaningmaterial 25 towards thetarget surface 11 of thearticle 10. However, as a result of cleaningmaterial 25 being projected toward thetarget surface 11 of thearticle 10, some of the cleaningmaterial 25 may enter one or more of thepassageways 12 from thesecond side 19 of thearticle 10. As such, some of the cleaningmaterial 25, and more particularly any particulates (e.g., sand, shot, abrasives, etc.), may potentially formobstructions 32 in the one ormore passageways 12 if left unopposed. - The
part cleaner 20 may be used for a variety of applications to clean thetarget surface 11 of thearticle 10. For example in some embodiments thepart cleaner 20 may be used to remove dirt or other contaminants prior to applying a new coat. In some embodiments, thepart cleaner 20 may be used to remove a previously applied coating that has since been worn and/or damaged. For example, in some embodiments thepart cleaner 20 may be used to remove part or all of a TBC on thetarget surface 11 before reapplying or rejuvenating the TBC. In some embodiments, thepart cleaner 20 may be used to remove one or more metallic coatings, contamination layers (e.g., rust, dirt, oxidation, etc.), diffused layers or other unwanted layers. While specific embodiments have been presented herein, it should be appreciated that these are exemplary only and any other application of thepart cleaner 20 as part of thepressurized masking system 100 may also be realized. - Referring still to
FIGS. 1-3 , thepressurized masking system 100 further comprises apressure masker 30. Thepressure masker 30 comprises afluid connection 31 that fluidly connects a source of maskingfluid 35 to at least onepassageway 12 of thearticle 10. As used herein, "fluid connection" refers to a connection that allows the pressurized maskingfluid 35 to pass from thepressure masker 30 to thepassageway 12 with negligent loss to the outside environment. The fluid connection can comprise, for example, flexible tubes, hoses, pipes or any other conduit that directs the passage of the pressurized maskingfluid 35 to the one ormore passageways 12. - In
FIG. 2 , thefluid connection 31 may comprise a tube that directly connects the output of thepressure masker 30 to thefirst side 18 of thepassageway 12. In some cases, thefluid connection 31 may comprise a single tube between thepressure masker 30 and a single passageway 12 (such as that illustrated inFIG. 2 ). In other cases, the fluid connection may comprise a single tube leaving thepressure masker 30 that breaks off into segments that connect to a plurality of passageways 12 (such as that illustrated inFIG. 1 ). In even other cases, thefluid connection 31 may comprise a plurality of tubes leaving thepressure masker 30 that connects to a single or a plurality ofpassageways 12. For example, thefluid connection 31 may comprise a plurality of channels of similar or dissimilarpressurized masking fluids 35 that connect to two or more passageways. Moreover, the plurality of channels may comprise different pressures, temperatures, directions or mixtures of pressurized maskingfluids 35. - Refering now to
FIG. 3 , thefluid connection 31 of the invention comprises amulti-outlet manifold connection 40 comprising aninternal passage 41 that can receive pressurized masking fluid 35 from thepressure masker 30 and fluidly distribute it to one or more passageways. Themulti-outlet manifold connection 40 can thereby attach directly to thefirst side 18 of thearticle 10 and distribute the pressurized maskingfluid 35 to a wide area about thearticle 10. Anypassageways 12 within that area will thereby have pressurized maskingfluid 35 fluidly pass there through. - The
pressurized masking fluid 35 can comprise any medium that can pass through thepassageway 12 with a positive energy and prevent the permanent altering of a cross sectional area of the at least one passageway by the cleaning material 25 (or particulates thereof). As used herein, "prevent the permanent altering of a cross sectional area" (and variants thereof), in the context of a cleaning operation, refers to removing and/or preventing substantially all of the cleaningmaterial 25 that may enter thepassageway 12 so that the cross sectional area of the passageway is not substantially reduced by apermanent obstruction 32 or increased due to erosion, deformation or the like. Examples of obstructions that would permanently alter the cross sectional area of thepassageway 12 include, for example, large particulates lodged against a wall, a clumping of cleaningmaterial 25 or the like. Thepressurized masking fluid 35 may thereby comprise any material that can be forced through the one ormore passageways 12 at a masking pressure to impact on and removepotential obstructions 32 from the cleaningmaterial 25 that would alter the cross sectional area. - For example, in some embodiments, the pressurized masking
fluid 35 may comprise a gas such as inert gas or nitrogen. Such embodiments may be realized when thepart cleaner 20 comprises a grit blaster or shot peening device such that the gas can counter any sand, peen or other cleaning particulate from thepart cleaner 20 that enters thepassageway 12 and remove it therefrom. In some embodiments, the pressurized maskingfluid 35 may comprise water with or without abrasives distributed therein. Such embodiments may be realized when thepart cleaner 20 comprises a water jet or similar device. While specific embodiments of pressurized masking fluid and part cleaners have been presented herein, it should be appreciated that additional and alternative pressurized masking fluids and part cleaners may also be realized. Moreover, the pressurized maskingfluid 35 may comprise a masking pressure that is greater than, equal to, or less than a cleaning pressure of the cleaning material so long as thepressurized masking fluid 35 has enough energy to removeobstructions 32 from thepassageways 12. In other embodiments, the masking pressure may comprise a negative pressure (such as via a vacuum or suction element on thesecond side 19 of thearticle 10 such that the negative pressure pulls the pressurized maskingfluid 35 through thepassageway 12. In some embodiments, the masking pressure may comprise a variable pressure that fluctuates during the masking process. - In operation, the
pressure masker 30 thereby passes the pressurized maskingfluid 35 through the at least onepassageway 12 at a masking pressure from thefirst side 18 to the second side 19 (wherein thesecond side 19 comprises thetarget surface 11 of thearticle 10 that is to be cleaned). Likewise, the part cleaner cleans thetarget surface 11 of thearticle 10 by projecting cleaningmaterial 25 towards the target surface. As a result of flow pattern distributions, some of the cleaningmaterial 25 may enter one ormore passageways 12 and form one ormore obstructions 32. For example, theobstructions 32 may comprise a grouping of particulates from the cleaning material that would decrease the cross sectional area of thepassageway 12 and reduce the amount of air that could flow there through. However, to prevent thecleaning material 25 from permanently obstructing the at least one passageway 12 (and altering its cross sectional area), the pressurized maskingfluid 35 will contact theobstruction 32 and push it back out of thepassageway 12. In some embodiments, the pressurized maskingfluid 35 may prevent anyobstructions 32 from even entering thepassageways 12 via the pressurized maskingfluid 35 exiting thepassageway 12 on thesecond side 19 of thearticle 10. - Referring now to
FIGS. 1-4 , amethod 200 is illustrated for pressure cleaning atarget surface 11 of anarticle 10 comprising one ormore passageways 12. Themethod 200 first comprises fluidly connecting thepressure masker 30 to afirst side 18 of at least onepassageway 12 of thearticle 10 instep 210. As discussed above, thefluid connection 31 comprises amulti-outlet manifold connection 40 and connect thepressure masker 30 to any number ofpassageways 12. Thepressure masker 30 then passespressurized masking fluid 35 through the at least one passageway from thefirst side 18 to thesecond side 19 instep 220. Likewise, thepart cleaner 20 cleans thetarget surface 11 on thesecond side 19 of thearticle 10 by projecting cleaningmaterial 25 towards thetarget surface 11 instep 230. - It should be appreciated that passing pressurized masking
fluid 35 through the at least onepassageway 12 instep 220 and cleaning thetarget surface 11 instep 230 may start and end simultaneously in or with relative delay. For example, in some embodiments the pressurized maskingfluid 35 may be passing through thepassageway 12 instep 20 prior to the initiation of cleaning thetarget surface 11 instep 230. Such embodiments may prevent a buildup ofobstructions 32 prior to activation of thepressure masker 30. In some embodiments, the pressurized maskingfluid 35 may continue to pass through thepassageway 12 instep 220 after thearticle 10 is cleaned instep 230. Such embodiments may help ensure anyobstacles 32 remaining in thepassageways 12 after cleaning is complete instep 230 are still removed by the pressurized maskingfluid 35. - Another embodiment relates to a method of pressure cleaning a target surface of an article comprising one or more passageways. The method comprises fluidly connecting a pressure masker comprising pressurized masking fluid to a first side of at least one passageway, and passing the pressurized masking fluid through the at least one passageway from the first side to a second side comprising the target surface. The method further comprises cleaning the target surface by projecting a cleaning material towards the target surface. The pressurized masking fluid passing through the at least one passageway prevents the cleaning material from permanently altering a cross sectional area of the at least one passageway.
- The fluid connection comprises a multi-outlet manifold connection that connects to the first side and comprises an internal passage. The internal passage receives the pressurized masking fluid and fluidly distributes it to one or more passageways.
- In another embodiment, the pressurized masking fluid comprises a gas, e.g., nitrogen.
- In another embodiment, the method comprises cleaning the target surface by projecting the cleaning material towards the target surface. A grit blaster or shot peening device cleans the target surface using the cleaning material.
- In another embodiment, the passageway comprises a cooling hole.
- In another embodiment, the pressurized masking fluid comprises a liquid.
- In another embodiment, the liquid comprises abrasives.
- In another embodiment, the method comprises cleaning the target surface by projecting the cleaning material towards the target surface. A water jet cleans the target surface using the cleaning material.
- In another embodiment, the method comprises cleaning the target surface by projecting the cleaning material towards the target surface. The pressurized masking fluid continues to pass through the at least one passageway after cleaning the target surface is complete.
- In another embodiment, the method comprises cleaning the target surface by projecting the cleaning material towards the target surface. The pressurized masking fluid passes through the at least one passageway at a masking pressure that is less than a cleaning pressure of the cleaning material.
- Another embodiment relates to a pressurized masking system for cleaning a target surface of an article comprising passageways. The pressurized masking system comprises a pressure masker configured to fluidly connect to a first side of at least one passageway of the article and to pass a pressurized masking fluid through the passageway from the first side to a second side. The second side comprises the target surface. The system further comprises a part cleaner configured to project a cleaning material towards the target surface. The pressurized masking fluid prevents the cleaning material from permanently altering a cross sectional area of the at least one passageway.
- The fluid connection comprises a multi-outlet manifold connection that connects to the first side of the article and comprises an internal passage. The internal passage receives the pressurized masking fluid and fluidly distributes it to one or more passageways.
- In another embodiment of the pressurized masking system, the pressurized masking fluid comprises a gas or a liquid, e.g., the liquid comprising abrasives.
- In another embodiment where the pressurized masking system includes the part cleaner, the part cleaner comprises a grit blaster.
- In another embodiment where the pressurized masking system includes the part cleaner, the part cleaner comprises a shot peening device.
- In another embodiment where the pressurized masking system includes the part cleaner, the part cleaner comprises a water jet.
- In another embodiment where the pressurized masking system includes the part cleaner configured to project the cleaning material towards the target surface, the pressurized masking fluid passes through the at least one passageway at a masking pressure that is less than a cleaning pressure of the cleaning material.
- In another embodiment of the pressurized masking system, the target surface comprises a thermal barrier coating.
- In another embodiment of the pressurized masking system, the at least one passageway comprises a cooling hole.
- In another embodiment of the pressurized masking system, the article comprises a turbine component.
- It should now be appreciated that pressurized masking systems may be used to clean the target surface of an article while preventing the permanent altering of a cross sectional area of one or more passageways. The use of a fluid connection comprising a multi-outlet manifold connection between the pressure masker and the one or more passageways can prevent the need for physical masking barriers such as tape, wax, or the like, potentially providing a more efficient cleaning system.
- While the invention has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the invention is not limited to such disclosed embodiments. Rather, the invention can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the scope of the invention. Additionally, while various embodiments of the invention have been described, it is to be understood that aspects of the invention may include only some of the described embodiments. Accordingly, the invention is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.
Claims (11)
- A pressurized masking system (100; 1000) for cleaning a target surface (11) of an article (10) comprising passageways (12), the pressurized masking system comprising:a pressure masker (30; 1030) configured to fluidly connect to a first side (18) of at least one passageway (12) of the article (10) and to pass a pressurized masking fluid (35; 1035) through the passageway from the first side (18) to a second side (19), wherein the second side (19) comprises the target surface (11); anda part cleaner (20) configured to project a cleaning material (25) towards the target surface, wherein the pressurized masking fluid (35; 1035) prevents the cleaning material from permanently altering a cross sectional area of the at least one passageway (12), characterized in thatthe fluid connection comprises a multi-outlet manifold connection (40) that connects to the first side of the article and comprises an internal passage, wherein the internal passage receives the pressurized masking fluid and fluidly distributes it to one or more passageways.
- The pressurized masking system of claim 1, wherein the pressurized masking fluid comprises a gas.
- The pressurized masking system of claim 2, wherein the part cleaner (20) comprises one or more of: a grit blaster; a shot peening device; a water jet and a thermal spray gun.
- The pressurized masking system of claim 1, wherein the part cleaner (20) is configured to project the cleaning material (25) towards the target surface (11), and wherein the pressurized masking fluid (35) passes through the at least one passageway (12) at a masking pressure that is less than a cleaning pressure of the cleaning material (25).
- The pressurized masking system of claim 1, wherein the target surface (11) comprises a thermal barrier coating.
- The pressurized masking system of claim 1, wherein the pressurized masking fluid comprises a liquid.
- The pressurized masking system of claim 1, wherein the at least one passageway (12) comprises a cooling hole.
- The pressurized masking system of claim 1, wherein the pressurized fluid comprises a liquid comprising abrasives.
- Use of the pressurized masking system (100; 1000) of any preceding claim for pressure cleaning a target surface of an article comprising one or more passageways.
- A method for pressure cleaning a target surface of an article comprising one or more passageways, the method comprising:fluidly connecting (210; 2010) a pressure masker comprising pressurized masking fluid to a first side of at least one passageway;passing (220; 2020) the pressurized masking fluid through the at least one passageway from the first side to a second side comprising the target surface; and,cleaning (230) the target surface by projecting a cleaning material towards the target surface, wherein the pressurized masking fluid passing through the at least one passageway prevents the cleaning material from permanently altering a cross sectional area of the at least one passageway, characterized in thatthe fluid connection comprises a multi-outlet manifold connection that connects to the first side and comprises an internal passage, wherein the internal passage receives the pressurized masking fluid and fluidly distributes it to one or more passageways.
- The method of claim 10, wherein the method comprises cleaning the target surface by projecting the cleaning material towards the target surface, and wherein one of:the pressurized masking fluid continues to pass through the at least one passageway after cleaning the target surface is complete, andthe pressurized masking fluid passes through the at least one passageway at a masking pressure that is less than a cleaning pressure of the cleaning material.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/339,468 US20130167870A1 (en) | 2011-12-29 | 2011-12-29 | Pressure masking systems and methods for using the same |
| US13/339,449 US8887662B2 (en) | 2011-12-29 | 2011-12-29 | Pressure masking systems and methods for using the same |
| PCT/US2012/071798 WO2013101921A2 (en) | 2011-12-29 | 2012-12-27 | Pressure masking systems and methods for using the same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2798095A2 EP2798095A2 (en) | 2014-11-05 |
| EP2798095B1 true EP2798095B1 (en) | 2022-07-20 |
Family
ID=47604140
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP12818755.6A Active EP2798095B1 (en) | 2011-12-29 | 2012-12-27 | Pressure masking systems and methods for using the same |
Country Status (4)
| Country | Link |
|---|---|
| EP (1) | EP2798095B1 (en) |
| JP (1) | JP6220346B2 (en) |
| CN (1) | CN104024465A (en) |
| WO (1) | WO2013101921A2 (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6235449B2 (en) * | 2014-12-03 | 2017-11-22 | 三菱日立パワーシステムズ株式会社 | Thermal spray coating method, turbine high-temperature component, turbine, thermal spray coating masking pin, and masking member |
| CN106269648A (en) * | 2016-08-29 | 2017-01-04 | 中航动力股份有限公司 | A kind of ceramic layer minimizing technology of thermal barrier coating |
| US10829845B2 (en) * | 2017-01-06 | 2020-11-10 | General Electric Company | Selective thermal coating of cooling holes with air flow |
| FR3070693B1 (en) * | 2017-09-07 | 2022-06-10 | Safran | COATING DEPOSIT METHOD AND DEVICE FOR MULTI-PERFORATED AIRCRAFT ENGINE COMPONENTS WITH VENT BLOWING |
| US10882158B2 (en) * | 2019-01-29 | 2021-01-05 | General Electric Company | Peening coated internal surfaces of turbomachine components |
| JP7686395B2 (en) * | 2020-12-28 | 2025-06-02 | 三菱重工航空エンジン株式会社 | Thermal barrier coating application method and heat-resistant member |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4402992A (en) * | 1981-12-07 | 1983-09-06 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Covering solid, film cooled surfaces with a duplex thermal barrier coating |
| FR2680120B1 (en) * | 1991-08-08 | 1995-03-24 | Snecma | METHOD AND DEVICE FOR COATING SURFACES PROVIDED WITH PROJECTION PERFORATIONS, PARTICULARLY FOR PLASMA METALLIZATION. |
| WO1999023273A1 (en) * | 1997-11-03 | 1999-05-14 | Siemens Aktiengesellschaft | Coating method and device |
| US6183811B1 (en) * | 1998-12-15 | 2001-02-06 | General Electric Company | Method of repairing turbine airfoils |
| US6158955A (en) * | 1999-06-03 | 2000-12-12 | General Electric Company | Welding method and assembly therefor |
| SG127668A1 (en) * | 1999-11-24 | 2006-12-29 | Gen Electric | Method for thermal barrier coating |
| DE50214917D1 (en) * | 2001-07-11 | 2011-04-07 | Alstom Technology Ltd | Process for coating a high-temperature-resistant component with a thermal protective layer and high-temperature-resistant component |
| CA2433613A1 (en) * | 2002-08-13 | 2004-02-13 | Russel J. Ruprecht, Jr. | Spray method for mcralx coating |
| EP1645363A1 (en) * | 2004-10-05 | 2006-04-12 | Siemens Aktiengesellschaft | Process and device for smoothing the surface of a workpiece |
| US7622160B2 (en) * | 2006-07-28 | 2009-11-24 | General Electric Company | Method for concurrent thermal spray and cooling hole cleaning |
| EP2439305A1 (en) * | 2010-10-07 | 2012-04-11 | Sulzer Metco AG | Thermal spray process avoiding the blockage of cooling holes in turbine components |
| US8460760B2 (en) * | 2010-11-30 | 2013-06-11 | United Technologies Corporation | Coating a perforated surface |
-
2012
- 2012-12-27 WO PCT/US2012/071798 patent/WO2013101921A2/en not_active Ceased
- 2012-12-27 EP EP12818755.6A patent/EP2798095B1/en active Active
- 2012-12-27 CN CN201280065042.2A patent/CN104024465A/en active Pending
- 2012-12-27 JP JP2014550460A patent/JP6220346B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| WO2013101921A2 (en) | 2013-07-04 |
| CN104024465A (en) | 2014-09-03 |
| JP2015509828A (en) | 2015-04-02 |
| WO2013101921A3 (en) | 2013-10-10 |
| EP2798095A2 (en) | 2014-11-05 |
| JP6220346B2 (en) | 2017-10-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP5355869B2 (en) | Simultaneous spraying and cooling hole cleaning methods | |
| US8985049B2 (en) | Pressure maskers and pressure masking systems | |
| EP2798095B1 (en) | Pressure masking systems and methods for using the same | |
| US7805822B2 (en) | Process for removing thermal barrier coatings | |
| EP3213827B1 (en) | Dry detergent and method for cleaning gas turbine engine components | |
| EP3213828B1 (en) | System and method for cleaning gas turbine engine components | |
| US8262802B2 (en) | Method of removing deposits | |
| JP6200740B2 (en) | Micro-channel coating deposition system and method of use | |
| JP2004332113A (en) | Method for performing thermal barrier coating or repairing the same | |
| EP2777827A2 (en) | Pressure masking systems and methods for using same in treating techniques | |
| US20130180952A1 (en) | Pressure masking systems and methods for using the same | |
| JP2016148322A (en) | Engine component and methods for engine component | |
| US5290364A (en) | Process for blast cleaning fixtures having internal passageways | |
| US8887662B2 (en) | Pressure masking systems and methods for using the same | |
| US9845703B2 (en) | Turbine component surface treatment processes and systems | |
| US20130167870A1 (en) | Pressure masking systems and methods for using the same | |
| HK1094175A (en) | Process for removing thermal barrier coatings | |
| HK1094175B (en) | Process for removing thermal barrier coatings | |
| BRPI0703007B1 (en) | Method of applying a thermal spray coating |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| 17P | Request for examination filed |
Effective date: 20140729 |
|
| AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| DAX | Request for extension of the european patent (deleted) | ||
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
| 17Q | First examination report despatched |
Effective date: 20171211 |
|
| GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
| INTG | Intention to grant announced |
Effective date: 20220217 |
|
| GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
| GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
| AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602012078504 Country of ref document: DE |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 1505581 Country of ref document: AT Kind code of ref document: T Effective date: 20220815 |
|
| REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
| REG | Reference to a national code |
Ref country code: NL Ref legal event code: FP |
|
| REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG9D |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20221121 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20221020 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 1505581 Country of ref document: AT Kind code of ref document: T Effective date: 20220720 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20221120 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20221021 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602012078504 Country of ref document: DE |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 |
|
| PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 |
|
| 26N | No opposition filed |
Effective date: 20230421 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
| REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20221231 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221227 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221231 Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221227 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221231 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 602012078504 Country of ref document: DE Owner name: GENERAL ELECTRIC TECHNOLOGY GMBH, CH Free format text: FORMER OWNER: GENERAL ELECTRIC COMPANY, SCHENECTADY, NY, US |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221231 |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: 732E Free format text: REGISTERED BETWEEN 20240222 AND 20240228 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20121227 |
|
| REG | Reference to a national code |
Ref country code: NL Ref legal event code: PD Owner name: GENERAL ELECTRIC TECHNOLOGY GMBH; CH Free format text: DETAILS ASSIGNMENT: CHANGE OF OWNER(S), ASSIGNMENT; FORMER OWNER NAME: GENERAL ELECTRIC COMPANY Effective date: 20240410 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220720 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20251119 Year of fee payment: 14 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20251126 Year of fee payment: 14 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20251119 Year of fee payment: 14 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20251119 Year of fee payment: 14 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20251120 Year of fee payment: 14 |