[go: up one dir, main page]

US20120160265A1 - Use of a catalyst in a base coating to improve the strippability of subsequent coatings - Google Patents

Use of a catalyst in a base coating to improve the strippability of subsequent coatings Download PDF

Info

Publication number
US20120160265A1
US20120160265A1 US13/392,127 US201013392127A US2012160265A1 US 20120160265 A1 US20120160265 A1 US 20120160265A1 US 201013392127 A US201013392127 A US 201013392127A US 2012160265 A1 US2012160265 A1 US 2012160265A1
Authority
US
United States
Prior art keywords
catalyst
coating
barrier
barrier primer
hydrogen peroxide
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.)
Abandoned
Application number
US13/392,127
Other languages
English (en)
Inventor
Mark Robert Zentner
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Akzo Nobel Coatings International BV
Original Assignee
Akzo Nobel Coatings International BV
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Akzo Nobel Coatings International BV filed Critical Akzo Nobel Coatings International BV
Priority to US13/392,127 priority Critical patent/US20120160265A1/en
Assigned to AKZO NOBEL COATINGS INTERNATIONAL B.V. reassignment AKZO NOBEL COATINGS INTERNATIONAL B.V. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ZENTNER, MARK ROBERT
Publication of US20120160265A1 publication Critical patent/US20120160265A1/en
Abandoned legal-status Critical Current

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
    • C23G—CLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
    • C23G5/00—Cleaning or de-greasing metallic material by other methods; Apparatus for cleaning or de-greasing metallic material with organic solvents
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B08—CLEANING
    • B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
    • B08B3/00—Cleaning by methods involving the use or presence of liquid or steam
    • B08B3/04—Cleaning involving contact with liquid
    • B08B3/08—Cleaning involving contact with liquid the liquid having chemical or dissolving effect
    • C—CHEMISTRY; METALLURGY
    • C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
    • C09D9/00—Chemical paint or ink removers

Definitions

  • the field to which this invention relates is the stripping of coatings from a surface.
  • references such as U.S. Pat. Nos. 3,654,940; 5,830,836; and 5,954,890 disclose use of hydrogen peroxide for stripping polymeric coatings from surfaces, particularly non-porous substrates, such as an aircraft body.
  • JP 56.070.062 discloses a thermosetting primer containing manganese dioxide. No reference, however, hints to the use of hydrogen peroxide stripping agent for removal of an intermediate coat and/or a topcoat from a barrier primer coat that contains a catalyst for decomposing hydrogen peroxide.
  • the present invention is a method of stripping one or more additional coats from a barrier primer coat containing a catalyst for the decomposition of hydrogen peroxide, comprising contacting the top coat of a surface covered with the primer and one or more additional coats with a stripping agent comprising hydrogen peroxide at decomposition reaction conditions.
  • FIG. 1 is a depiction of the sample coatings made in connection with the testing done on the coating system of Example 1.
  • FIG. 2 is a depiction of the sample coatings made in connection with the testing done on the coating system of Example 2.
  • FIG. 3 is a depiction of the sample coatings made in connection with the testing done on the coating system of Example 3.
  • FIG. 4 is a depiction of the sample coatings made in connection with the testing done on the coating system of Example 4.
  • FIG. 5 is a depiction of the sample coatings made in connection with the testing done on the coating system of Example 5.
  • FIG. 6 is a depiction of the sample coatings made in connection with the testing done on the coating system of Example 6.
  • FIG. 7 is a depiction of the sample coatings made in connection with the testing done on the coating system of Example 7.
  • FIG. 8 is a depiction of the sample coatings made in connection with the testing done on the coating system of Example 8.
  • Hydrogen peroxide decomposition can be achieved by different catalytic materials. There are generally two families of compounds where catalytic conditions will cause decomposition. Certain transition metals and their salts are one family of compounds available for use along with organic, and more specifically metallo-organic compounds that possibly could be bound or cross linked into a composite matrix.
  • the catalytic material is in a solid phase, possibly as a crystalline solid or adsorbed onto or absorbed into a solid and inert carrier that forms the barrier primer coat, and the oxidizer is carried in the liquid (usually water) phase that comes in contact with the solid.
  • Molybdate and tungstate are also effective decomposition catalysts for hydrogen peroxide.
  • Titanium Dioxide has catalytic properties if the proper crystal structure version is used.
  • the metals in elemental form it is contemplated that they can be in the form of a substituent of a larger molecule or compound.
  • oxides of the above elements can be used as active catalysts for formulation of the barrier primer coat.
  • combinations of some of these oxides/hydroxides can be used as the catalyst.
  • samarium can be used as the catalyst. It is believed that samarium can accelerate the decomposition of hydrogen peroxide without generating hydroxyl radicals. Depending on the coating system, this may be an important consideration where barrier primer integrity is concerned. Other solid state forms of metallic compounds may also be considered.
  • Organics provide a very broad classification but may offer a very effective approach to the chemistry of the present invention.
  • oxides and other insoluble forms of metallic compounds are embedded into the primer layer so as to be available to the hydrogen peroxide as it penetrates the coating system.
  • this can potentially cause issues with coating properties that may degrade product performance and be unacceptable.
  • polymer functionality is built into the layer which has chelating capability and the polymer is loaded with the metal catalyst.
  • the catalyst loading is moved from the macroscopic scale (embedded solids) past the nanoscale to the molecular level. It is believed that in certain coating systems, such loading can improve strippability while minimizing impact on coating product performance.
  • the present invention involves use of a catalyst additive to a base coating to improve the strippability of subsequent coatings applied over the base coating with peroxide based strippers while maintaining or improving other performance characteristics of the base coating and coating system. It is believed that oxygen gas produced by the decomposition of hydrogen peroxide helps to lift and remove coatings from the barrier primer containing the catalyst.
  • a catalyst additive to a base coating to improve the strippability of subsequent coatings applied over the base coating with peroxide based strippers while maintaining or improving other performance characteristics of the base coating and coating system. It is believed that oxygen gas produced by the decomposition of hydrogen peroxide helps to lift and remove coatings from the barrier primer containing the catalyst.
  • One specific example is addition of manganese dioxide to a high solids 2K epoxy amine barrier primer to improve the strippability of a 2K urethane intermediate coating and 2K urethane topcoat over this primer.
  • the coating system of the present invention has particular utility for a composite substrate comprising the exterior of aircraft.
  • the system includes a permanent barrier primer applied to the composite and a decorative topcoat, with or without an intermediate coating, applied to this primer.
  • the barrier primer preferably has excellent adhesion to the composite substrate and the subsequent coating or coatings applied over the primer preferably has excellent intercoat adhesion (i.e. rain erosion resistance) and chemical resistance to solvents, jet fuels, hydraulic and other fluids that the coating will be exposed to.
  • the coating system can be removed with chemical based paint removers down to the barrier primer without damage or removal of the barrier primer itself.
  • Hydrogen peroxide based strippers are commercially used to remove paint from airplanes because they are non-corrosive and safe to use when proper precautions are followed.
  • peroxide based strippers have drawbacks in that they may not be effective in stripping multiple layers of conventional coatings that have strong adherence between layers. It has been found that such layers can be effectively stripped according to the present invention which includes an appropriate catalyst in the primer coat.
  • Peroxide stripping agents comprise solutions of the hydrogen peroxide. Most of the commercial peroxide based strippers contain 1 to 7 wt % peroxide. This is a practical range for storage stability and minimizing corrosion to metals and other substrates. Special labeling is also needed for blends containing over 7% peroxide. However, formulations up to 20% peroxide have been tried.
  • the hydrogen peroxide concentration can be as low as about 1%. In other embodiments, the concentration is in the range of about 1 to about 10%, or about 2 to about 9%, or about 4 to about 7%. For example, in an embodiment where the catalyst is manganese, a level at 1% is effective, but levels of 4 to 7% are preferred. In other embodiments, levels higher than 7% also work quite well.
  • solvents can be used including high boiling aromatics, glycol ethers, N-methyl pyrollidone and others. Solvents, when present, are usually used in the range of 1 to 10% to enhance swelling and diffusion through the film being stripped.
  • a commercially available stripping agent useful in connection with the invention is Sea to Sky® SPC-909, which is a peroxide based paint stripper that is a stable emulsion of benzyl alcohol in water. It contains roughly 40% benzyl alcohol, 50% water and 4 to 7% hydrogen peroxide. Corrosion inhibiting and other additives are also used. Other hydrogen peroxide based paint removers are commercially available and can also be used.
  • catalyst levels can range from about 0.01 to about 35%, or about 0.1 to about 30%, or about 0.2 to about 25%, or about 0.5 to about 20%, by volume of dry film in the primer coat, although lower or higher levels may work.
  • the catalyst is chosen from manganese dioxide and manganese carbonate alone or in combination. It is believed the catalysts according to the invention accelerate the decomposition of hydrogen peroxide to water and oxygen gas.
  • manganese dioxide is used alone, its concentration range can be from about 0.1 to about 20%, or about 0.3 to about 15%, or about 0.5 to 10% by volume of dry film.
  • manganese carbonate in an embodiment where manganese carbonate is used alone, its concentration range can be from about 1 to about 30%, or about 2 to about 25%, or about 3 to about 20% by volume of dry film.
  • an intermediate coating and topcoat were applied to barrier primers containing various levels of manganese dioxide, including a control having 0% manganese dioxide.
  • strippability with the primers containing the manganese dioxide was greatly enhanced with peroxide based strippers.
  • the control system with 0% MnO 2 did not strip after 24 hours exposure to a commercially available strippers having 7% hydrogen peroxide (SPC-909).
  • SPC-909 commercially available strippers having 7% hydrogen peroxide
  • the systems with 3 and 10% manganese dioxide in the barrier primer were completely stripped to the barrier primer in 4 to 5 hours with the SPC-909 stripper. The barrier primer was maintained intact.
  • the hydrogen peroxide containing stripper permeates thru the coating system to the barrier primer. It then comes into contact with the catalyst, e.g., manganese dioxide, on the surface of the barrier primer. This contact results in rapid decomposition of the hydrogen peroxide which releases oxygen gas which helps to lift and remove the coatings attached to the barrier primer, but does not remove the barrier primer itself. It is believed that a very high vapor pressure is built up between the barrier primer containing the catalyst, e.g., manganese dioxide, and the coatings above it which overcomes the adhesive forces between the barrier primer and coating above it.
  • the catalyst e.g., manganese dioxide
  • the term “barrier primer” as used herein usually is the coating directly applied to the substrate, the barrier primer containing the catalyst may in fact be an intermediate coating that covers one or more coatings that are applied directly to the substrate. In such an embodiment, it is believed the hydrogen peroxide stripper will affect only the coatings that cover the barrier primer and leave the coatings beneath the coating containing the catalyst undisturbed.
  • the barrier primer with the peroxide decomposition catalyst can also be used without an intermediate coating, as shown in Example 8. In Example 8, the final topcoat was applied directly to the barrier primer. Intercoat adhesion was excellent and the topcoat was easily removed from the barrier primer with a hydrogen peroxide containing paint remover.
  • stripping may be carried out at ambient temperatures which range from about 20 to 24° C. (68 to 75° F.). It is believed higher temperatures can speed up the decomposition of the peroxide by the catalyst which can in turn speed up stripping time. Higher temperatures can be used, but are not required. Generally, stripping time may range from about 4 to 24 hours, depending on catalyst content and resistance to rain erosion.
  • the barrier primer was a high solids 2K epoxy amine coating, but with varying amounts and types of catalyst.
  • Barrier primer (BP 1 ) was a control with 0% peroxide catalyst.
  • Barrier primers (BP 2 , 3 and 4 ) had 10%, 3% and 1% by dry film volume, respectively, of manganese dioxide.
  • Barrier primer (BP 5 ) had 9% by dry volume manganese carbonate.
  • Barrier primer (BP 6 ) had 8.5% manganese carbonate/0.5% manganese dioxide by dry film volume.
  • Intermediate coating (IC 1 ) was a 2K urethane coating based on a polyester crosslinked with an aliphatic isocyanate and intermediate coating (IC 2 ) was a 2K urethane coating based on an epoxidized soybean oil crosslinked with a carboxyl functional polyester (commercially available from Reichhold as Aroflint 607 and Epotuf 91-314).
  • the examples all used Eclipse® decorative 2K urethane topcoat as the topcoat layer. Other commercially available aircraft topcoats can be used.
  • One test applied was Rain erosion resistance.
  • Rain erosion resistance is a very severe test for intercoat adhesion for paint systems applied to the exterior fuselage of an aircraft.
  • the rain erosion test was performed as follows: airfoils as shown in the subsequent examples were masked off to expose the leading edge and then coated with the appropriate coating system. The coated airfoils were cured for two weeks at 25° C. (77° F.)/50% RH and then soaked in room temperature water for 24 hours. The airfoils were then immediately placed on a whirling arm apparatus and rotated for 30 minutes at around 500 miles per hour while exposed to simulated rainfall. The airfoils were then inspected for intercoat adhesion failure back from the leading edge. No adhesion loss or slight chipping less than 0.10 inches from the leading edge are desired. Examples 1, 3 and 4 showed excellent rain erosion resistance.
  • Example 2 showed poor rain erosion resistance.
  • Swelling should be less than 1 mm beyond the scribe, pencil hardness should be B minimum and there should be no loss of adhesion.
  • Example 1 showed excellent Skydrol® resistance with no swelling beyond the scribe, H pencil hardness and no loss of adhesion, while Example 2 showed 2 mm swelling beyond the scribe.
  • Sample panels prepared in accordance with the invention were also tested for strippability.
  • the strippability test was performed as follows: a coated panel, including the top coat, was cured for 1 week at 25° C. (77° F.)/50% RH followed by 1 week cure at 71° C. (160° F.).
  • the perimeter of panel was taped with aluminum tape to prevent penetration of the stripper at the panel edge.
  • the panel was placed horizontally on a lab bench and paint stripper (e.g., SPC 909) was applied onto the panel using a bristle paint brush to provide a coating of stripper evenly and uniformly over the entire coated surface. After 3 to 4 hours, the stripper was removed with a plastic squeegee using light pressure only.
  • the stripper did not remove all of the paint down to the barrier primer, it was applied a second time in the same manner as the first application. After 3 to 4 hours, the stripper applied the second time was removed with a plastic squeegee using light pressure only. If the stripper (applied the second time) did not removed all of the paint down to the barrier primer, it was applied a third time in the same manner as the first application. The stripper applied the third time remained on the panel overnight and then was removed with a plastic squeegee the next day. Any remaining stripper and residue was removed with a cloth soaked with isopropanol. The panel was examined and the amount of topcoat and intermediate coating removed was noted. It was also determined if the barrier primer was still intact.
  • the stripping agents used in the examples to conduct the strippability tests were the SPC 909, stripping agent 022409, Turco® EA 6930 and Turco® EA 6950.
  • Stripping agent 022409 was a modified version of the SPC 909 stripping agent, with a modified solvent component, but having similar levels of hydrogen peroxide.
  • Turco® EA 6930 and EA 6950 are commercially available stripping agents from Henkel Corp.
  • the EA 6930 contains 30-60% Benzyl alcohol, 5-10% hydrogen peroxide and 1-5% D-Limonene, as well as corrosion inhibiting and other additives.
  • the EA 6950 contains 30-60% Benzyl alcohol and 5-10% hydrogen peroxide, as well as corrosion inhibiting and other additives.
  • Sample panels prepared in accordance with the invention were also tested for dry and wet adhesion according to ASTM D3359 Test Method B guidelines.
  • the dry adhesion test was performed as follows: a coated panel, including the top coat, was cured for one week at 25° C. (77° F.)/50% RH. Five parallel cuts were made 3 mm apart from each other through the coating to the substrate using a sharp razor knife with a 3 mm shim as guide. The cuts were approximately 2 inches long. Then five cuts were made 3 mm apart from each other at an angle approximately 45 degrees to the first set of cuts.
  • Adhesive tape (3M 250) was applied over the cuts and the tape was rubbed firmly with an eraser from the end of a pencil. The tape was then removed rapidly from the panel. The coating was examined for any adhesion loss to the substrate or between the coating layers and the % adhesion loss was determined.
  • the wet adhesion test was performed in the same manner as the dry adhesion test, except that the following steps were added after the panels were cured for one week at 25° C. (77° F.)/50% RH: the cured panels were immersed in deionized or distilled water for one week at 25° C. (77° F.). After one week, the panels were removed from the water, wiped dry and checked for adhesion within 30 seconds after removal from water following the remaining steps described above (with respect to the dry adhesion test.
  • BP 1 Barrier Primer
  • ICI Intermediate Coating
  • Decorative topcoat was applied at 2 to 3 mils dry film thickness over the intermediate coating.
  • This system has very good intercoat adhesion as shown by the rain erosion airfoils, and also has excellent resistance to phosphate ester hydraulic fluids. However, it was not stripped with mild paint remover (emulsions of benzyl alcohol in water). It also was not strippable with peroxide based paint strippers.
  • BP 1 Barrier Primer
  • IC 2 Intermediate Coating
  • Decorative topcoat-2 component urethane topcoat designated as Eclipse® applied at 2 to 3 mils dry film thickness over the intermediate coating.
  • BP 2 Barrier primer
  • IC 1 Intermediate Coating
  • Decorative topcoat-2 component urethane topcoat designated as Eclipse® applied at 2 to 3 mils dry film thickness over the intermediate coating.
  • BP 3 Barrier primer
  • IC 1 Intermediate Coating
  • Decorative topcoat-2 component urethane topcoat designated as Eclipse® applied at 2 to 3 mils dry film thickness over the intermediate coating.
  • BP 4 Barrier primer
  • IC 1 Intermediate Coating
  • Decorative topcoat-2 component urethane topcoat designated as Eclipse® applied at 2 to 3 mils dry film thickness over the intermediate coating.
  • Dry and wet adhesion excellent, no adhesion loss Strippability—decorative and intermediate coats were completely removed down to the barrier primer after 8 hours exposure to SPC-909 stripper.
  • the decorative and intermediate coats were only partially removed with the EA 6930 stripper.
  • BP 5 Barrier primer
  • IC 1 Intermediate Coating
  • Decorative topcoat-2 component urethane topcoat designated as Eclipse® applied at 2 to 3 mils dry film thickness over the intermediate coating.
  • Dry and wet adhesion excellent, no adhesion loss Strippability—decorative and intermediate coats were completely removed down to the barrier primer after 8 to 24 hours exposure to SPC-909 stripper.
  • the decorative and intermediate coats were only partially removed with the EA 6930 stripper.
  • the decorative and intermediate coats remained mostly intact with the EA 6930 stripper.
  • BP 6 Barrier primer
  • IC 1 Intermediate Coating
  • BP 3 Barrier primer
  • Eclipse® Decorative topcoat—2 component urethane topcoat designated as Eclipse® applied at 2 to 3 mils dry film thickness over the intermediate coating.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Wood Science & Technology (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Paints Or Removers (AREA)
  • Catalysts (AREA)
US13/392,127 2009-08-27 2010-08-25 Use of a catalyst in a base coating to improve the strippability of subsequent coatings Abandoned US20120160265A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US13/392,127 US20120160265A1 (en) 2009-08-27 2010-08-25 Use of a catalyst in a base coating to improve the strippability of subsequent coatings

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US23749009P 2009-08-27 2009-08-27
EP09173113.3 2009-10-15
EP09173113 2009-10-15
PCT/EP2010/062408 WO2011023727A1 (en) 2009-08-27 2010-08-25 Use of a catalyst in a base coating to improve the strippability of subsequent coatings
US13/392,127 US20120160265A1 (en) 2009-08-27 2010-08-25 Use of a catalyst in a base coating to improve the strippability of subsequent coatings

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2010/062408 A-371-Of-International WO2011023727A1 (en) 2009-08-27 2010-08-25 Use of a catalyst in a base coating to improve the strippability of subsequent coatings

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US14/988,961 Continuation US10407779B2 (en) 2009-08-27 2016-01-06 Use of a catalyst in a base coating to improve the strippability of subsequent coatings

Publications (1)

Publication Number Publication Date
US20120160265A1 true US20120160265A1 (en) 2012-06-28

Family

ID=42115821

Family Applications (2)

Application Number Title Priority Date Filing Date
US13/392,127 Abandoned US20120160265A1 (en) 2009-08-27 2010-08-25 Use of a catalyst in a base coating to improve the strippability of subsequent coatings
US14/988,961 Active US10407779B2 (en) 2009-08-27 2016-01-06 Use of a catalyst in a base coating to improve the strippability of subsequent coatings

Family Applications After (1)

Application Number Title Priority Date Filing Date
US14/988,961 Active US10407779B2 (en) 2009-08-27 2016-01-06 Use of a catalyst in a base coating to improve the strippability of subsequent coatings

Country Status (7)

Country Link
US (2) US20120160265A1 (ru)
EP (1) EP2470609B1 (ru)
CN (1) CN102471617B (ru)
CA (1) CA2770094C (ru)
ES (1) ES2431271T3 (ru)
RU (1) RU2553469C2 (ru)
WO (1) WO2011023727A1 (ru)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104114651B (zh) * 2011-12-16 2017-12-12 联邦科学与工业研究组织 涂料系统

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020022682A1 (en) * 1999-10-21 2002-02-21 Wallace Penny Jo Inorganic/organic compositions
US20050288456A1 (en) * 2004-06-28 2005-12-29 Morkunas Bernard T Flexible, impact resistant primer

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3654940A (en) 1970-11-25 1972-04-11 Chemed Corp Method for removing resinous or rubber deposits with organic peroxides
JPS5833902B2 (ja) 1979-11-14 1983-07-22 大日本塗料株式会社 金属前処理塗料組成物
US4728455A (en) * 1986-03-07 1988-03-01 Lever Brothers Company Detergent bleach compositions, bleaching agents and bleach activators
US5215675A (en) * 1992-03-16 1993-06-01 Isp Investments Inc. Aqueous stripping composition containing peroxide and water soluble ester
US5830836A (en) 1995-10-27 1998-11-03 Eldorado Chemical Co., Inc. Compositions and methods for coating removal
RU2002123933A (ru) * 2002-09-10 2004-03-20 Саито ТАКЕШИ (JP) Состав для удаления полимерных пленок
EP1745327A4 (en) * 2004-05-14 2010-12-15 Ricoh Co Ltd MULTICOLOR DISPLAY ELEMENT
MXPA06014491A (es) * 2004-06-16 2007-03-12 Ppg Ind Ohio Inc Metodos para la remocion de capas de recubrimiento polimericas de sustratos recubiertos.
CN1988956B (zh) * 2004-07-21 2012-10-03 西巴特殊化学品控股有限公司 通过倒置的两阶段工序光活化催化剂的方法及其应用
US20070017266A1 (en) * 2005-07-20 2007-01-25 Ho E Screw & Hardware Co., Ltd. Key-ring clasp
US8178160B2 (en) * 2006-01-20 2012-05-15 Ppg Industries Ohio, Inc. Decorative and durable coating having a homogeneous hue, methods for their preparation, and articles coated therewith
US20100129524A1 (en) 2006-01-20 2010-05-27 Steven Sternberger Methods of dispensing powder coating compositions and articles coated therewith

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020022682A1 (en) * 1999-10-21 2002-02-21 Wallace Penny Jo Inorganic/organic compositions
US20050288456A1 (en) * 2004-06-28 2005-12-29 Morkunas Bernard T Flexible, impact resistant primer

Also Published As

Publication number Publication date
CN102471617A (zh) 2012-05-23
WO2011023727A1 (en) 2011-03-03
RU2553469C2 (ru) 2015-06-20
CN102471617B (zh) 2014-08-13
EP2470609B1 (en) 2013-07-24
US20160115599A1 (en) 2016-04-28
CA2770094C (en) 2017-06-27
ES2431271T3 (es) 2013-11-25
EP2470609A1 (en) 2012-07-04
US10407779B2 (en) 2019-09-10
RU2012110374A (ru) 2013-10-10
CA2770094A1 (en) 2011-03-03

Similar Documents

Publication Publication Date Title
US5721204A (en) Paint stripping composition
KR101986487B1 (ko) 도료 및 피복 강재
US9868867B1 (en) Solvents and uses thereof
US12157833B2 (en) Composition and method for removing a coating from a surface
EP1732707B1 (en) Activation method
JP2008528247A (ja) 改質物質を用いる活性化方法
US10407779B2 (en) Use of a catalyst in a base coating to improve the strippability of subsequent coatings
JP4767317B2 (ja) コーティング液およびコーティング方法
JP2008519902A (ja) 選択的に剥ぎ取り可能な中間被覆および使用方法
CN101412863A (zh) 低挥发低毒脱漆剂
JP6333324B2 (ja) 錆転換剤組成物及びその製造方法
EP2791258B1 (en) Coating systems
BR112012003199A2 (pt) método de extração de um ou mais revestimentos adicionais que cobrem um revestimento de primer de barreira
EP1021490B1 (en) Paint stripping composition
KR20220057256A (ko) 자기계층형 도료 조성물 및 자기계층형 도막을 포함하는 선박용 기재
JP2022523924A (ja) 固体表面、特に金属表面にシランベースのコーティングを適用するための改善された方法
EP2521755B1 (en) Corrosion protection coatings and methods of making the same
AU2005223685B2 (en) Activation method

Legal Events

Date Code Title Description
AS Assignment

Owner name: AKZO NOBEL COATINGS INTERNATIONAL B.V., NETHERLAND

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:ZENTNER, MARK ROBERT;REEL/FRAME:027795/0359

Effective date: 20120214

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION