US20150159257A1 - Coating method, coating system, and coated article - Google Patents
Coating method, coating system, and coated article Download PDFInfo
- Publication number
- US20150159257A1 US20150159257A1 US14/097,940 US201314097940A US2015159257A1 US 20150159257 A1 US20150159257 A1 US 20150159257A1 US 201314097940 A US201314097940 A US 201314097940A US 2015159257 A1 US2015159257 A1 US 2015159257A1
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- Prior art keywords
- coating
- energy source
- substrate
- edge portion
- peripheral edge
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- 238000000576 coating method Methods 0.000 title claims abstract description 151
- 239000011248 coating agent Substances 0.000 title claims abstract description 127
- 230000002093 peripheral effect Effects 0.000 claims abstract description 73
- 239000000463 material Substances 0.000 claims abstract description 63
- 239000000758 substrate Substances 0.000 claims abstract description 62
- 239000007921 spray Substances 0.000 claims abstract description 20
- 238000005507 spraying Methods 0.000 claims abstract description 12
- 230000003247 decreasing effect Effects 0.000 claims description 10
- 238000007751 thermal spraying Methods 0.000 claims description 10
- 230000007547 defect Effects 0.000 claims description 5
- 238000010288 cold spraying Methods 0.000 claims description 4
- 238000002844 melting Methods 0.000 claims description 4
- 230000008018 melting Effects 0.000 claims description 4
- 239000000835 fiber Substances 0.000 claims description 2
- 238000010438 heat treatment Methods 0.000 claims description 2
- 230000007423 decrease Effects 0.000 description 9
- 238000000034 method Methods 0.000 description 5
- 230000001133 acceleration Effects 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical group [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910000943 NiAl Inorganic materials 0.000 description 1
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000011153 ceramic matrix composite Substances 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000011156 metal matrix composite Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 229910052702 rhenium Inorganic materials 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 229910000601 superalloy Inorganic materials 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- 229910052713 technetium Inorganic materials 0.000 description 1
- 239000006163 transport media Substances 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 238000010290 vacuum plasma spraying Methods 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
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
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
- B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
- B23K26/0604—Shaping the laser beam, e.g. by masks or multi-focusing by a combination of beams
- B23K26/0608—Shaping the laser beam, e.g. by masks or multi-focusing by a combination of beams in the same heat affected zone [HAZ]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
- B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
- B23K26/062—Shaping the laser beam, e.g. by masks or multi-focusing by direct control of the laser beam
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/14—Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
- B23K26/1462—Nozzles; Features related to nozzles
- B23K26/1464—Supply to, or discharge from, nozzles of media, e.g. gas, powder, wire
- B23K26/147—Features outside the nozzle for feeding the fluid stream towards the workpiece
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/34—Laser welding for purposes other than joining
- B23K26/342—Build-up welding
-
- 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
- C23C24/00—Coating starting from inorganic powder
- C23C24/02—Coating starting from inorganic powder by application of pressure only
- C23C24/04—Impact or kinetic deposition of particles
-
- 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
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
- C23C4/073—Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
-
- C23C4/085—
Definitions
- the present invention is directed to a coating method, a coating system and a coated article. More specifically, the present invention is directed to a hybrid spray coating method, a hybrid spray coating system, and a hybrid spray coated article.
- coated articles are formed through thermal spraying of a coating material.
- the coating material is directed towards a substrate at a high velocity.
- the coating material contacts the substrate at the high velocity, generating heat and forming a mechanical bond.
- a peripheral portion of the spray contacts the substrate at a decreased velocity as compared to a central portion of the spray.
- the decreased velocity of the peripheral portion of the spray decreases the heat generated by the spray.
- the coating formed from the peripheral portions of the spray cools at an increased rate, causing a poor mechanical bond between the coating and the substrate at such locations.
- One attempt to improve the bonding between the coating and the substrate includes a preheating of the substrate followed by thermal spraying.
- the preheating of the substrate could cause a formation of defects throughout the coating.
- a coating method, coating system and coated article that do not suffer from one or more of the above drawbacks would be desirable in the art.
- a coating method includes providing a substrate, directing a coating material towards the substrate, the coating material contacting a coating region of the substrate to form a coating deposit, providing an energy source, and directing the energy source towards a first peripheral edge portion and a second peripheral edge portion of the coating region.
- the directing of the energy source is concurrent with the directing of the coating material.
- a coating system in another exemplary embodiment, includes a substrate, a thermal spray nozzle directed towards the substrate, and an energy source directed towards the substrate.
- the energy source is configured to contact only a first peripheral edge portion and a second peripheral edge portion of a coating region of the substrate.
- a coated article in another exemplary embodiment, includes a substrate, and a uniform thermal spray coating over the substrate.
- the thermal spray coating is bonded mechanically to the substrate at all locations of coverage with an absence of defects.
- FIG. 1 is a side view of a coating method according to an embodiment of the disclosure.
- FIG. 2 is a top view of a coating method according to an embodiment of the disclosure.
- Embodiments of the present disclosure in comparison to processes and articles not using one or more of the features disclosed herein, increase bonding of a coating to a substrate, increase coating efficiency, decrease coating cost, decrease spray coating velocity, increase uniformity of the coating, remove coating defects such as cracking, or a combination thereof
- a coating method 100 includes providing a substrate 101 , providing an energy source 102 , and directing both a coating material 104 (e.g. powdered coating material) and the energy source 102 towards a coating region 105 of the substrate 101 without melting the coating material 104 , the substrate 101 , or the coating deposit 106 .
- the coating material 104 contacts the substrate 101 and forms a coating deposit 106 on the substrate 101 , while the energy source 102 provides heat to the substrate 101 , the coating material 104 , and/or the coating deposit 106 without preheating the substrate 101 .
- the coating material 104 is directed toward the coating region 105 by any suitable application method.
- one suitable application method includes directing the coating material 104 towards the substrate 101 by thermal spraying of the coating material 104 .
- Thermal spraying includes, but is not limited to, vacuum plasma spraying, high velocity oxy-fuel spraying, cold spraying, other thermal spraying methods, or a combination thereof.
- the coating deposit 106 is formed as application of the coating material 104 and the energy source 102 proceed in a direction of travel 201 .
- the application of the coating material 104 includes directing the coating material 104 towards the substrate 101 with a thermal spray nozzle 103 , which includes, but is not limited to, a cold spray nozzle.
- the thermal spray nozzle 103 accelerates the coating material 104 towards the substrate 101 with any suitable transport medium such as, but not limited to, nitrogen gas, non-oxidizing gas, inert gas, or a combination thereof without melting the substrate 101 or the coating material 104 .
- the coating material 104 includes any suitable composition for thermal spraying to form the coating deposit 106 .
- suitable compositions include, but are not limited to, metal matrix composites, ceramic matrix composites, high melt superalloys, bond coats such as MCrAlX, PtAl, NiAl, Pt(Ni)Al, or a combination thereof.
- the MCrAlX is an alloy having M selected from one or a combination of iron, nickel, cobalt, and combinations thereof and Cr is chromium, Al is aluminum, and X is an element selected from the group of solid solution strengtheners and gamma prime formers consisting of Y, Tc, Ta, Re, Mo, and W and grain boundary strengtheners consisting of B, C, Hf, Zr, and combinations thereof.
- the accelerated coating material 104 exiting the thermal spray nozzle 103 contacts the substrate 101 , generating heat which facilitates a mechanical bond between the coating material 104 and the substrate 101 .
- the mechanical bond between the coating material 104 and the substrate 101 forms the coating deposit 106 .
- the acceleration of the coating material 104 generates a predetermined velocity of the coating material 104 exiting the thermal spray nozzle 103 .
- the predetermined velocity is any suitable velocity capable of generating suitable heat for forming the coating deposit 106 .
- the predetermined velocity of the coating material 104 accelerated by the cold spray nozzle is up to about 1000 m/s.
- An increase or decrease in a velocity of the coating material 104 increases or decreases the heat generated by the coating material 104 contacting the substrate 101 , respectively.
- the velocity of the coating material 104 exiting the thermal spray nozzle 103 decreases slightly towards a periphery of the coating region 105 .
- the velocity of the coating material 104 contacting the periphery of the coating region 105 is decreased as compared to the rest of the coating region 105 , decreasing the heat generated in the first peripheral edge portion 107 and the second peripheral edge portion 108 .
- the conduction of heat generated by the process away from the coating region 105 increases at the periphery of the coating region 105 , accelerating cooling in the first peripheral edge portion 107 and the second peripheral edge portion 108 .
- the decreased heat generated by the decreased velocity and/or the accelerated cooling from the increased conduction cause the coating material 104 to bond to the first peripheral edge portion 107 and the second peripheral edge portion 108 at a peripheral bonding strength that is significantly reduced as compared to a non-peripheral bonding strength of the coating material in the rest of the coating region 105 .
- the non-peripheral bonding strength includes about 100 MPa, while the peripheral bonding strength includes, but is not limited to, up to about 90% of the non-peripheral bonding strength, between about 1% and about 90% of the non-peripheral bonding strength, between about 1% and about 80% of the non-peripheral bonding strength, between about 1% and about 50% of the non-peripheral bonding strength, between about 1% and about 25% of the non-peripheral bonding strength, between about 1% and about 10% of the non-peripheral bonding strength, between about 0.5% and about 5% of the non-peripheral bonding strength, or any combination, sub-combination, range, or sub-range thereof
- the non-peripheral bonding strength may vary between different materials and applications.
- the rapid movement of the reduced heat input at the edges is believed to contribute to formation of defects such as lack of bonding and cracks.
- the energy source 102 provides additional heat to the substrate 101 along the periphery, the coating material 104 , and/or the coating deposit 106 .
- the energy source 102 is any suitable energy source such as, but not limited to, a focused or defocused high energy beam, a diode laser, a CO 2 laser, a fiber laser, an electron beam, a disc laser, a scanning laser, or a combination thereof.
- the scanning laser is configured to increase the heat of the coating material 104 being applied to any suitable portion of the coating region 105 .
- the energy source 102 is positioned outside the thermal spray nozzle 103 , in any suitable configuration for increasing the heat of the coating material 104 being applied in the first peripheral edge portion 107 and the second peripheral edge portion 108 .
- a single energy source 102 provides a U-shaped beam which contacts the first peripheral edge portion 107 , the second peripheral edge portion 108 , and the coating deposit 106 trailing the thermal spray nozzle 103 .
- Alternate beam shapes include any suitable shape for increasing the heat of the coating material 104 being applied in the first peripheral edge portion 107 and the second peripheral edge portion 108 , such as, but not limited to, a rectangular-shaped beam, or a circular-shaped beam.
- a plurality of energy sources 102 provides one or more split beam(s) that contact at least the first peripheral edge portion 107 and the second peripheral edge portion 108 .
- at least two energy sources 102 provide at least one beam directed to either of the first peripheral edge portion 107 and the second peripheral edge portion 108 .
- a first beam 112 from the energy source 102 contacts the substrate 101 and the coating material 104 in the first peripheral edge portion 107
- a second beam 113 from the energy source 102 contacts the substrate 101 and the coating material 104 in the second peripheral edge portion 108 .
- the contacting of the energy source 102 with the first peripheral edge portion 107 and the second peripheral edge portion 108 provides heat to both the coating material 104 and the substrate 101 , without preheating the substrate 101 .
- the heat softens the first peripheral edge portion 107 and the second peripheral edge portion 108 , without melting the substrate 101 or the coating material 104 , to increase a mechanical bonding strength between the applied coating material 104 and the substrate 101 .
- the single beam from the energy source 102 may be split using optics, into a first beam 112 and a second beam 113 .
- the beam from the energy source 102 may be rapidly scanned along the first peripheral edge portion 107 and the second peripheral edge portion 108 as well as, optionally, the coating deposit 106 .
- the heat from the energy source 102 decreases a rate of cooling of the coating deposit 106 , permitting an increase in the deposition rate of the coating material 104 and/or decreasing or eliminating the formation of cracks in the coating deposit 106 .
- the increased heat from the contacting of the energy source 102 with the first peripheral edge portion 107 and the second peripheral edge portion 108 permits a decrease in acceleration of the coating material 104 .
- the energy source 102 provides any suitable amount of increased heat to replace the decreased heat from the decreased acceleration of the coating material 104 , and form the coating deposit 106 having uniform or substantially uniform mechanical bonding to the substrate 101 .
- a density of the coating deposit 106 in the first peripheral edge portion 107 and the second peripheral edge portion 108 is locally increased by the increased heat from the energy source 102 .
- the increased heat coalesces the coating material 104 during spraying, forming the increase in the density of the first peripheral edge portion 107 and the second peripheral edge portion 108 .
- the increase in the density of the first peripheral edge portion 107 and the second peripheral edge portion 108 forms a uniform or substantially uniform density in the applied coating deposit 106 .
- a positioning of the energy source 102 relative to the deposit 106 , a size of a width of the beam generated by the energy source 102 , a distance between two of the energy sources 102 , and a power range of the energy source 102 control a width of the coating deposit 106 formed by the application of the coating material 104 .
- the first peripheral edge portion 107 and the second peripheral edge portion 108 together are adjusted to occupy any suitable percentage of the coating region 105 , such as, but not limited to, up to about 40%, between about 1% and about 40%, between about 10% and about 40%, between about 20% and about 40%, between about 10% and about 30%, or any combination, sub-combination, range, or sub-range thereof.
- the first peripheral edge portion 107 and the second peripheral edge portion 108 are similar or substantially similar in size.
- the energy source 102 generates the beam having any suitable width and any suitable length for contacting the first peripheral edge portion 107 and/or the second peripheral edge portion 108 or otherwise scans these areas.
- Suitable widths of the beam include, but are not limited to, up to about 5 mm, between about 0.01 mm and about 5 mm, between about 0.1 mm and about 3 mm, up to about 2 mm, or any combination, sub-combination, range, or sub-range thereof.
- Suitable lengths of the beam include, but are not limited to, up to about 15 mm, up to about 10 mm, between about 0.1 and about 10 mm, or any combination, sub-combination, range, or sub-range thereof.
- the width and the length of the beam may vary with differing conditions, such as, but not limited to, the energy source 102 , the shape of the beam, or the size of the coating region 105 .
- the diode laser may produce the beam having the rectangular-shape and a width of between about 0.1 mm and about 1 mm
- the focused high energy beam may produce the beam having the circular-shape and a width of between about 0.1 mm and about 5 mm.
- the power range for the energy source 102 is adjusted based upon coating properties, such as, but not limited to, thickness, speed of application, velocity of application, coating region 105 size, energy source 102 orientation, or a combination thereof.
- coating properties such as, but not limited to, thickness, speed of application, velocity of application, coating region 105 size, energy source 102 orientation, or a combination thereof.
- the power range for the energy source 102 includes, but is not limited to, between about 0.1 kw and about 10 kw, between about 0.1 kw and about 6 kw, between about 0.5 kw and about 6 kw, or any combination, sub-combination, range, or sub-range thereof.
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Abstract
A coating method, coating system and coated article are provided. The coating method includes providing a substrate, directing a coating material towards the substrate, the coating material contacting a coating region of the substrate to form a coating deposit, providing an energy source, and directing the energy source towards a first peripheral edge portion and a second peripheral edge portion of the coating region. The directing of the energy source is concurrent with the directing of the coating material. The coating system includes a substrate, a thermal spray nozzle directed towards the substrate, and an energy source directed towards the substrate. The energy source is configured to contact only a first peripheral edge portion and a second peripheral edge portion of a coating region of the substrate. The coated article includes a substrate, and a uniform thermal spray coating mechanically bonded to the substrate.
Description
- The present invention is directed to a coating method, a coating system and a coated article. More specifically, the present invention is directed to a hybrid spray coating method, a hybrid spray coating system, and a hybrid spray coated article.
- Many coated articles are formed through thermal spraying of a coating material. During the thermal spraying, the coating material is directed towards a substrate at a high velocity. The coating material contacts the substrate at the high velocity, generating heat and forming a mechanical bond.
- During the thermal spraying of the coating material, a peripheral portion of the spray contacts the substrate at a decreased velocity as compared to a central portion of the spray. The decreased velocity of the peripheral portion of the spray decreases the heat generated by the spray. The coating formed from the peripheral portions of the spray cools at an increased rate, causing a poor mechanical bond between the coating and the substrate at such locations.
- One attempt to improve the bonding between the coating and the substrate includes a preheating of the substrate followed by thermal spraying. However, the preheating of the substrate could cause a formation of defects throughout the coating.
- A coating method, coating system and coated article that do not suffer from one or more of the above drawbacks would be desirable in the art.
- In an exemplary embodiment, a coating method includes providing a substrate, directing a coating material towards the substrate, the coating material contacting a coating region of the substrate to form a coating deposit, providing an energy source, and directing the energy source towards a first peripheral edge portion and a second peripheral edge portion of the coating region. The directing of the energy source is concurrent with the directing of the coating material.
- In another exemplary embodiment, a coating system includes a substrate, a thermal spray nozzle directed towards the substrate, and an energy source directed towards the substrate. The energy source is configured to contact only a first peripheral edge portion and a second peripheral edge portion of a coating region of the substrate.
- In another exemplary embodiment, a coated article includes a substrate, and a uniform thermal spray coating over the substrate. The thermal spray coating is bonded mechanically to the substrate at all locations of coverage with an absence of defects.
- Other features and advantages of the present invention will be apparent from the following more detailed description of the preferred embodiment, taken in conjunction with the accompanying drawings which illustrate, by way of example, the principles of the invention.
-
FIG. 1 is a side view of a coating method according to an embodiment of the disclosure. -
FIG. 2 is a top view of a coating method according to an embodiment of the disclosure. - Wherever possible, the same reference numbers will be used throughout the drawings to represent the same parts.
- Provided are a coating method, a coating system and a coated article. Embodiments of the present disclosure, in comparison to processes and articles not using one or more of the features disclosed herein, increase bonding of a coating to a substrate, increase coating efficiency, decrease coating cost, decrease spray coating velocity, increase uniformity of the coating, remove coating defects such as cracking, or a combination thereof
- Referring to
FIG. 1 andFIG. 2 , in one embodiment, a coating method 100 includes providing asubstrate 101, providing anenergy source 102, and directing both a coating material 104 (e.g. powdered coating material) and theenergy source 102 towards acoating region 105 of thesubstrate 101 without melting thecoating material 104, thesubstrate 101, or thecoating deposit 106. Thecoating material 104 contacts thesubstrate 101 and forms acoating deposit 106 on thesubstrate 101, while theenergy source 102 provides heat to thesubstrate 101, thecoating material 104, and/or thecoating deposit 106 without preheating thesubstrate 101. Thecoating material 104 is directed toward thecoating region 105 by any suitable application method. For example, one suitable application method includes directing thecoating material 104 towards thesubstrate 101 by thermal spraying of thecoating material 104. Thermal spraying includes, but is not limited to, vacuum plasma spraying, high velocity oxy-fuel spraying, cold spraying, other thermal spraying methods, or a combination thereof. - In one embodiment, the
coating deposit 106 is formed as application of thecoating material 104 and theenergy source 102 proceed in a direction oftravel 201. In another embodiment, the application of thecoating material 104 includes directing thecoating material 104 towards thesubstrate 101 with athermal spray nozzle 103, which includes, but is not limited to, a cold spray nozzle. Thethermal spray nozzle 103 accelerates thecoating material 104 towards thesubstrate 101 with any suitable transport medium such as, but not limited to, nitrogen gas, non-oxidizing gas, inert gas, or a combination thereof without melting thesubstrate 101 or thecoating material 104. - The
coating material 104 includes any suitable composition for thermal spraying to form thecoating deposit 106. Suitable compositions include, but are not limited to, metal matrix composites, ceramic matrix composites, high melt superalloys, bond coats such as MCrAlX, PtAl, NiAl, Pt(Ni)Al, or a combination thereof. The MCrAlX is an alloy having M selected from one or a combination of iron, nickel, cobalt, and combinations thereof and Cr is chromium, Al is aluminum, and X is an element selected from the group of solid solution strengtheners and gamma prime formers consisting of Y, Tc, Ta, Re, Mo, and W and grain boundary strengtheners consisting of B, C, Hf, Zr, and combinations thereof. - The accelerated
coating material 104 exiting thethermal spray nozzle 103 contacts thesubstrate 101, generating heat which facilitates a mechanical bond between thecoating material 104 and thesubstrate 101. The mechanical bond between thecoating material 104 and thesubstrate 101 forms thecoating deposit 106. Additionally, the acceleration of thecoating material 104 generates a predetermined velocity of thecoating material 104 exiting thethermal spray nozzle 103. The predetermined velocity is any suitable velocity capable of generating suitable heat for forming thecoating deposit 106. For example, in one embodiment, during cold spraying the predetermined velocity of thecoating material 104 accelerated by the cold spray nozzle is up to about 1000 m/s. An increase or decrease in a velocity of thecoating material 104 increases or decreases the heat generated by thecoating material 104 contacting thesubstrate 101, respectively. - In one embodiment, the velocity of the
coating material 104 exiting thethermal spray nozzle 103 decreases slightly towards a periphery of thecoating region 105. As such, the velocity of thecoating material 104 contacting the periphery of thecoating region 105 is decreased as compared to the rest of thecoating region 105, decreasing the heat generated in the firstperipheral edge portion 107 and the secondperipheral edge portion 108. In another embodiment, the conduction of heat generated by the process away from thecoating region 105 increases at the periphery of thecoating region 105, accelerating cooling in the firstperipheral edge portion 107 and the secondperipheral edge portion 108. The decreased heat generated by the decreased velocity and/or the accelerated cooling from the increased conduction cause thecoating material 104 to bond to the firstperipheral edge portion 107 and the secondperipheral edge portion 108 at a peripheral bonding strength that is significantly reduced as compared to a non-peripheral bonding strength of the coating material in the rest of thecoating region 105. For example, for a single pass, the non-peripheral bonding strength includes about 100 MPa, while the peripheral bonding strength includes, but is not limited to, up to about 90% of the non-peripheral bonding strength, between about 1% and about 90% of the non-peripheral bonding strength, between about 1% and about 80% of the non-peripheral bonding strength, between about 1% and about 50% of the non-peripheral bonding strength, between about 1% and about 25% of the non-peripheral bonding strength, between about 1% and about 10% of the non-peripheral bonding strength, between about 0.5% and about 5% of the non-peripheral bonding strength, or any combination, sub-combination, range, or sub-range thereof The non-peripheral bonding strength may vary between different materials and applications. - Without wishing to be bound by theory, the rapid movement of the reduced heat input at the edges is believed to contribute to formation of defects such as lack of bonding and cracks. In one embodiment, to increase the amount of mechanical bonding and/or decrease cracking seen with pre-heating of the
substrate 101, theenergy source 102 provides additional heat to thesubstrate 101 along the periphery, thecoating material 104, and/or thecoating deposit 106. - The
energy source 102 is any suitable energy source such as, but not limited to, a focused or defocused high energy beam, a diode laser, a CO2 laser, a fiber laser, an electron beam, a disc laser, a scanning laser, or a combination thereof. In one embodiment, the scanning laser is configured to increase the heat of thecoating material 104 being applied to any suitable portion of thecoating region 105. In an alternate embodiment, theenergy source 102 is positioned outside thethermal spray nozzle 103, in any suitable configuration for increasing the heat of thecoating material 104 being applied in the firstperipheral edge portion 107 and the secondperipheral edge portion 108. For example, in one embodiment, asingle energy source 102 provides a U-shaped beam which contacts the firstperipheral edge portion 107, the secondperipheral edge portion 108, and thecoating deposit 106 trailing thethermal spray nozzle 103. Alternate beam shapes include any suitable shape for increasing the heat of thecoating material 104 being applied in the firstperipheral edge portion 107 and the secondperipheral edge portion 108, such as, but not limited to, a rectangular-shaped beam, or a circular-shaped beam. In another embodiment, a plurality ofenergy sources 102 provides one or more split beam(s) that contact at least the firstperipheral edge portion 107 and the secondperipheral edge portion 108. In a further embodiment, at least twoenergy sources 102 provide at least one beam directed to either of the firstperipheral edge portion 107 and the secondperipheral edge portion 108. - In one embodiment, a
first beam 112 from theenergy source 102 contacts thesubstrate 101 and thecoating material 104 in the firstperipheral edge portion 107, and asecond beam 113 from theenergy source 102 contacts thesubstrate 101 and thecoating material 104 in the secondperipheral edge portion 108. The contacting of theenergy source 102 with the firstperipheral edge portion 107 and the secondperipheral edge portion 108 provides heat to both thecoating material 104 and thesubstrate 101, without preheating thesubstrate 101. The heat softens the firstperipheral edge portion 107 and the secondperipheral edge portion 108, without melting thesubstrate 101 or thecoating material 104, to increase a mechanical bonding strength between the appliedcoating material 104 and thesubstrate 101. The single beam from theenergy source 102 may be split using optics, into afirst beam 112 and asecond beam 113. In another embodiment, the beam from theenergy source 102 may be rapidly scanned along the firstperipheral edge portion 107 and the secondperipheral edge portion 108 as well as, optionally, thecoating deposit 106. - In one embodiment, the heat from the
energy source 102 decreases a rate of cooling of thecoating deposit 106, permitting an increase in the deposition rate of thecoating material 104 and/or decreasing or eliminating the formation of cracks in thecoating deposit 106. In another embodiment, the increased heat from the contacting of theenergy source 102 with the firstperipheral edge portion 107 and the secondperipheral edge portion 108 permits a decrease in acceleration of thecoating material 104. Theenergy source 102 provides any suitable amount of increased heat to replace the decreased heat from the decreased acceleration of thecoating material 104, and form thecoating deposit 106 having uniform or substantially uniform mechanical bonding to thesubstrate 101. - A density of the
coating deposit 106 in the firstperipheral edge portion 107 and the secondperipheral edge portion 108 is locally increased by the increased heat from theenergy source 102. The increased heat coalesces thecoating material 104 during spraying, forming the increase in the density of the firstperipheral edge portion 107 and the secondperipheral edge portion 108. In one embodiment, the increase in the density of the firstperipheral edge portion 107 and the secondperipheral edge portion 108 forms a uniform or substantially uniform density in the appliedcoating deposit 106. - A positioning of the
energy source 102 relative to thedeposit 106, a size of a width of the beam generated by theenergy source 102, a distance between two of theenergy sources 102, and a power range of theenergy source 102 control a width of thecoating deposit 106 formed by the application of thecoating material 104. The firstperipheral edge portion 107 and the secondperipheral edge portion 108 together are adjusted to occupy any suitable percentage of thecoating region 105, such as, but not limited to, up to about 40%, between about 1% and about 40%, between about 10% and about 40%, between about 20% and about 40%, between about 10% and about 30%, or any combination, sub-combination, range, or sub-range thereof. In another embodiment, the firstperipheral edge portion 107 and the secondperipheral edge portion 108 are similar or substantially similar in size. - The
energy source 102 generates the beam having any suitable width and any suitable length for contacting the firstperipheral edge portion 107 and/or the secondperipheral edge portion 108 or otherwise scans these areas. Suitable widths of the beam include, but are not limited to, up to about 5 mm, between about 0.01 mm and about 5 mm, between about 0.1 mm and about 3 mm, up to about 2 mm, or any combination, sub-combination, range, or sub-range thereof. Suitable lengths of the beam include, but are not limited to, up to about 15 mm, up to about 10 mm, between about 0.1 and about 10 mm, or any combination, sub-combination, range, or sub-range thereof. The width and the length of the beam may vary with differing conditions, such as, but not limited to, theenergy source 102, the shape of the beam, or the size of thecoating region 105. For example, the diode laser may produce the beam having the rectangular-shape and a width of between about 0.1 mm and about 1 mm, while the focused high energy beam may produce the beam having the circular-shape and a width of between about 0.1 mm and about 5 mm. - The power range for the
energy source 102 is adjusted based upon coating properties, such as, but not limited to, thickness, speed of application, velocity of application,coating region 105 size,energy source 102 orientation, or a combination thereof. For example, in one embodiment, during cold spraying of thecoating material 104 the power range for theenergy source 102 includes, but is not limited to, between about 0.1 kw and about 10 kw, between about 0.1 kw and about 6 kw, between about 0.5 kw and about 6 kw, or any combination, sub-combination, range, or sub-range thereof. - While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.
Claims (20)
1. A coating method, comprising:
providing a substrate;
directing a coating material towards the substrate, the coating material contacting a coating region of the substrate to form a coating deposit;
providing an energy source; and
directing the energy source towards a first peripheral edge portion and a second peripheral edge portion of the coating region;
wherein directing of the energy source is concurrent with the directing of the coating material.
2. The coating method of claim 1 , wherein directing the coating material towards the substrate further comprises thermal spraying the coating material.
3. The coating method of claim 2 , wherein thermal spraying the coating material further comprises cold spraying the coating material.
4. The coating method of claim 1 , wherein providing the energy source further comprises:
selecting the energy source from the group consisting of a focused high energy beam, a defocused high energy beam, and a laser beam;
wherein the laser beam is selected from the group consisting of a diode laser, a CO2 laser, a fiber laser, and a disc laser.
5. The coating method of claim 4 , wherein a laser energy of the laser beam comprises between 0.5 kw and 6 kw.
6. The coating method of claim 4 , wherein a beam width of the laser beam comprises between 0.1 mm and 5 mm.
7. The coating method of claim 1 , further comprising directing the energy source to increase a density of the coating deposit.
8. The coating method of claim 1 , comprising contacting the first peripheral edge portion and the second peripheral edge portion with the energy source.
9. The coating method of claim 8 , further comprising heating the coating material without melting the coating material.
10. The coating method of claim 1 , wherein providing the energy source further comprises providing a first energy source and a second energy source.
11. The coating method of claim 10 , further comprising adjusting a spacing between the first energy source and the second energy source to control a width of the coating deposit.
12. The coating method of claim 10 , comprising contacting the first peripheral edge portion with the first energy source and the second peripheral edge portion with the second energy source.
13. The coating method of claim 1 , comprising decreasing a velocity of the coating material contacting the coating region as compared to the coating method without the energy source.
14. A coating system, comprising:
a substrate;
a thermal spray nozzle directed towards the substrate; and
an energy source directed towards the substrate;
wherein the energy source is configured to contact only a first peripheral edge portion and a second peripheral edge portion of a coating region of the substrate.
15. The coating system of claim 14 , wherein the thermal spray nozzle comprises a cold spray nozzle.
16. The coating system of claim 14 , wherein the energy source comprises a first energy source and a second energy source.
17. The coating system of claim 14 , wherein the first peripheral edge portion and the second peripheral edge portion comprise up to 40% of the coating region.
18. The coating system of claim 17 , wherein a first peripheral edge portion size is equal to a second peripheral edge portion size.
19. A coated article, comprising:
a substrate; and
a uniform thermal spray coating over the substrate;
wherein the thermal spray coating is bonded mechanically to the substrate at all locations of coverage with an absence of defects.
20. The coated article of claim 19 , wherein the uniform thermal spray coating is a uniform cold spray coating.
Priority Applications (3)
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US14/097,940 US20150159257A1 (en) | 2013-12-05 | 2013-12-05 | Coating method, coating system, and coated article |
EP14195806.6A EP2881495A1 (en) | 2013-12-05 | 2014-12-02 | Coating method, coating system and coated article |
CN201410738287.8A CN104694867A (en) | 2013-12-05 | 2014-12-05 | Coating method, coating system and coated article |
Applications Claiming Priority (1)
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US14/097,940 US20150159257A1 (en) | 2013-12-05 | 2013-12-05 | Coating method, coating system, and coated article |
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US20150159257A1 true US20150159257A1 (en) | 2015-06-11 |
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US14/097,940 Abandoned US20150159257A1 (en) | 2013-12-05 | 2013-12-05 | Coating method, coating system, and coated article |
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US (1) | US20150159257A1 (en) |
EP (1) | EP2881495A1 (en) |
CN (1) | CN104694867A (en) |
Cited By (5)
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US20150165547A1 (en) * | 2013-12-12 | 2015-06-18 | General Electric Company | Fabrication process and fabricated article |
US10029299B2 (en) | 2015-07-09 | 2018-07-24 | General Electric Company | Three-dimensional manufacturing methods and systems for turbine components |
WO2021080943A1 (en) * | 2019-10-21 | 2021-04-29 | Westinghouse Electric Company Llc | Multiple nozzle design in a cold spray system and associated method |
US11247392B2 (en) * | 2019-08-29 | 2022-02-15 | Huazhong University Of Science And Technology | Forming system and method of hybrid additive manufacturing and surface coating |
US20230202115A1 (en) * | 2020-04-01 | 2023-06-29 | Effusiontech IP Pty Ltd | A method for automated treating of 3d surfaces |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN109295450A (en) * | 2018-09-30 | 2019-02-01 | 武汉大学 | An ultrafast pulsed laser-cold spray surface processing device for thin-walled structures |
DE102019218273A1 (en) * | 2019-11-26 | 2021-05-27 | Siemens Aktiengesellschaft | Cold gas spray system with a heating gas nozzle and method for coating a substrate |
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US5847357A (en) * | 1997-08-25 | 1998-12-08 | General Electric Company | Laser-assisted material spray processing |
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DE19740205B4 (en) * | 1997-09-12 | 2004-11-25 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Process for applying a coating by means of plasma spraying |
DE102005005359B4 (en) * | 2005-02-02 | 2009-05-07 | Siemens Ag | Method for cold gas spraying |
US8020509B2 (en) * | 2009-01-08 | 2011-09-20 | General Electric Company | Apparatus, systems, and methods involving cold spray coating |
GB201118698D0 (en) * | 2011-10-28 | 2011-12-14 | Laser Fusion Technologies Ltd | Deposition of coatings on subtrates |
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2013
- 2013-12-05 US US14/097,940 patent/US20150159257A1/en not_active Abandoned
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2014
- 2014-12-02 EP EP14195806.6A patent/EP2881495A1/en not_active Withdrawn
- 2014-12-05 CN CN201410738287.8A patent/CN104694867A/en active Pending
Patent Citations (1)
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US5847357A (en) * | 1997-08-25 | 1998-12-08 | General Electric Company | Laser-assisted material spray processing |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20150165547A1 (en) * | 2013-12-12 | 2015-06-18 | General Electric Company | Fabrication process and fabricated article |
US9511447B2 (en) * | 2013-12-12 | 2016-12-06 | General Electric Company | Process for making a turbulator by additive manufacturing |
US10029299B2 (en) | 2015-07-09 | 2018-07-24 | General Electric Company | Three-dimensional manufacturing methods and systems for turbine components |
US11247392B2 (en) * | 2019-08-29 | 2022-02-15 | Huazhong University Of Science And Technology | Forming system and method of hybrid additive manufacturing and surface coating |
WO2021080943A1 (en) * | 2019-10-21 | 2021-04-29 | Westinghouse Electric Company Llc | Multiple nozzle design in a cold spray system and associated method |
TWI769561B (en) * | 2019-10-21 | 2022-07-01 | 美商西屋電器公司 | Multiple nozzle design in a cold spray system and associated method |
US20230202115A1 (en) * | 2020-04-01 | 2023-06-29 | Effusiontech IP Pty Ltd | A method for automated treating of 3d surfaces |
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CN104694867A (en) | 2015-06-10 |
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