GB2115013A - Composition for selective chemical removal of hard surface coatings from superalloy substrates - Google Patents
Composition for selective chemical removal of hard surface coatings from superalloy substrates Download PDFInfo
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- GB2115013A GB2115013A GB08301268A GB8301268A GB2115013A GB 2115013 A GB2115013 A GB 2115013A GB 08301268 A GB08301268 A GB 08301268A GB 8301268 A GB8301268 A GB 8301268A GB 2115013 A GB2115013 A GB 2115013A
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- water soluble
- nickel
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- 239000000203 mixture Substances 0.000 title claims abstract description 35
- 239000000758 substrate Substances 0.000 title claims abstract description 31
- 238000000576 coating method Methods 0.000 title claims description 41
- 229910000601 superalloy Inorganic materials 0.000 title abstract description 7
- 239000000126 substance Substances 0.000 title description 14
- 238000000034 method Methods 0.000 claims abstract description 23
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 claims abstract description 22
- 235000011149 sulphuric acid Nutrition 0.000 claims abstract description 12
- 238000013019 agitation Methods 0.000 claims abstract description 9
- 239000004094 surface-active agent Substances 0.000 claims abstract description 7
- 150000001491 aromatic compounds Chemical class 0.000 claims abstract description 5
- 229910052751 metal Inorganic materials 0.000 claims description 19
- 239000002184 metal Substances 0.000 claims description 19
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 19
- -1 fluoride ions Chemical class 0.000 claims description 16
- 239000011248 coating agent Substances 0.000 claims description 15
- 239000000919 ceramic Substances 0.000 claims description 13
- 239000011195 cermet Substances 0.000 claims description 7
- USIUVYZYUHIAEV-UHFFFAOYSA-N diphenyl ether Chemical compound C=1C=CC=CC=1OC1=CC=CC=C1 USIUVYZYUHIAEV-UHFFFAOYSA-N 0.000 claims description 7
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 claims description 6
- 239000011737 fluorine Substances 0.000 claims description 6
- 229910052731 fluorine Inorganic materials 0.000 claims description 6
- 230000002378 acidificating effect Effects 0.000 claims description 5
- RILZRCJGXSFXNE-UHFFFAOYSA-N 2-[4-(trifluoromethoxy)phenyl]ethanol Chemical compound OCCC1=CC=C(OC(F)(F)F)C=C1 RILZRCJGXSFXNE-UHFFFAOYSA-N 0.000 claims description 4
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 claims description 3
- 229910052708 sodium Inorganic materials 0.000 claims description 3
- 239000011734 sodium Substances 0.000 claims description 3
- BDHFUVZGWQCTTF-UHFFFAOYSA-M sulfonate Chemical compound [O-]S(=O)=O BDHFUVZGWQCTTF-UHFFFAOYSA-M 0.000 claims 2
- 239000000243 solution Substances 0.000 abstract description 29
- 239000007921 spray Substances 0.000 abstract description 4
- 239000007864 aqueous solution Substances 0.000 abstract description 3
- 238000005474 detonation Methods 0.000 abstract description 3
- KRHYYFGTRYWZRS-UHFFFAOYSA-M Fluoride anion Chemical compound [F-] KRHYYFGTRYWZRS-UHFFFAOYSA-M 0.000 abstract description 2
- 239000002344 surface layer Substances 0.000 abstract 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 15
- 239000002585 base Substances 0.000 description 13
- 238000002485 combustion reaction Methods 0.000 description 6
- 239000010410 layer Substances 0.000 description 6
- 229910052759 nickel Inorganic materials 0.000 description 4
- 229910004039 HBF4 Inorganic materials 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 3
- MCMNRKCIXSYSNV-UHFFFAOYSA-N ZrO2 Inorganic materials O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 3
- 239000002253 acid Substances 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 239000000470 constituent Substances 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 2
- 239000004743 Polypropylene Substances 0.000 description 2
- 229910052783 alkali metal Inorganic materials 0.000 description 2
- 229910052784 alkaline earth metal Inorganic materials 0.000 description 2
- SOIFLUNRINLCBN-UHFFFAOYSA-N ammonium thiocyanate Chemical compound [NH4+].[S-]C#N SOIFLUNRINLCBN-UHFFFAOYSA-N 0.000 description 2
- 230000015556 catabolic process Effects 0.000 description 2
- 238000005524 ceramic coating Methods 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 238000006731 degradation reaction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000000227 grinding Methods 0.000 description 2
- 238000010297 mechanical methods and process Methods 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 229920001155 polypropylene Polymers 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 239000011253 protective coating Substances 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- LSNNMFCWUKXFEE-UHFFFAOYSA-M Bisulfite Chemical compound OS([O-])=O LSNNMFCWUKXFEE-UHFFFAOYSA-M 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910017665 NH4HF2 Inorganic materials 0.000 description 1
- PMZURENOXWZQFD-UHFFFAOYSA-L Sodium Sulfate Chemical compound [Na+].[Na+].[O-]S([O-])(=O)=O PMZURENOXWZQFD-UHFFFAOYSA-L 0.000 description 1
- 238000005270 abrasive blasting Methods 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- 150000001340 alkali metals Chemical group 0.000 description 1
- 125000000217 alkyl group Chemical group 0.000 description 1
- 125000003118 aryl group Chemical class 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910000856 hastalloy Inorganic materials 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000001257 hydrogen Chemical group 0.000 description 1
- 229910052739 hydrogen Chemical group 0.000 description 1
- 125000004435 hydrogen atom Chemical group [H]* 0.000 description 1
- 230000003301 hydrolyzing effect Effects 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 230000009972 noncorrosive effect Effects 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 229910052938 sodium sulfate Inorganic materials 0.000 description 1
- 235000011152 sodium sulphate Nutrition 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 229910002076 stabilized zirconia Inorganic materials 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 231100000331 toxic Toxicity 0.000 description 1
- 230000002588 toxic effect Effects 0.000 description 1
- 239000000080 wetting agent Substances 0.000 description 1
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
- C23G—CLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
- C23G1/00—Cleaning or pickling metallic material with solutions or molten salts
- C23G1/02—Cleaning or pickling metallic material with solutions or molten salts with acid solutions
- C23G1/10—Other heavy metals
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K13/00—Etching, surface-brightening or pickling compositions
- C09K13/04—Etching, surface-brightening or pickling compositions containing an inorganic acid
- C09K13/06—Etching, surface-brightening or pickling compositions containing an inorganic acid with organic material
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K13/00—Etching, surface-brightening or pickling compositions
- C09K13/04—Etching, surface-brightening or pickling compositions containing an inorganic acid
- C09K13/08—Etching, surface-brightening or pickling compositions containing an inorganic acid containing a fluorine compound
-
- 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
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F1/00—Etching metallic material by chemical means
- C23F1/44—Compositions for etching metallic material from a metallic material substrate of different composition
Landscapes
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Metallurgy (AREA)
- Mechanical Engineering (AREA)
- General Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Inorganic Chemistry (AREA)
- Cleaning And De-Greasing Of Metallic Materials By Chemical Methods (AREA)
- ing And Chemical Polishing (AREA)
- Cleaning By Liquid Or Steam (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Coating By Spraying Or Casting (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Abstract
The composition comprises an aqueous solution of H2SO4, a nitro- substituted aromatic compound, and optionally a fluoride ion producing species, and a surfactant. The composition can selectively remove hard surface layers deposited through flame, plasma spray, and detonation gun techniques on superalloy substrates by contacting the above stripping solution in a heated bath wherein the bath is continuously agitated by an ultrasonic agitation means.
Description
SPECIFICATION
Selective chemical removal of hard surface coatings from superalloy substrates
This invention is related to the removal of ceramic, cermet and metallic coatings from high strength, high temperature resistant metal substrates and, more particularly, to the removal of these hard surface coatings from superalloys, particularly nickel-base substrates by use of an aqueous acidic stripper bath equipped with a high energy density agitation means.
One of the most difficuit requirements in the chemical stripping art has been to develop a composition which will chemically remove the "hard surface" coatings, that is, molten particle coatings which are applied by detonation gun, plasma, and flame spray methods onto metal surfaces, such as the nickel-base jet engine combustion chambers. Such coatings, which are usually applied in thin layers to provide protection against high temperature oxidative gas streams, include heat resistant ceramics, cermets, and nickel-base mixtures.
The Prior Art has lacked an efficient chemical stripper which can quickly and selectively remove such coatings without damaging the underlying substrate. Currently used techniques feature mechanical methods such as machining, grinding and abrasive blasting the coating, and nonmechanical methods such as chemical immersion in solutions which only soften a ceramic coating, e.g.
hydrochloric acid base solutions, and the use of molten salt baths. However, mechanical methods are very time consuming, and additionally can easily damage a very expensive piece of equipment, due to the ease in creating extensive dimensional damage on the metal substrate, which is frequently used in a "high technology" application. Although current chemical methods will soften certain ceramic coatings, subsequent mechanical removal of the ceramic, along with the underlying inner bond coating is still required. Molten salt baths are hazardous to operate, and are effective on only a limited number of coating substrate combinations. Also these techniques are all deficient in their speed of removal, cost of operation, and effectiveness of result. U.S.Patent 2,698,781 discloses sulfuric acid solutions containing nitroaromatic additives which are effective in removing oxide scale and electroplated nickel from copper substrates. However, there is no teaching inferring that ceramic, cermet or hard surface metallic coatings might be chemically removable from a nickel-base substrate.
It is an object of this invention to create an effective composition and accompanying method for the removal of hard surface coatings from high strength, high temperature resistant alloy substrates.
It is another object of this invention to create an effective composition and accompanying method for the selective, non-corrosive removal of hard, high temperature resistant ceramics, cermets and nickel-base bond coats from nickel-base substrates.
It is still another object of this invention to devise a method of selectively stripping only the hard surface coating from jet engine component metal surfaces without dimensional damage to the stripped metal surfaces.
These and other objects of the invention have been accomplished by the discovery of a novel composition and accompanying method for the selective removal of hard surface coatings particularly heat resistant ceramic, cermets and nickel-base coats, from high strength, high temperature resistant metal substrates, in particular nickel-base substrates.The stripping composition comprises H2SO4, preferably about 90450 grams/liter (g/l) of concentrated H2SO4, e.g., 660 Be' (B 1.84 spec. grav., most preferably about 250-300 g/l; about 20 g/l to saturation of a water soluble, nitro-substituted aromatic compound, and most preferably about 100-1 20 g/l of meta-nitrobenzene sodium sulfonate; about 0--70 g/l of a water soluble, fluorine-containing species, most preferably about 10-20 g/l of fluoroboric acid; about 0-1.0 g/l of a surfactant, most preferably about 0-.5 g/l of one of the group of diphenylether sulfonates; the remainder being water in amount of about 2-90 wt. % of the solution.The stripping method of the invention involves contacting the hard surface coatings, usually a heat resistant ceramic, cermet, or nickel-base coating on the metal substrate with the acidic stripping solution described above, preferably comprising sulfuric acid, a soluble fluorine-containing species, a soluble nitro-substituted aromatic compound, a surfactant and water, and continuing the contacting until the hard surface coating has been selectively removed from the metal surface.The contacting is carried out by immersing the deposited substrate in the solution bath which is kept at about 120 1 800 F., most preferably about 130-1 500 F., as the bath is actively agitated by an ultrasonic agitation means, most preferably an adequately powered ultrasonic generator-transducer, to a power density of at least about 4 watts/in2, and preferably about 7-8 watts/in2. Upon complete coating removal, the substrate is removed from the solution, rinsed, and is in condition for further processing.
A well known technique, particularly in the "high technology" industries involving the construction of jet engines, and gas turbine engines which employ superalloys that are useful, for example, in aeronautical applications, is to coat the metal surfaces which will be exposed to severe high temperature oxidation environments with a thin, i.e., a few mils, coatings of a protective metallic or nonmetallic layer. These coatings, commonly referred to as "hard surface" coatings, can be any one of a number of high strength heat and corrosion resistant substances, and usually include a "nickelbase", hereinafter defined as "a metallic mixture rich in nickel which can function as both a bonding coat for a protective ceramic layer, or, the protective layer itself"; a ceramic substance, or a cermet, as well as certain mixtures of these substances.One particularly hard coating which is frequently used on aircraft combustion chambers as a protective coating is a three layer system, which has the following composition:
Bond Coat: 3-5 mils, Ni 80%, Cr 15% Intermediate Coat: 'i 6 mils, 3565% mixture of Ni 80%--Cr 20% and MgO-ZrO2 Outer Coat: 6-10 mils MgO-ZrO2.
Other hard surface coatings which are finding application in jet engine combustion chambers and are of particular note are:
A: Co 23, Cr 18, Al 12, Yo 5, Ni balance;
B: Y stabilized zirconia;
C: Co Cr Al Y;
D: Ni+Cr 94, Al 6, Yl.
These hard surface coatings which can be stripped from a variety of metal substrates which, in the broadest embodiment of the invention, can be of any metal which is resistant to acid or alkaline corrosion, and more specifically, metal superalloys which have both high temperature resistance and high strength at these elevated temperatures. In particular, alloys located in the VIII A Group on the
Periodic Chart, i.e., iron, nickel and cobalt, and particularly nickel-base alloys, such as the well known "Hastelloy X" are stripped of their coatings by the composition of the invention.The coatings are applied to the substrates through a variety of well known techniques in the art, e.g., detonation gun, plasma spray, and flame spray particle applications, which all essentially consist of grinding the compositions into a fine powder, heating the powder up into its molten form, and spraying the molten material, which has been accelerated in a gas plasma to high speeds, onto the substrate to be coated in the form of a fine, very thin metal mist, which hardens to form an extremely tough, protective coating.
This invention is further directed to an improved composition and accompanying method of removal of these coatings which have been applied in the above-described manner. In order for a strong chemical stripper to function effectively several problems must first be overcome. The stripping composition must be able to strip at a satisfactory rate, e.g., of the order of 1/2--2 mils per/hour, and must be carefully ventilated so as to remove toxic vapors resulting from the process, which is always a major consideration when dealing with chemicals in this art, both in the lab and in their industrial environments and applications.Such a solution has been found by creating an aqueous acidic bath having the following composition: Sulfuric acid, H2SO4, preferably in its concentrated form, e.g., 66 Be', although any commercially available brand is satisfactory, is an essential constituent of the solution.
The concentration of H2SO4 should range between about 90 ii-50 g/l, and preferably between about 250--300 girl. Too little acid will not give the bath the necessary acid strength to remove the coatings at a suitable rate, while amounts in excess of 450 g/l do not provide additional superior stripping results and cannot be economically justified; however, in theory, H2SO4 could consist of as much as 90% of the solution.
A second, essential element in the stripping solution, functioning as an oxidizing agent, is, in the broadest embodiment of the invention, a water soluble nitro-substituted aromatic compound, or, more preferably, a water soluble nitro-substituted benzene compound such as the class of compounds disclosed in U.S. Patent 2,698,781. Most preferably, meta-nitrobenzene sodium sulfonate or sulfonic acid, or the like, e.g., any suitable alkali or alkaline earth metal nitrobenzene sulfonate, including the ammonium radical as a functional equivalent thereof, will function effectively. This class of chemicals is believed to function in solution as a kinetic accelerator, although applicants' do not wish to be bound by theory.
The concentration of the nitro-substituted aromatic constituent can range from about 20 g/l to saturation, and should range between about 20-1 20 g/l, with the higher levels, e.g., 60-1 20 g/l, being the most preferred.
Another constituent of the bath which although not essential is highly preferred, is the addition of a soluble fluorine-containing species, most preferably fluoroboric acid, HBF4, but other fluorinecontaining species, e.g., HF, NH4HF2, Na3AIF6 et al, that can disassociate in aqueous solution to generate low fluoride ion concentrations, are particularly suitable. The concentration of the fluorinecontaining species is determined by how much of it is required to produce a desired concentration of fluoride ions in solution; and generally will range between about 0-70 girl, and preferably, about 1020 g/l for substances which highly disassociated in aqueous solution. As the concentration of fluoride ions increase, the chance of harmful corrosion to the substrate rises, creating an upper limit barrier on the amount which can be added to the stripping solution.
It is preferred, although not essential, to include a small amount, e.g., 0-3.0 g/l and most preferably about 0-1.0 g/l of a surfactant to function as a wetting agent on the surface to be dissolved. Compounds which are particularly preferred for this task are the diphenylether sulfonates, e.g., compounds having the generic formula
where R is an alkyl group or hydrogen, and X is an alkali metal, such as sodium. Such a product is currently sold under the trade name "Dowfax 3B2", marketed by the Dow Chemical Co., Midland,
Michigan. Most alkali metal diphenylether sulfonates are suitable equivalents, and, in the broadest embodiment of the invention, any surfactant which possesses hydrolytic and oxidative stability toward the stripping solution is an acceptable substitute.The stripping composition is completed by adding water, in amounts ranging from 2-90 wt. %, to bring the solution to the desired strength. Water lowers the viscosity of the stripping solution and increases the mobility of ionic species in solution.
The addition of water to sulfuric acid has the desirable effect of lowering the solution cavitation threshold, i.e., the minimum power required to reduce the local pressure on a liquid to a value less than its vapor pressure. This arises through an increase in vapor pressure and decrease in viscosity and density upon dilution. For room temperature water at 20 KHz, the cavitation threshold is 2.45 W/in2.
The method of this invention involves contacting the hard surface coating with the acidic stripping solution, and continuing the contacting until the hard coating has been substantially removed from the metal substrate without any dimensional change occurring to the underlying surface. In order for the stripping to occur at an acceptable rate, it is essential that the solution bath be continually agitated by a suitable agitation means, and preferably by an ultrasonic generator-transducer, either a magnetostrictive (preferred) or a piezoelectric transducer. The transducer should operate in such a manner so as to produce a minimal power density of about 4 watts/in2, and preferably about 7-8 watts/in2. Stirring by conventional techniques simply will not produce the required solution agitation in the stripper bath needed to produce an effective rate.Coupled with the ultrasonic agitator, which inherently will supply energy to the solution, it is necessary to keep the solution at a temperature range of about 1 10--1800F in order to produce an acceptable rate of stripping, and most preferably about 130-1 500F during operation.
The invention is now illustrated by the following examples which are not intended to be limiting.
Example I
An aircraft combustor used in jet engines is made of Hastelloy-X (22 Cur, 1 8.5 Fe, 9.0 Mo, 1.5 Co, 0.6 W, balance Ni) and plasma flame sprayed with a triple layer coating over 520 in2, comprised of a bond coat, 3-5 mils thickness, Ni/Cr 95% intermediate coat, 4-6 mils, 35-36% mixture of Ni 80%-Cr 20% and MgO-ZrO outer coat, 6-10 mils, MgO-ZrO2.Two of these combustion can chambers were stripped of their coatings in 10 and 1 6 hours, using ultrasonic agitation in a bath kept at a temperature range of 120-1 700 F. A 30 gallon stainless steel hot water tank containing two 1 200 watt side mounted immersible ultrasonic transducers was employed during the stripping operation and 6 gallons of the stripping solution (275 g/l H2SO4 660 Be', 14 g/l HBF4 (48%), 120 g/l mnitrobenzene sodium sulfonate1O.1 g/l Dowfax 3B2) contained in a square polypropylene container was used. Metallagraphic examination failed to show any suitable degradation of the combustion can chambers.
Example II
A military jet engine combustion can chamber was immersed in a stripping solution containing 275 grams/liter concentrated sulfuric acid H2SO4 (660 Be'), 145 grams/liter fluoroboric acid, HBF4 (48%), and 116 grams/liter meta-nitrobenzene sodium sulfonate. After 20 hours at 130-1 700 F, the three layer coating had been removed from the burner can. A 5 gallon stainless steel tank, fitted with a
1000 watt bottom-mounted ultrasonic transducer, containing 2 gallons of the stripping solution, in a
square polypropylene container was used. No substrate degradation was observed.
Example Ill
A Hastelloy-X coupon with Metco 443 (Ni/Cr 93, 6 Al), a product of Metco Inc., Westbury, N.Y., was immersed into a stripping solution containing 90 grams/liter concentrated sulfuric acid H2SO4 (660 Be'), 72 grams/liter meta-nitrobenzene sodium sulfonate, 46 gramslliter sodium sulfate Na2504, and 1.2 grams/liter ammonium thiocyanate NH4SCN.
After 45 minutes with ultrasonic agitation at 145--150"F the several mil thick coating had been removed from the coupon.
This invention is capable of removing not only ceramics, cermets and nickel-base substances from metals, particularly nickel base superalloy substrates, without causing unacceptable dimensional changes or structural changes to the base metal, but also of removing a wide variety of hard surface coatings from these substrates without damage to the underlying material.
Obviously, numerous modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood that within the scope of the appended ciaims, the invention may be practiced otherwise than as specifically described herein.
Claims (15)
1. A composition for the selective removal of hard surface metal coatings, particularly ceramic, cermet and nickel-base mixtures, from high strength, high temperature resistant substrates, comprising:
about 90450 g/l of H2SO4;
about 20--240 g/I of a water soluble nitro-substituted aromatic compound;
the remainder being water.
2. A composition as claimed in claim 1 wherein the solution further includes up to about 70 g/l of a water soluble fluorine-containing species which disassociates to provide a source of fluoride ions in solution.
3. A composition as claimed in claim 1 or claim 2 wherein the solution further includes up to about 3.0 g/l of a surfactant selected from the class of diphenylether sulfonates.
4. A composition for the selective removal of hard surface metal coatings, particularly ceramic, cermet and nickel-base mixtures, from high strength, high temperature resistant substrates, wherein the composition comprises:
about 250-300 g/l of H2SO4;
about 60--120 g/l of a water soluble nitro-substituted benzene compound;
about 10--20 g/l of a water soluble fluorine-containing species which disassociates to provide a source of fluoride ions in solution;
up to about 1.0 g/l of a surfactant selected from the class of diphenylether sulfonates;
the remainder being water.
5. A composition as claimed in claim 4 wherein the composition comprises about 270--280 g/l of H2SO4.
6. A composition as claimed in claim 4 wherein the water soluble nitro-substituted benzene compound is about 100--120 g/l of meta-nitrobenzene sodium sulfonate.
7. A composition as claimed in claim 4 wherein the water soluble fluorine-containing species is about 10--20 g/l of fluoroboric acid.
8. A composition as claimed in claim 4 wherein the diphenylether sulfonate is up to about 0.5 g/l of sodium diphenylether sulfonate.
9. A composition as claimed in claim 1 or claim 4 substantially as hereinbefore described with particular reference to the Examples.
10. A composition as claimed in claim 1 or claim 4, substantially as illustrated in any one of the
Examples.
11. A method for the selective removal of hard surface metal coatings, including ceramic, cermet and nickel-base mixtures from high strength, high temperature resistant substrates, the method comprising contacting the hard surface coating with an acidic stripping solution as claimed in any one of claims 1 to 10, in a suitable container means which is kept at a solution temperature of about 120 1 800F and is continually agitated by an ultrasonic agitation means;
continuing the contacting until the hard surface coating has been substantially removed from the metal substrate without damaging the underlying substrate;
removing the substrate from the solution bath.
12. A method as claimed in claim 11 wherein the temperature of the solution is kept at about 130-1 500F during operation.
13. A method as claimed in claim 11 or claim 12 wherein the ultrasonic agitation means is an ultrasonic generator-transducer which continually supplies a power density to the solution of at least 4 watts/in2 during operation.
14. A method as claimed in claim 13 wherein the transducer is kept at a power density of about 7-8 watts/in2.
15. A method as claimed in claim 11 substantially as hereinhefore described with particular reference to the Examples.
1 6. A method as claimed in claim 11 substantially as illustrated in any one of the Examples.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US34196582A | 1982-01-22 | 1982-01-22 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB8301268D0 GB8301268D0 (en) | 1983-02-16 |
| GB2115013A true GB2115013A (en) | 1983-09-01 |
| GB2115013B GB2115013B (en) | 1985-12-18 |
Family
ID=23339766
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08301268A Expired GB2115013B (en) | 1982-01-22 | 1983-01-18 | Composition for selective chemical removal of hard surface coatings from superalloy substrates |
Country Status (11)
| Country | Link |
|---|---|
| JP (1) | JPS58130280A (en) |
| AU (1) | AU546054B2 (en) |
| BE (1) | BE895241A (en) |
| CA (1) | CA1185152A (en) |
| CH (1) | CH651849A5 (en) |
| DE (1) | DE3248006A1 (en) |
| ES (1) | ES8402624A1 (en) |
| FR (1) | FR2520374B1 (en) |
| GB (1) | GB2115013B (en) |
| IT (1) | IT1164864B (en) |
| SE (1) | SE8207490L (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5976265A (en) * | 1998-04-27 | 1999-11-02 | General Electric Company | Method for removing an aluminide-containing material from a metal substrate |
| WO2000000667A1 (en) * | 1998-06-29 | 2000-01-06 | General Electric Company | Method of stripping a coating from a rotary seal of an aircraft engine |
| US6494960B1 (en) | 1998-04-27 | 2002-12-17 | General Electric Company | Method for removing an aluminide coating from a substrate |
| US6833328B1 (en) | 2000-06-09 | 2004-12-21 | General Electric Company | Method for removing a coating from a substrate, and related compositions |
| US6863738B2 (en) | 2001-01-29 | 2005-03-08 | General Electric Company | Method for removing oxides and coatings from a substrate |
| US6953533B2 (en) | 2003-06-16 | 2005-10-11 | General Electric Company | Process for removing chromide coatings from metal substrates, and related compositions |
| EP1788125A3 (en) * | 2005-11-22 | 2007-06-13 | United Technologies Corporation | Strip process for superalloys |
| CN102978631A (en) * | 2011-09-06 | 2013-03-20 | 沈阳黎明航空发动机(集团)有限责任公司 | Precise titanium alloy part re-melted layer removing method |
| IT202100025232A1 (en) * | 2021-10-01 | 2023-04-01 | T A G Srl | METHOD OF REMOVING A CERAMIC THERMAL BARRIER COATING |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4113283C2 (en) * | 1991-04-24 | 1994-05-05 | Kernforschungsz Karlsruhe | Use of an etching solution for the selective etching of a metallic sacrificial layer in the production of microstructures |
| DE4219667C2 (en) * | 1992-06-16 | 1994-12-01 | Kernforschungsz Karlsruhe | Tool and method for producing a microstructured plastic layer |
| DE19833990A1 (en) | 1998-07-29 | 2000-02-10 | Metallgesellschaft Ag | Mordant for stainless steels |
| US6238743B1 (en) * | 2000-01-20 | 2001-05-29 | General Electric Company | Method of removing a thermal barrier coating |
| US6379749B2 (en) * | 2000-01-20 | 2002-04-30 | General Electric Company | Method of removing ceramic coatings |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2698781A (en) * | 1953-04-27 | 1955-01-04 | Enthone | Accelerating action of acids on metals |
| DE1926228C3 (en) * | 1969-05-22 | 1974-02-21 | Bergische Metallwarenfabrik Dillenberg & Co Kg, 5601 Gruiten | Bath for the electrolytic removal of metal coatings made of nickel or chrome from base bodies made of non-ferrous metal |
| FR2345503A1 (en) * | 1976-03-22 | 1977-10-21 | Oxy Metal Industries Corp | Rapid removal of nickel-contg. alloys from metal substrates - using complexing media for nickel, iron and cadmium |
| JPS52133830A (en) * | 1976-05-04 | 1977-11-09 | Nihon Kagaku Kizai Kk | Metal coat exfoliating solution |
| DE2824975A1 (en) * | 1978-06-07 | 1979-12-20 | Basf Ag | Additive for etching, polishing and demetallisation bath - comprises a reaction prod. of ethylene! oxide-propylene! oxide copolymer and poly:amine |
| GB2066386B (en) * | 1979-12-26 | 1983-10-12 | Gen Electric | Filler removal method |
| US4302246A (en) * | 1980-01-03 | 1981-11-24 | Enthone, Incorporated | Solution and method for selectively stripping alloys containing nickel with gold, phosphorous or chromium from stainless steel and related nickel base alloys |
| JPS579874A (en) * | 1980-06-17 | 1982-01-19 | Toshiba Corp | Etching solution for nickel |
-
1982
- 1982-11-10 CA CA000415360A patent/CA1185152A/en not_active Expired
- 1982-11-12 AU AU90416/82A patent/AU546054B2/en not_active Ceased
- 1982-12-03 BE BE0/209645A patent/BE895241A/en not_active IP Right Cessation
- 1982-12-20 CH CH7416/82A patent/CH651849A5/en not_active IP Right Cessation
- 1982-12-24 DE DE19823248006 patent/DE3248006A1/en not_active Withdrawn
- 1982-12-29 SE SE8207490A patent/SE8207490L/en not_active Application Discontinuation
-
1983
- 1983-01-18 GB GB08301268A patent/GB2115013B/en not_active Expired
- 1983-01-19 FR FR8300786A patent/FR2520374B1/en not_active Expired
- 1983-01-20 ES ES519129A patent/ES8402624A1/en not_active Expired
- 1983-01-21 IT IT47598/83A patent/IT1164864B/en active
- 1983-01-21 JP JP58007476A patent/JPS58130280A/en active Granted
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5976265A (en) * | 1998-04-27 | 1999-11-02 | General Electric Company | Method for removing an aluminide-containing material from a metal substrate |
| US6494960B1 (en) | 1998-04-27 | 2002-12-17 | General Electric Company | Method for removing an aluminide coating from a substrate |
| WO2000000667A1 (en) * | 1998-06-29 | 2000-01-06 | General Electric Company | Method of stripping a coating from a rotary seal of an aircraft engine |
| US6833328B1 (en) | 2000-06-09 | 2004-12-21 | General Electric Company | Method for removing a coating from a substrate, and related compositions |
| US6863738B2 (en) | 2001-01-29 | 2005-03-08 | General Electric Company | Method for removing oxides and coatings from a substrate |
| US6953533B2 (en) | 2003-06-16 | 2005-10-11 | General Electric Company | Process for removing chromide coatings from metal substrates, and related compositions |
| EP1788125A3 (en) * | 2005-11-22 | 2007-06-13 | United Technologies Corporation | Strip process for superalloys |
| US8475598B2 (en) | 2005-11-22 | 2013-07-02 | United Technologies Corporation | Strip process for superalloys |
| CN102978631A (en) * | 2011-09-06 | 2013-03-20 | 沈阳黎明航空发动机(集团)有限责任公司 | Precise titanium alloy part re-melted layer removing method |
| IT202100025232A1 (en) * | 2021-10-01 | 2023-04-01 | T A G Srl | METHOD OF REMOVING A CERAMIC THERMAL BARRIER COATING |
Also Published As
| Publication number | Publication date |
|---|---|
| ES519129A0 (en) | 1984-02-01 |
| CH651849A5 (en) | 1985-10-15 |
| FR2520374B1 (en) | 1988-06-24 |
| JPS6261670B2 (en) | 1987-12-22 |
| ES8402624A1 (en) | 1984-02-01 |
| FR2520374A1 (en) | 1983-07-29 |
| GB2115013B (en) | 1985-12-18 |
| GB8301268D0 (en) | 1983-02-16 |
| IT8347598A0 (en) | 1983-01-21 |
| SE8207490D0 (en) | 1982-12-29 |
| AU9041682A (en) | 1983-07-28 |
| JPS58130280A (en) | 1983-08-03 |
| SE8207490L (en) | 1983-07-23 |
| IT1164864B (en) | 1987-04-15 |
| DE3248006A1 (en) | 1983-07-28 |
| CA1185152A (en) | 1985-04-09 |
| AU546054B2 (en) | 1985-08-15 |
| BE895241A (en) | 1983-03-31 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |