EP0676488A1 - Process for removing organic materials from machinery components - Google Patents
Process for removing organic materials from machinery components Download PDFInfo
- Publication number
- EP0676488A1 EP0676488A1 EP95104352A EP95104352A EP0676488A1 EP 0676488 A1 EP0676488 A1 EP 0676488A1 EP 95104352 A EP95104352 A EP 95104352A EP 95104352 A EP95104352 A EP 95104352A EP 0676488 A1 EP0676488 A1 EP 0676488A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- cleaner
- vol
- oil
- organic
- dissolving
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims description 28
- 239000011368 organic material Substances 0.000 title claims description 14
- 238000004140 cleaning Methods 0.000 claims abstract description 26
- 239000000463 material Substances 0.000 claims abstract description 26
- 238000001035 drying Methods 0.000 claims abstract description 8
- 238000007865 diluting Methods 0.000 claims abstract description 5
- 239000000155 melt Substances 0.000 claims abstract description 5
- 238000002844 melting Methods 0.000 claims abstract description 3
- 230000008018 melting Effects 0.000 claims abstract description 3
- 239000003921 oil Substances 0.000 claims description 21
- 239000000243 solution Substances 0.000 claims description 19
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 14
- 150000002334 glycols Chemical class 0.000 claims description 10
- 238000010790 dilution Methods 0.000 claims description 7
- 239000012895 dilution Substances 0.000 claims description 7
- 238000011049 filling Methods 0.000 claims description 6
- 238000013016 damping Methods 0.000 claims description 5
- 239000004094 surface-active agent Substances 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 4
- 238000001291 vacuum drying Methods 0.000 claims description 4
- 125000004066 1-hydroxyethyl group Chemical group [H]OC([H])([*])C([H])([H])[H] 0.000 claims description 3
- 125000000956 methoxy group Chemical group [H]C([H])([H])O* 0.000 claims description 3
- OKKJLVBELUTLKV-UHFFFAOYSA-N Methanol Chemical compound OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 claims description 2
- 239000002480 mineral oil Substances 0.000 claims description 2
- 235000010446 mineral oil Nutrition 0.000 claims description 2
- 125000000963 oxybis(methylene) group Chemical group [H]C([H])(*)OC([H])([H])* 0.000 claims description 2
- 238000000576 coating method Methods 0.000 abstract description 5
- 239000011248 coating agent Substances 0.000 abstract description 3
- 230000001464 adherent effect Effects 0.000 abstract 1
- 238000005406 washing Methods 0.000 abstract 1
- 239000010408 film Substances 0.000 description 21
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 13
- 239000010410 layer Substances 0.000 description 7
- 238000005530 etching Methods 0.000 description 6
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical group [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 229910052759 nickel Inorganic materials 0.000 description 5
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 3
- 238000011109 contamination Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 238000005553 drilling Methods 0.000 description 3
- 229910052697 platinum Inorganic materials 0.000 description 3
- 239000011241 protective layer Substances 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- LYCAIKOWRPUZTN-UHFFFAOYSA-N Ethylene glycol Chemical compound OCCO LYCAIKOWRPUZTN-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 150000005827 chlorofluoro hydrocarbons Chemical class 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000004821 distillation Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000007935 neutral effect Effects 0.000 description 2
- 238000004321 preservation Methods 0.000 description 2
- 239000010409 thin film Substances 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- BOSAWIQFTJIYIS-UHFFFAOYSA-N 1,1,1-trichloro-2,2,2-trifluoroethane Chemical compound FC(F)(F)C(Cl)(Cl)Cl BOSAWIQFTJIYIS-UHFFFAOYSA-N 0.000 description 1
- DDMOUSALMHHKOS-UHFFFAOYSA-N 1,2-dichloro-1,1,2,2-tetrafluoroethane Chemical compound FC(F)(Cl)C(F)(F)Cl DDMOUSALMHHKOS-UHFFFAOYSA-N 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- CYTYCFOTNPOANT-UHFFFAOYSA-N Perchloroethylene Chemical group ClC(Cl)=C(Cl)Cl CYTYCFOTNPOANT-UHFFFAOYSA-N 0.000 description 1
- XSTXAVWGXDQKEL-UHFFFAOYSA-N Trichloroethylene Chemical group ClC=C(Cl)Cl XSTXAVWGXDQKEL-UHFFFAOYSA-N 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 229940087091 dichlorotetrafluoroethane Drugs 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- WGCNASOHLSPBMP-UHFFFAOYSA-N hydroxyacetaldehyde Natural products OCC=O WGCNASOHLSPBMP-UHFFFAOYSA-N 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000001223 reverse osmosis Methods 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000001577 simple distillation Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229950011008 tetrachloroethylene Drugs 0.000 description 1
- 238000000108 ultra-filtration Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C11—ANIMAL OR VEGETABLE OILS, FATS, FATTY SUBSTANCES OR WAXES; FATTY ACIDS THEREFROM; DETERGENTS; CANDLES
- C11D—DETERGENT COMPOSITIONS; USE OF SINGLE SUBSTANCES AS DETERGENTS; SOAP OR SOAP-MAKING; RESIN SOAPS; RECOVERY OF GLYCEROL
- C11D3/00—Other compounding ingredients of detergent compositions covered in group C11D1/00
- C11D3/43—Solvents
-
- 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
-
- 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
- C23G5/02—Cleaning or de-greasing metallic material by other methods; Apparatus for cleaning or de-greasing metallic material with organic solvents using organic solvents
- C23G5/024—Cleaning or de-greasing metallic material by other methods; Apparatus for cleaning or de-greasing metallic material with organic solvents using organic solvents containing hydrocarbons
-
- 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
- C23G5/02—Cleaning or de-greasing metallic material by other methods; Apparatus for cleaning or de-greasing metallic material with organic solvents using organic solvents
- C23G5/032—Cleaning or de-greasing metallic material by other methods; Apparatus for cleaning or de-greasing metallic material with organic solvents using organic solvents containing oxygen-containing compounds
-
- C—CHEMISTRY; METALLURGY
- C11—ANIMAL OR VEGETABLE OILS, FATS, FATTY SUBSTANCES OR WAXES; FATTY ACIDS THEREFROM; DETERGENTS; CANDLES
- C11D—DETERGENT COMPOSITIONS; USE OF SINGLE SUBSTANCES AS DETERGENTS; SOAP OR SOAP-MAKING; RESIN SOAPS; RECOVERY OF GLYCEROL
- C11D2111/00—Cleaning compositions characterised by the objects to be cleaned; Cleaning compositions characterised by non-standard cleaning or washing processes
- C11D2111/10—Objects to be cleaned
- C11D2111/14—Hard surfaces
- C11D2111/20—Industrial or commercial equipment, e.g. reactors, tubes or engines
Definitions
- the invention relates to a method for removing organic materials from engine components, in particular for removing fusible organic covering, filling or damping materials from cavities and from surfaces of engine components.
- Meltable organic covering, filling or damping materials such as wax or wax mixtures are used in the coating processes, laser drilling, etching of coatings or in turning and grinding operations of engine components for the new part production and repair of engine components.
- Such fusible organic covering, filling or damping materials have hitherto been used in plants which work with CHCs (for example trichlorethylene or tetrachlorethylene) or CFCs (for example trichlorotrifluoroethane or dichlorotetrafluoroethane) to dissolve the wax-like covering, filling or damping materials from the adhering organic materials exempted.
- CHCs or CFCs Plants that are operated with CHCs or CFCs are complex and expensive to care for, service and maintenance. This is partly due to stricter environmental and occupational safety requirements. Furthermore, a high level of analytical effort must be exerted in order to ensure that these systems function reliably. In addition, CKWs are only of limited use for cleaning surfaces of titanium components, which are often used as engine components, because of the risk of increased stress corrosion cracking of the titanium after contact with CKWS.
- the object of the invention is to provide a method for removing meltable organic materials from engine components, which overcomes the above disadvantages and cleans the surfaces of engine components in a cost-effective, reproducible and reliable manner and completely frees them from residual organic films without polluting the environment and the workplace.
- the advantage of this solution is that, apart from a residual film adhering to the engine component, the meltable organic material is recovered completely and without great technical effort in process step a).
- the thickness of the residual film can be minimized by increasing the temperature of the melt and the temperature of the engine component immersed in the melt.
- the tempered oil used in process step b) can also be used several times until it is removed from that taken up in process step b) by means of distillation or other separation processes organic material must be separated and thus regenerated.
- the adhering residual film is dissolved in a mineral oil or fully synthetic oil with a density of 0.6-0.8 g / cm3.
- This specifically light oil has the advantage that the specifically heavier organic material settles as an oil bath sump and the oil bath above it remains ready for use.
- the adhering residual film is dissolved in an oil bath at bath temperatures of 80 ° C. to 150 ° C. These relatively high bath temperatures contribute to the rapid dissolving and thinning of the residual film on the one hand, and that on the other Material film adhering to the surface of the engine component from essentially oil molecules is minimized in its thickness.
- the treatment of the material film can be done by alcohol-based cleaners.
- the aftertreatment of the material film is preferably carried out using a cleaner from 0.1% by volume to 1 Vol% surfactant and 99 vol% to 99.9 vol% glycol derivative or mixtures of glycol derivatives.
- This cleaner is able to completely dissolve the material film remaining on the surface, which essentially consists of oil molecules, without the use of CHCs or CFCs.
- the glycol derivatives are water-soluble and can be rinsed off the surfaces of the engine components with simple rinsing steps. Distilled and / or demineralized water is preferably used for this.
- the cleaner is preferably diluted with water in a ratio of 1: 1 to 1:10 as a cleaning solution for the aftertreatment used.
- the cleaning solutions are gradually being diluted. A particularly effective cleaning of the surfaces is shown within the preferred limits of the dilution, which can be carried out without additional control processes.
- the cleaner and / or the cleaning solutions are preferably heated to 60 ° C to 80 ° C. This improves the effect of the surfactants in the cleaner in particular and increases the cleaning effect of the cleaning solutions.
- the water is preferably heated to 80 ° C to 95 ° C.
- the alcohol can be heated to just below its boiling point in order to ensure that adhering residual materials are cleaned or remaining substances are rinsed off the surface.
- drying steps with hot air at a temperature between 110 and 150 ° C. can preferably be carried out.
- aqueous liquids are advantageously evaporated.
- vacuum drying can preferably be carried out as the last drying step.
- the cooling channels of a turbine blade are poured for laser drilling with wax that softens at 75 ° C and has a dropping point between 80 ° and 85 ° C.
- This wax is preferably a mineral-saturated hydrocarbon wax that solidifies between 73 ° C, 73 ° C and 78 ° C.
- the turbine blade is heated to 80 ° C and immersed in a wax melt of the same type, which was heated to 110 ° C.
- the wax flows out of the cooling channels of the turbine blade.
- the remaining wax film, which adheres to the inner walls of the cooling channels, is then diluted and dissolved in a 120 ° C oil bath for 15 to 30 minutes.
- the turbine blade is then immersed in a neutral cleaner that can be used for all metals at a temperature of 60 to 80 ° C for 15 to 30 minutes and finally in hot demineralized water at a temperature of 95 ° C for 5 minutes.
- a neutral cleaner that can be used for all metals at a temperature of 60 to 80 ° C for 15 to 30 minutes and finally in hot demineralized water at a temperature of 95 ° C for 5 minutes.
- the turbine blade is dried at 130 ° C for 15 to 45 minutes.
- protective layers and preservation layers can also be removed in the same way, provided that they consist of a meltable, organic material.
- the BLISK rotor After reaching the final dimension of the blade tips, the BLISK rotor is heated and immersed in a wax melt, so that only a residual film of organic material adheres to the rotor surface after the main portion of the wax has melted.
- This residual film is dissolved in a temperature-controlled oil bath at 130 ° C. and further diluted, so that only a thin film of material remains, which essentially consists of oil molecules.
- This material film is then dissolved and further diluted in a cleaner consisting of 0.1% by volume of surfactants and 99.9% by volume of a mixture of glycol derivatives, so that it is subjected to several subsequent rinsing and cleaning steps in which the dilution a cleaning solution is gradually enlarged, disappears completely from the surface.
- the BLISK rotor is subjected to vacuum drying so that it is completely freed of contamination.
- the areas that are not to be coated are first protected with a protective layer made of a meltable organic material. After the platinum has been deposited, the meltable organic material is removed. After a thorough rinsing and drying step, the engine component is converted into an identical type Melt made of organic material dipped until only a residual film of minimal thickness adheres to the turbine component. This residual film is treated in a temperature-controlled oil bath as in Example 2, so that only a material film of essentially oil molecules remains on the surface.
- this material film is dissolved and further thinned, so that rinsing with a cleaning solution and rinsing with distilled and demineralized water are the surface that are not coated with platinum should be fully exposed.
- a metal spray layer made of Ni / Al is to be selectively etched away from a turbine component.
- a nickel layer which is located on the component in places, must be partially protected.
- the component itself consists of a nickel-based material.
- a main component of the etching solution is a nitroaromatic. In this solution, the base material, the metal spray coating and the nickel coating are not chemically stable.
- the component is cleaned in a neutral cleaner and covered with wax from the example.
- the places where the metal spray layer made of Ni / Al is to be etched off are mechanically exposed.
- the component After the selective etching of the metal spray layer made of Ni / Al, the component is first sprayed with cold water and then blown dry.
- the wax cover over the nickel layer and the nickel-based material of the component after the etching has ended is melted in a wax melt, treated in an oil bath and immersed in a cleaner according to Example 2 for 15 to 30 minutes at 78 ° C.
- the component is immersed in a cleaning solution with a first dilution stage and rinsed again with hot water.
- the component is then immersed in a cleaning solution with greater dilution and rinsed repeatedly with hot water.
- the dilution of the cleaning solution is gradually increased until only water adheres to the surfaces of the component, so that contamination can be completely removed from the component with a subsequent vacuum drying.
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Organic Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Metallurgy (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- General Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Wood Science & Technology (AREA)
- Cleaning By Liquid Or Steam (AREA)
- Cleaning And De-Greasing Of Metallic Materials By Chemical Methods (AREA)
- Detergent Compositions (AREA)
Abstract
Description
Die Erfindung betrifft ein Verfahren zum Entfernen organischer Materialien von Triebwerkskomponenten, insbesondere zum Entfernen von schmelzbaren organischen Abdeck-, Füll- oder Dämpfungsmaterialien aus Hohlräumen und von Oberflächen von Triebwerkskomponenten.The invention relates to a method for removing organic materials from engine components, in particular for removing fusible organic covering, filling or damping materials from cavities and from surfaces of engine components.
Für die Neuteilfertigung und Instandsetzung von Triebwerkskomponenten werden schmelzbare organische Abdeck-, Füll- oder Dämpfungsmaterialien wie beispielsweise Wachs oder Wachsgemische bei Beschichtungsprozessen, beim Laserbohren, beim Abätzen von Beschichtungen oder bei Dreh- und Schleifoperationen von Triebwerkskomponenten eingesetzt. Darüber hinaus werden die Oberflächen von nicht korrosionsbeständigen Werkstoffen während der Lagerung mit öl- oder wachshaltigen Schutzschichten zur Konservierung versehen. Derartige schmelzbare organische Abdeck-, Füll- oder Dämpfungsmaterialien werden bisher in Anlagen, die mit CKWs (beispielwweise Trichlorethen oder Tetrachlorethen) oder FCKWs (beispielsweise Trichlortrifluorethan oder Dichlortetrafluorethan) zur Auflösung der wachsartigen Abdeck-, Füll- oder Dämpfungsmaterialien arbeiten, von den anhaftenden organischen Materialien befreit.Meltable organic covering, filling or damping materials such as wax or wax mixtures are used in the coating processes, laser drilling, etching of coatings or in turning and grinding operations of engine components for the new part production and repair of engine components. In addition, the surfaces of non-corrosion-resistant materials during the Provide storage with protective layers containing oil or wax for preservation. Such fusible organic covering, filling or damping materials have hitherto been used in plants which work with CHCs (for example trichlorethylene or tetrachlorethylene) or CFCs (for example trichlorotrifluoroethane or dichlorotetrafluoroethane) to dissolve the wax-like covering, filling or damping materials from the adhering organic materials exempted.
Anlagen die mit CKWs oder FCKWs betrieben werden sind aufwendig und teuer in ihrer Pflege, Wartung und Instandhaltung. Dies beruht teilweise auf verschärften Auflagen in Bezug auf Umwelt- und Arbeitsschutz. Weiterhin muß ein hoher analytischer Aufwand betrieben werden, um eine sichere Funktionsweise dieser Anlagen zu gewährleisten. Darüberhinaus sind CKWs nur begrenzt für die Reinigung von Oberflächen von Titanbauteilen, die häufig als Triebwerkskomponenten eingesetzt werden, wegen der Gefahr einer erhöhten Spannungsrißkorrosion des Titans nach Kontakt mit CKWS verwendbar.Plants that are operated with CHCs or CFCs are complex and expensive to care for, service and maintenance. This is partly due to stricter environmental and occupational safety requirements. Furthermore, a high level of analytical effort must be exerted in order to ensure that these systems function reliably. In addition, CKWs are only of limited use for cleaning surfaces of titanium components, which are often used as engine components, because of the risk of increased stress corrosion cracking of the titanium after contact with CKWS.
Aufgabe der Erfindung ist es, ein Verfahren zum Entfernen von abschmelzbaren organischen Materialien von Triebwerkskomponenten anzugeben, das die obigen Nachteile überwindet und kostengünstig, reproduzierbar und zuverlässig die Oberflächen von Triebwerkskomponenten reinigt und von organischen Restfilmen vollständig befreit, ohne Umwelt und Arbeitsplatz zu belasten.The object of the invention is to provide a method for removing meltable organic materials from engine components, which overcomes the above disadvantages and cleans the surfaces of engine components in a cost-effective, reproducible and reliable manner and completely frees them from residual organic films without polluting the environment and the workplace.
Gelöst wird diese Aufgabe durch folgende Verfahrensschritte
- a) Abschmelzen des organischen Materials in einer artgleichen Schmelze,
- b) Verdünnen und Anlösen eines anhaftenden Restfilms mittels temperiertem Öl an der vorgewärmten Triebwerkskomponente,
- c) Verdünnen und Anlösen eines noch an den Oberflächen anhaftenden Materialfilms mittels organischen Reinigern, die FCKW und CKW frei sind,
- d) ein- oder mehrfaches Nachbehandeln der Oberflächen der Triebwerkskomponenten mittels verdünnten Reinigungslösungen mit zwischengeschalteten Spül- und/oder Trocknungsschritten, wobei die Reinigungslösungen schrittweise zunehmend verdünnt werden.
- a) melting the organic material in a melt of the same type,
- b) diluting and dissolving an adhering residual film by means of tempered oil on the preheated engine component,
- c) diluting and dissolving a material film still adhering to the surfaces by means of organic cleaners which are CFC and CHC free,
- d) single or multiple aftertreatment of the surfaces of the engine components by means of diluted cleaning solutions with intermediate rinsing and / or drying steps, the cleaning solutions being gradually diluted step by step.
Der Vorteil dieser Lösung liegt darin, daß das aufschmelzbare organische Material bis auf einen an der Triebwerkskomponente anhaftenden Restfilm vollständig und ohne großen technischen Aufwand im Verfahrensschritt a) zurückgewonnen wird. Die Dicke des Restfilms kann durch Erhöhung der Temperatur der Schmelze und der Temperatur der in die Schmelze eintauchenden Triebwerkskomponente minimiert werden.The advantage of this solution is that, apart from a residual film adhering to the engine component, the meltable organic material is recovered completely and without great technical effort in process step a). The thickness of the residual film can be minimized by increasing the temperature of the melt and the temperature of the engine component immersed in the melt.
Auch das im Verfahrensschritt b) verwendete temperierte Öl kann mehrfach eingesetzt werden bis es mittels Destillation oder anderen Trennverfahren von dem im Verfahrensschritt b) aufgenommenem organischen Material getrennt und damit regeneriert werden muß.The tempered oil used in process step b) can also be used several times until it is removed from that taken up in process step b) by means of distillation or other separation processes organic material must be separated and thus regenerated.
Schließlich können alle Reinigungs- und Spülprozesse dieses Verfahrens vorteilhaft in Kreisprozessen geführt werden, wobei die Reiniger und Reinigungslösungen über Umkehrosmose, Ultrafiltration und/oder Destillation zurückgewonnen werden können, ohne die Umwelt zu belasten.Finally, all cleaning and rinsing processes of this method can advantageously be carried out in circular processes, the cleaners and cleaning solutions being able to be recovered via reverse osmosis, ultrafiltration and / or distillation without polluting the environment.
In einer bevorzugten Durchführung des Verfahrens erfolgt die Auflösung des anhaftenden Restfilms in einem Mineralöl oder voll synthetischen Öl mit einer Dichte von 0,6-0,8 g/cm³ . Dieses spezifisch leichte Öl hat den Vorteil, daß sich das spezifisch schwerere organische Material als Ölbadsumpf absetz und das Ölbad darüber im oberen Bereich einsatzbereit bleibt.In a preferred embodiment of the method, the adhering residual film is dissolved in a mineral oil or fully synthetic oil with a density of 0.6-0.8 g / cm³. This specifically light oil has the advantage that the specifically heavier organic material settles as an oil bath sump and the oil bath above it remains ready for use.
Bei einer anderen bevorzugten Durchführung des Verfahrens erfolgt die Auflösung des anhaftenden Restfilms in einem Ölbad bei Badtemperaturen von 80 °C bis 150° C. Diese relativ hohen Badtemperaturen tragen dazu bei, daß einerseits ein schnelles Anlösen und Verdünnen des Restfilms erfolgt und andererseits der auf der Oberfläche der Triebwerkskomponente anhaftende Materialfilm aus im wesentlichen Ölmolekülen in seiner Dicke minimiert wird.In another preferred implementation of the method, the adhering residual film is dissolved in an oil bath at bath temperatures of 80 ° C. to 150 ° C. These relatively high bath temperatures contribute to the rapid dissolving and thinning of the residual film on the one hand, and that on the other Material film adhering to the surface of the engine component from essentially oil molecules is minimized in its thickness.
Das Nachbehandeln des Materialfilms kann durch Reiniger auf Alkoholbasis erfolgen. Vorzugsweise erfolgt die Nachbehandlung des Materialfilms mittels eines Reinigers aus 0,1 Vol% bis 1 Vol% Tensid und 99 Vol% bis 99,9 Vol% Glycolderivat oder Mischungen von Glycolderivaten. Dieser Reiniger ist in der Lage den auf der Oberfläche verbliebenen Materialfilm, der im wesentlichen aus Ölmolekühlen besteht, vollständig aufzulösen, ohne daß der Einsatz von CKWs oder FCKWs erforderlich wird. Die Glycolderivate ihrerseits sind wasserlöslich und können mit einfachen Spülschritten von den Oberflächen der Triebwerkskomponenten abgespült werden. Dazu wird vorzugsweise destilliertes und/oder demineralisiertes Wasser verwendet.The treatment of the material film can be done by alcohol-based cleaners. The aftertreatment of the material film is preferably carried out using a cleaner from 0.1% by volume to 1 Vol% surfactant and 99 vol% to 99.9 vol% glycol derivative or mixtures of glycol derivatives. This cleaner is able to completely dissolve the material film remaining on the surface, which essentially consists of oil molecules, without the use of CHCs or CFCs. The glycol derivatives are water-soluble and can be rinsed off the surfaces of the engine components with simple rinsing steps. Distilled and / or demineralized water is preferably used for this.
Der Reiniger auf Glycolbasis enthält vorzugsweise mindesten eines der folgenden Glycolderivate :
- a) R1-(CH₄O)OH, mit R1 = CH₃, R1 = C₂H₅ oder R1 = C₄H₉,
- b) R1-(C₄H₇O₃), mit R1 = CH₃, R1 = C₂H oder R1 = C₄H₉
und - c) R2-(C₂H₄O)nH, mit R2 = CH₃O, R2 = C₂H₅O oder R2 = C₄H₉
und mit n = 2 bis 5.
- a) R1- (CH₄O) OH, with R1 = CH₃, R1 = C₂H₅ or R1 = C₄H₉,
- b) R1- (C₄H₇O₃), with R1 = CH₃, R1 = C₂H or R1 = C₄H₉
and - c) R2- (C₂H₄O) nH, with R2 = CH₃O, R2 = C₂H₅O or R2 = C₄H₉
and with n = 2 to 5.
Diese Reiniger haben den Vorteil,, daß durch einen einfachen Destillationsvorgang die Glycolderivate zurückgewonnen werden können und damit wiederverwendbar sind, so daß ein Kreisprozess ermöglicht wird..These cleaners have the advantage that the glycol derivatives can be recovered by a simple distillation process and are therefore reusable, so that a cycle process is made possible.
Vorzugsweise wird der Reiniger in Verdünnungsgraden mit Wasser im Verhältnis 1:1 bis 1:10 als Reinigungslösung für die Nachbehandlung eingesetzt. Dabei werden die Reinigungslösungen schrittweise zunehmend verdünnt. Innerhalb der bevorzugten Grenzen der Verdünnung zeigt sich eine besonders effektive Reinigung der Oberflächen, die ohne zusätzliche Kontrollverfahren durchgeführt werden kann.The cleaner is preferably diluted with water in a ratio of 1: 1 to 1:10 as a cleaning solution for the aftertreatment used. The cleaning solutions are gradually being diluted. A particularly effective cleaning of the surfaces is shown within the preferred limits of the dilution, which can be carried out without additional control processes.
Zum Reinigen werden vorzugsweise der Reiniger und/oder die Reinigungslösungen auf 60 °C bis 80 °C aufgeheizt. Das verbessert die Wirkung insbesondere der Tenside im Reiniger und erhöht die Reinigungswirkung der Reinigungslösungen. Beim Spülen wird vorzugsweise das Wasser auf 80 °C bis 95 °C aufgeheizt. Wenn mit Alkohol gespült oder gereingt wird, kann der Alkohol bis kurz unter seinen Siedepunkt erhizt werden, um eine Rei-nigung von anhaftenden Restmaterialien oder ein Abspülen verbliebener Restsubstanzen von der Oberfläche zu gewährleisten..For cleaning, the cleaner and / or the cleaning solutions are preferably heated to 60 ° C to 80 ° C. This improves the effect of the surfactants in the cleaner in particular and increases the cleaning effect of the cleaning solutions. When rinsing, the water is preferably heated to 80 ° C to 95 ° C. When rinsing or cleaning with alcohol, the alcohol can be heated to just below its boiling point in order to ensure that adhering residual materials are cleaned or remaining substances are rinsed off the surface.
Zwischen den Spül- und Reinigungsschritten können vorzugsweise Trocknungsschritte mit Heißluft einer Temperatur zwischen 110 und 150 °C erfolgen. Mit diesem bevorzugten Temperaturbereich werden vorteilhaft wässerige Flüssigkeiten abgedampft. Um vorteilhaft die Oberflächen von jeglicher Kontamination zu befreien, kann vorzugsweise als letzter Trocknungsschritt ein Vakuumtrocknen durchgeführt werden.Between the rinsing and cleaning steps, drying steps with hot air at a temperature between 110 and 150 ° C. can preferably be carried out. With this preferred temperature range, aqueous liquids are advantageously evaporated. In order to advantageously free the surfaces of any contamination, vacuum drying can preferably be carried out as the last drying step.
Im folgenden wird das erfindungsgemäße Verfahren an Durchführungsbeispielen erläutert.The method according to the invention is explained below using exemplary embodiments.
Die Kühlkanäle einer Turbinenschaufel werden für das Laserbohren mit Wachs, das bei 75 °C erweicht und einen Tropfpunkt zwichen 80° und 85°C aufweist ausgegossen. Dieses Wachs ist vorzugsweise ein mineralisch gesättigtes Kohlenwasserstoffwachs, das zwischen 73°C 73°C und 78°C fest wird. Nach dem Laserbohren wird die Turbinenschaufel auf 80 °C erwärmt und in eine artgleiche Wachsschmelze, die auf 110 °Cerhitzt wurde, getaucht. Beim Herausziehen der Turbinenschaufel aus der Wachsschmelze fließt das Wachs aus den Kühlkanälen der Turbinenschaufel. Der Restfilm aus Wachs, der an den Innenwänden der Kühlkanäle anhaftet, wird anschließend in einem 120 °Cheißen Ölbad für 15 bis 30 Minuten verdünnt und angelöst. Beim Herausnehmen der Turbinenschaufel aus dem Ölbad verbleibt ein dünner Materialfilm auf den Oberflächen und Innenflächen der Turbinenschaufel, der im wesentlichen aus Ölmolekülen besteht. Dieser Materialfilm wird mit einem Reiniger auf der Basis von DI-Alkoholderivaten mit einem Flammpunkt von 80 bis 130 °C bei einer Temperatur zwischen 60 und 80 °C für 15 bis 30 Minuten verdünnt und angelöst und anschließend in demineralisiertem Wasser abgespült.The cooling channels of a turbine blade are poured for laser drilling with wax that softens at 75 ° C and has a dropping point between 80 ° and 85 ° C. This wax is preferably a mineral-saturated hydrocarbon wax that solidifies between 73 ° C, 73 ° C and 78 ° C. After laser drilling, the turbine blade is heated to 80 ° C and immersed in a wax melt of the same type, which was heated to 110 ° C. When the turbine blade is pulled out of the wax melt, the wax flows out of the cooling channels of the turbine blade. The remaining wax film, which adheres to the inner walls of the cooling channels, is then diluted and dissolved in a 120 ° C oil bath for 15 to 30 minutes. When the turbine blade is removed from the oil bath, a thin film of material remains on the surfaces and inner surfaces of the turbine blade, which essentially consists of oil molecules. This material film is diluted with a cleaner based on DI alcohol derivatives with a flash point of 80 to 130 ° C at a temperature between 60 and 80 ° C for 15 to 30 minutes and then rinsed in demineralized water.
Danach wird die Turbinenschaufel in einem für alle Metalle verwendbaren Neutralreiniger bei einer Temperatur von 60 bis 80 °Cfür 15 bis 30 Minuten getaucht und schließlich in heißem demineralisiertem Wasser bei einer Temperatur von 95 °Cfür 5 Minuten gespült.The turbine blade is then immersed in a neutral cleaner that can be used for all metals at a temperature of 60 to 80 ° C for 15 to 30 minutes and finally in hot demineralized water at a temperature of 95 ° C for 5 minutes.
Abschließend wird die Turbinenschaufel bei 130 °Cfür eine Zeit von 15 bis 45 Minuten getrocknet.Finally, the turbine blade is dried at 130 ° C for 15 to 45 minutes.
Die zeitliche Länge der einzelnen Verfahrensschritte hängt von der Größe der Triebwerkskomponente und von der Komplexität der Gestalt der Triebwerkskomponente ab. Neben dem hier beschriebenen Entfernen einer Wachsfüllung können auf gleiche Weise auch Schutzschichten und Konservierungsschichten entfernt werden, sofern diese aus einem aufschmelzbaren, organischen Material bestehen .The length of time for the individual process steps depends on the size of the engine component and on the complexity of the shape of the engine component. In addition to the removal of a wax filling described here, protective layers and preservation layers can also be removed in the same way, provided that they consist of a meltable, organic material.
Vor dem Abdrehen der Schaufel spitzen eines BLISK-Rotors, der einstückig aus Rotor-scheibe und Schaufeln besteht, auf einen Endradius werden zunächst die Zwischenräume zwischen den Schaufeln des BLISK-Rotors mit Wachs ausgegossen, um die Schwingungen der Schaufeln beim Abdrehen der Schaufelspitzen zu dämpfen.Before turning off the blade tips of a BLISK rotor, which consists in one piece of rotor disc and blades, the spaces between the blades of the BLISK rotor are first poured out with wax to dampen the vibrations of the blades when the blade tips are turned off .
Nach dem Erreichen des Endmaßes der Schaufelspitzen wird der BLISK-Rotor erwärmt und in eine Wachsschmelze getaucht, so daß nach dem Abschmelzen des Hauptanteils des Wachses nur ein Restfilm an organischem Material auf der Rotoroberfläche anhaftet.After reaching the final dimension of the blade tips, the BLISK rotor is heated and immersed in a wax melt, so that only a residual film of organic material adheres to the rotor surface after the main portion of the wax has melted.
Dieser Restfilm wird in einem temperierten Ölbad bei 130 C angelöst und weiter verdünnt, so daß nur ein dünner Materialfilm zurückbleibt, der im wesentlichen aus Ölmolekülen besteht. Dieser Materialfilm wird anschließend in einem Reiniger der zu 0, 1 Vol% aus Tensiden und zu 99,9 Vol% aus einer Mischung von Glycolderivaten besteht, angelöst und weiter verdünnt, so daß er mit mehreren nachfolgenden Spül- und Reinigungsschritten, bei denen die Verdünnung einer Reinigungslösung schrittweise vergrößert wird , vollständig von der Oberfläche verschwindet.This residual film is dissolved in a temperature-controlled oil bath at 130 ° C. and further diluted, so that only a thin film of material remains, which essentially consists of oil molecules. This material film is then dissolved and further diluted in a cleaner consisting of 0.1% by volume of surfactants and 99.9% by volume of a mixture of glycol derivatives, so that it is subjected to several subsequent rinsing and cleaning steps in which the dilution a cleaning solution is gradually enlarged, disappears completely from the surface.
Zum Abschluß wird der BLISK-Rotor einer Vakuumtrocknung ausgesetzt, so daß er vollständig von Kontaminationen befreit wird.Finally, the BLISK rotor is subjected to vacuum drying so that it is completely freed of contamination.
Zum Schutz vor Beschichtung beim galvanischen Abscheiden von Platinschichten auf einer Triebwerkskomponente werden die nicht zu beschichtenden Bereiche zunächst mit einer Schutzschicht aus einem aufschmelzbaren organischen Material geschütz. Nach der Abscheidung des Platins wird das aufschmelzbare organische Material entfernt. Dazu wird die Triebwerkskomponente nach einem gründlichen Spül- und Trocknungsschritt in eine artgleiche Schmelze aus organischem Material getaucht, bis nur noch ein Restfilm von minimaler Dicke auf der Turbinenkomponente haftet. Dieser Restfilm wird wie in Beispiel 2 in einem temperierten Ölbad behandelt, so daß nur noch ein Materialfilm aus im wesentlichen Ölmolekülen auf der Oberfläche verbleibt. Mit Hilfe eines Reinigungsbades aus 0,8 Vol% Tensiden und 99,2 Vol% Glycolderivaten wird dieser Materialfilm angelöst und weiter verdünnt, so daß ein Abspülen durch eine Reinigungslösung und ein Spülen mit destilliertem und demineralisiertem Wasser die Oberfläche, die nicht mit Platin beschichtet werden sollte, vollständig freilegt.To protect against coating during the galvanic deposition of platinum layers on an engine component, the areas that are not to be coated are first protected with a protective layer made of a meltable organic material. After the platinum has been deposited, the meltable organic material is removed. After a thorough rinsing and drying step, the engine component is converted into an identical type Melt made of organic material dipped until only a residual film of minimal thickness adheres to the turbine component. This residual film is treated in a temperature-controlled oil bath as in Example 2, so that only a material film of essentially oil molecules remains on the surface. With the help of a cleaning bath of 0.8 vol% surfactants and 99.2 vol% glycol derivatives, this material film is dissolved and further thinned, so that rinsing with a cleaning solution and rinsing with distilled and demineralized water are the surface that are not coated with platinum should be fully exposed.
Von einem Turbinenbauteil soll zur Vorbereitung einer Reparatur selektiv eine Metallspritzzschicht aus Ni/Al abgeätzt werden. Während des Abätzens ist eine Nickelschicht, die sich stellenweise auf dem Bauteil befindet, partiell zu schützen. Das Bauteil selber besteht aus einem Nickelbasiswerkstoff. Ein Hauptbestandteil der Ätzlösung ist ein Nitroaromat. In dieser Lösung sind der Grundwerkstoff, die Metallspritzschicht und die Nickelschicht chemisch nicht beständig.To prepare for a repair, a metal spray layer made of Ni / Al is to be selectively etched away from a turbine component. During the etching, a nickel layer, which is located on the component in places, must be partially protected. The component itself consists of a nickel-based material. A main component of the etching solution is a nitroaromatic. In this solution, the base material, the metal spray coating and the nickel coating are not chemically stable.
Zur Vorbereitung der selektiven Ätzung wird das Bauteil in einem Neutralreiniger gereinigt und mit Wachs des Beispiels abgedeckt. Die Stellen, an denen die Metallspritzzschicht aus Ni/Al abgeätzt werden soll, werden mechanisch freigelegt.To prepare for the selective etching, the component is cleaned in a neutral cleaner and covered with wax from the example. The places where the metal spray layer made of Ni / Al is to be etched off are mechanically exposed.
Nach dem selektiven Ätzen der Metalspritzschicht aus Ni/Al wird zunächst das Bauteil mit kaltem Wasser abgesprüht und anschließend trockengeblasen.After the selective etching of the metal spray layer made of Ni / Al, the component is first sprayed with cold water and then blown dry.
Zum Entfernen der Wachsabdeckung über der Nickelschicht und dem Nickelbasiswerkstoff des Bauteils nach Beendigung der Ätzung wird dieses in einer Wachsschmelze abgeschmolzen, in einem Ölbad behandelt und in einen Reiniger entsprechend Beispiel 2 für 15 bis 30 Minuten bei 78 °Cgetaucht. Nach einer Zwischenspülung in demineralisiertem Wasser wird das Bauteil in eine Reinigungslösung mit einer ersten Verdünnungsstufe getaucht und wieder mit heißem Wasser abgespült. Danach wird das Bauteil in eine Reinigungslösung mit größerer Verdünnung getaucht und wiederholt mit heißem Wasser abgespült. Die Verdünnung der Reinigungslösung wird solange schrittweise vergrößert, bis nur noch Wassser an den Oberflächen des Bauteils haftet, so daß mit einer anschließenden Vakuumtrocknung das Bauteil von Kontaminationen vollständig befreit werden kann.To remove the wax cover over the nickel layer and the nickel-based material of the component after the etching has ended, it is melted in a wax melt, treated in an oil bath and immersed in a cleaner according to Example 2 for 15 to 30 minutes at 78 ° C. After an intermediate rinse in demineralized water, the component is immersed in a cleaning solution with a first dilution stage and rinsed again with hot water. The component is then immersed in a cleaning solution with greater dilution and rinsed repeatedly with hot water. The dilution of the cleaning solution is gradually increased until only water adheres to the surfaces of the component, so that contamination can be completely removed from the component with a subsequent vacuum drying.
Claims (11)
und
und mit n = 2 bis 5.
and
and with n = 2 to 5.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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DE4411677 | 1994-04-05 | ||
DE4411677A DE4411677C1 (en) | 1994-04-05 | 1994-04-05 | Process for removing organic materials from engine components |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0676488A1 true EP0676488A1 (en) | 1995-10-11 |
EP0676488B1 EP0676488B1 (en) | 1998-06-10 |
Family
ID=6514646
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Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP95104352A Expired - Lifetime EP0676488B1 (en) | 1994-04-05 | 1995-03-24 | Process for removing organic materials from machinery components |
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---|---|
US (1) | US5653817A (en) |
EP (1) | EP0676488B1 (en) |
DE (1) | DE4411677C1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115283374A (en) * | 2022-07-22 | 2022-11-04 | 东风柳州汽车有限公司 | Cleaning method for solvent type coating paint conveying system |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0856375B1 (en) | 1996-12-03 | 2001-09-12 | MTU Aero Engines GmbH | Partially coated workpieces and process for manufacturing same |
CA2251208A1 (en) | 1998-11-12 | 2000-05-12 | Claude Perreault | Fully automatic plating wax collecting device and method thereof |
DE10210518A1 (en) | 2002-03-09 | 2003-10-02 | Mtu Aero Engines Gmbh | Process for stripping engine components and device for carrying out the process |
EP1599613B1 (en) * | 2003-03-03 | 2006-06-28 | DECHEMA Gesellschaft für Chemische Technologie und Biotechnologie e.V. | Method for coating a substrate |
US20060073348A1 (en) * | 2004-10-06 | 2006-04-06 | General Electric Company | Electroplated fuel nozzle/swirler wear coat |
DE102004049825B4 (en) * | 2004-10-13 | 2006-11-09 | Mtu Aero Engines Gmbh | Method for stripping coated components |
US10830093B2 (en) | 2017-06-13 | 2020-11-10 | General Electric Company | System and methods for selective cleaning of turbine engine components |
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CH513991A (en) * | 1969-09-18 | 1971-11-30 | Motag Bmw Imp | Removal of temporary protective coatings - from machine parts |
EP0426943A2 (en) * | 1989-11-08 | 1991-05-15 | Arakawa Chemical Industries, Ltd. | Agent and method for removing rosinbase solder flux |
EP0464652A1 (en) * | 1990-06-27 | 1992-01-08 | Arakawa Chemical Industries, Ltd. | Agent and method for removing rosin-base solder flux |
WO1993006204A1 (en) * | 1991-09-24 | 1993-04-01 | The Dow Chemical Company | Semi-aqueous cleaning process and solvent compositions |
WO1993009270A1 (en) * | 1991-10-30 | 1993-05-13 | United Technologies Corporation | Non-chlorinated solvent dewax process |
EP0541892A2 (en) * | 1991-11-11 | 1993-05-19 | Leybold Aktiengesellschaft | Process of de-oiling and cleaning material covered with greasy and/or oily substances |
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DE3838188A1 (en) * | 1988-11-10 | 1990-05-17 | Fourne Maschinenbau Gmbh | CLEANING POLYMER-TAPED PARTS |
US5484488A (en) * | 1994-04-06 | 1996-01-16 | Bj Services Company, U.S.A. | Methods for melting and dispersing paraffin wax in oil field production equipment |
-
1994
- 1994-04-05 DE DE4411677A patent/DE4411677C1/en not_active Expired - Fee Related
-
1995
- 1995-03-24 EP EP95104352A patent/EP0676488B1/en not_active Expired - Lifetime
- 1995-04-04 US US08/416,224 patent/US5653817A/en not_active Expired - Lifetime
Patent Citations (6)
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CH513991A (en) * | 1969-09-18 | 1971-11-30 | Motag Bmw Imp | Removal of temporary protective coatings - from machine parts |
EP0426943A2 (en) * | 1989-11-08 | 1991-05-15 | Arakawa Chemical Industries, Ltd. | Agent and method for removing rosinbase solder flux |
EP0464652A1 (en) * | 1990-06-27 | 1992-01-08 | Arakawa Chemical Industries, Ltd. | Agent and method for removing rosin-base solder flux |
WO1993006204A1 (en) * | 1991-09-24 | 1993-04-01 | The Dow Chemical Company | Semi-aqueous cleaning process and solvent compositions |
WO1993009270A1 (en) * | 1991-10-30 | 1993-05-13 | United Technologies Corporation | Non-chlorinated solvent dewax process |
EP0541892A2 (en) * | 1991-11-11 | 1993-05-19 | Leybold Aktiengesellschaft | Process of de-oiling and cleaning material covered with greasy and/or oily substances |
Cited By (1)
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CN115283374A (en) * | 2022-07-22 | 2022-11-04 | 东风柳州汽车有限公司 | Cleaning method for solvent type coating paint conveying system |
Also Published As
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DE4411677C1 (en) | 1995-10-26 |
EP0676488B1 (en) | 1998-06-10 |
US5653817A (en) | 1997-08-05 |
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