[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

CN103388167A - Protective treatment method of aluminum alloy surface - Google Patents

Protective treatment method of aluminum alloy surface Download PDF

Info

Publication number
CN103388167A
CN103388167A CN2013103649531A CN201310364953A CN103388167A CN 103388167 A CN103388167 A CN 103388167A CN 2013103649531 A CN2013103649531 A CN 2013103649531A CN 201310364953 A CN201310364953 A CN 201310364953A CN 103388167 A CN103388167 A CN 103388167A
Authority
CN
China
Prior art keywords
workpiece
acid
anodizing
treatment
aluminum alloy
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.)
Pending
Application number
CN2013103649531A
Other languages
Chinese (zh)
Inventor
颜杰红
屈广浩
贾荣华
刘建民
王立亮
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.)
AVIC Sac Commercial Aircraft Co Ltd
Original Assignee
AVIC Sac Commercial Aircraft Co Ltd
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 AVIC Sac Commercial Aircraft Co Ltd filed Critical AVIC Sac Commercial Aircraft Co Ltd
Priority to CN2013103649531A priority Critical patent/CN103388167A/en
Publication of CN103388167A publication Critical patent/CN103388167A/en
Pending legal-status Critical Current

Links

Landscapes

  • Chemical Treatment Of Metals (AREA)

Abstract

The invention discloses a protective treatment method of an aluminum alloy surface. The protective treatment method comprises the following steps of: carrying out pre-treatment and deoxidation treatment on a to-be-treated workpiece, so that a water film lasts for 30 seconds by a workpiece surface water film process test; and anodizing, wherein a boric acid-sulfuric acid solution is adopted, the anodizing temperature is 21 DEG C-29 DEG C, the direct-current voltage is 14V-16V, the anodizing time is 19 minutes-21 minutes, the voltage is increased to gradually reach 14V-16V at the velocity of 3V/minute from 0V, the boric acid-sulfuric acid is free of chromic acid and comprises 37.5g/L-52.0g/L (according to mass volume concentration) of sulfuric acid and 5.2g/L-10.7g/L of boric acid, the content of sodium benzoate additive is not bigger than 1000ppm, and the treated workpiece is obtained by washing in cold water and naturally drying. Compared with the chromic acid anodizing of the aluminum alloy, the anodizing solution is free of a chromic anhydride component, so that the use of chromic anhydride is reduced in an anodizing process, the environmental pollution is reduced, and the generated sewage treatment cost is lowered.

Description

A kind of aluminum alloy surface protection processing method
Technical field
The invention belongs to material surface protection field, is a kind of aluminum alloy surface protection processing method specifically.
Background technology
Current in aircraft industry the application more aluminum alloy anode metallization processes be chromic acid anodizing and sulfur acid anodizing.Sulfur acid anodizing is larger because of its Influence of Fatigue Properties to material, and the use in the aluminium alloy protection of civilian aircraft is few; Chromic acid anodizing is because its erosion resistance is better, and is less and more be widely used in the protection of domestic and international civilian aircraft aluminium alloy to the Influence of Fatigue Properties of material.
Chromic acid is a kind of poisonous carcinogenic substance.Chromic acid in chromic acid anodizing solution can be dispersed in air in process of production, stimulate people's respiratory mucosa, make it produce inflammation, simultaneously chromic acid anodizing production also can produce a large amount of chromate waste waters, and annual aviation factory all needs a large amount of man power and material of chromate waste water cost who produces in the chromic acid anodizing production process for processing.Along with the development of society and the enhancing of people's environmental protection consciousness, the requirement meeting of industrial sewage discharging is more and more higher, as these, produces in process of production the technique of a large amount of chromate waste waters and obnoxious flavour, can more and more can not adapt to the development of modernization industry.
Summary of the invention
For above shortcomings part in prior art, the technical problem to be solved in the present invention is to provide a kind of eco-friendly aluminum alloy surface protection processing method.
The present invention adopts following technical scheme:
A kind of aluminum alloy surface protection processing method comprises following step:
Step 1: carry out to workpiece to be handled pre-treatment and deoxidation treatment, made the workpiece surface moisture film continuous 30 seconds;
Step 2: the workpiece through step 1 carries out anodizing, and technique is: adopt boric acid-sulphuric acid soln, 21~29 ℃ of temperature; Volts DS 14~16V; Time is 19~21min; Voltage from 0V, increases with 3V/min speed, progressively reaches 14~16V; Do not contain chromic acid in this boric acid-sulfuric acid,, according to the mass body volume concentrations, comprise 37.5~52.0g/L sulfuric acid, 5.2~10.7g/L boric acid, the content of Sodium Benzoate additive is not more than 1000ppm;
3) through workpiece seasoning under room temperature after cold wash of step 2.
Further, the pre-treatment of step 1 is:
1) adopt acetone to carry out solution and clean to workpiece to be handled, during workpiece surface visual inspection after cleaning, workpiece surface is answered free from dust, grease and external residue; The workpiece dress is hung;
2) adopting mass concentration is the basic solution alkali cleaning of 45-60g/L, and the dipping alkaline solution cleans 10min at least, and water temperature 30-50 ℃ is carried out Warm Wash, then the surface after cold wash should reach moisture film continuous 30 seconds;
3) deoxidation treatment, according to the mass body volume concentrations, the solution that deoxidation treatment adopts contains Cr + 6Concentration be 22.5~26g/L, HNO 3Concentration be 75~105g/l, by add hydrofluoric acid adjust erosion rate 20~25 μ m/ single faces/hour, at room temperature, reaction 1~3min, the surface after cold wash reached moisture film continuous 30 seconds.
Further, through the anodized workpiece of step 2, adopt rare chromatedsolution to carry out sealing treatment, described rare chromatedsolution contains according to the mass body volume concentrations Cr that concentration is 45~100mg/L + 6, the pH value is between 3.2~3.8, temperature is controlled at 90 ± 2 ℃, time 23~28min.
Further, the mixing solutions that rare chromatedsolution is comprised of Sodium chromate and chromic anhydride, preparation is according to chromic anhydride CrO 3The mass body volume concentrations is 70mg/L; Sodium chromate Na 2CrO 3The mass body volume concentrations is 49mg/L, and surplus is water.
The present invention has following advantage and beneficial effect:
1, the present invention compares with the sulfur acid anodizing of routine, and is less to the fatigue property shadow of part.
2, technique of the present invention is compared with the chromic acid anodizing of aluminium alloy, owing to there is no the chromic anhydride composition in its anodization solution, make the use that has effectively reduced chromic anhydride in anodizing process, environmental contamination reduction has also reduced consequent sewage disposal expense (expense how much depend on turnout), due to this mill solution temperature and voltage lower, treatment time is also shorter, can reduce heat energy consumption 20%-40%; Power consumption is more than 32%, and the 10%-20% that can enhance productivity.
3, the solidity to corrosion part of having relatively high expectations, can do sealing treatment; When bonding force is had relatively high expectations, can not carry out sealing treatment.
Embodiment
Below in conjunction with embodiment and experimental example, the present invention is described in detail:
Embodiment 1
The Aluminium Alloys in Common Use workpiece of taking on aircraft adopts 7075 naked aluminium alloys and 2024 alclad alloys, according to following steps, processes:
Pre-treatment:
1) adopt acetone to carry out solution and clean to workpiece to be handled, during workpiece surface visual inspection after cleaning, workpiece surface is answered free from dust, grease and external residue; The workpiece dress is hung;
2) adopt the 44# clean-out system to carry out alkali and clean, the surface after cold wash should reach moisture film continuous 30 seconds; Being specially and adopting mass concentration is that the Isoprep44 basic solution alkali of 45g/L cleans, and the dipping alkaline solution cleans 10min at least, and 50 ℃ of water temperatures are carried out Warm Wash, then the surface after cold wash should reach moisture film continuous 30 seconds;
Deoxidation treatment:
Deoxidation treatment, according to the mass body volume concentrations, the solution that deoxidation treatment adopts contains Cr + 6Concentration be 22.5g/L, HNO 3Concentration be 75g/l, by add hydrofluoric acid adjust erosion rate 20 μ m/ single faces/hour, at room temperature, reaction 3min, the surface after cold wash reached moisture film continuous 30 seconds through the test of moisture film method.
The workpiece of processing carries out anodizing, and technique is: adopt boric acid-sulphuric acid soln, 21 ℃ of temperature; Volts DS 14V; Time is 19min; Voltage from 0V, increases with 3V/min speed, progressively reaches 14V; Do not contain chromic acid in this boric acid-sulfuric acid,, according to the mass body volume concentrations, comprise 37.5g/L sulfuric acid, 5.2g/L boric acid, the content 500ppm of Sodium Benzoate additive;
Anodized workpiece is seasoning under room temperature after cold wash, obtains finished product.
Embodiment 2
Be with the difference of embodiment 1:
Adopt 2024 naked aluminium alloys and 2024 alclads.
In pre-treatment, adopting mass concentration is that the Isoprep44 basic solution alkali of 60g/L cleans, and the dipping alkaline solution cleans 10min at least, and 50 ℃ of water temperatures are carried out Warm Wash, then the surface after cold wash should reach moisture film continuous 30 seconds;
Deoxidation treatment:
According to the mass body volume concentrations, the solution that deoxidation treatment adopts contains Cr + 6Concentration be 23g/L, HNO 3Concentration be 80g/l, by add hydrofluoric acid adjust erosion rate 21 μ m/ single faces/hour, at room temperature, reaction 2min, the surface after cold wash reached moisture film continuous 30 seconds through the test of moisture film method.
Workpiece through deoxidation treatment carries out anodizing, and technique is: adopt boric acid-sulphuric acid soln, 23 ℃ of temperature; Volts DS 15V; Time is 20min; Voltage from 0V, increases with 3V/min speed, progressively reaches 15V; Do not contain chromic acid in this boric acid-sulfuric acid,, according to the mass body volume concentrations, comprise 40g/L sulfuric acid, 7g/L boric acid, the content 300ppm of Sodium Benzoate additive;
Embodiment 3
Be with the difference of embodiment 1:
Adopt respectively 2024 naked aluminium alloys and two kinds of samples of 2024 alclad alloys.
In pre-treatment:
Adopting mass concentration is that the Isoprep44 basic solution alkali of 50g/L cleans, and the dipping alkaline solution cleans 10min at least, and 40 ℃ of water temperatures are carried out Warm Wash, then the surface after cold wash should reach moisture film continuous 30 seconds;
Deoxidation treatment:
According to the mass body volume concentrations, the solution that deoxidation treatment adopts contains Cr + 6Concentration be 25g/L, HNO 3Concentration be 90g/l, by add hydrofluoric acid adjust erosion rate 23 μ m/ single faces/hour, at room temperature, reaction 3min, the surface after cold wash reached moisture film continuous 30 seconds.
Workpiece through deoxidation treatment carries out anodizing, and technique is: adopt boric acid-sulphuric acid soln, 25 ℃ of temperature; Volts DS 16V; Time is 21min; Voltage from 0V, increases with 3V/min speed, progressively reaches 16V; Do not contain chromic acid in this boric acid-sulfuric acid,, according to the mass body volume concentrations, comprise 45g/L sulfuric acid, 8g/L boric acid, the content 700ppm of Sodium Benzoate additive;
Workpiece after anodizing adopts rare chromatedsolution to carry out sealing treatment, and rare chromatedsolution contains the Cr of 45mg/L + 6, the pH value is 3.8, temperature is controlled at 90 ± 2 ℃, time 40min.
Embodiment 4
Be with the difference of embodiment 1:
Adopt respectively 2024 naked aluminium alloys and two kinds of samples of 2024 alclad alloys.
In pre-treatment: adopting mass concentration is that the Isoprep44 basic solution alkali of 48g/L cleans, and the dipping alkaline solution cleans 10min at least, and 45 ℃ of water temperatures are carried out Warm Wash, then the surface after cold wash should reach moisture film continuous 30 seconds;
Deoxidation treatment:
According to the mass body volume concentrations, the solution that deoxidation treatment adopts contains Cr + 6Concentration be 26g/L, HNO 3Concentration be 105g/l, by add hydrofluoric acid adjust erosion rate 25 μ m/ single faces/hour, at room temperature, reaction 1min, the surface after cold wash reached moisture film continuous 30 seconds through the test of moisture film method.
Workpiece through deoxidation treatment carries out anodizing, and technique is: adopt boric acid-sulphuric acid soln, 28 ℃ of temperature; Volts DS 15V; Time is 20min; Voltage from 0V, increases with 3V/min speed, progressively reaches 15V; Do not contain chromic acid in this boric acid-sulfuric acid,, according to the mass body volume concentrations, comprise 45g/L sulfuric acid, 9g/L boric acid, the content 1000ppm of Sodium Benzoate additive;
Adopt rare chromatedsolution to carry out sealing treatment through anodized workpiece, rare chromatedsolution contains the Cr of 52mg/L + 6, the pH value is 3.2, temperature is controlled at 90 ± 2 ℃, time 25min.
Embodiment 5
Be with the difference of embodiment 1:
Adopt respectively 2024 naked aluminium alloys and two kinds of samples of 2024 alclad alloys.
In pre-treatment: adopting mass concentration is that the Isoprep44 basic solution alkali of 55g/L cleans, and the dipping alkaline solution cleans 10min at least, and 38 ℃ of water temperatures are carried out Warm Wash, then the surface after cold wash should reach moisture film continuous 30 seconds;
Deoxidation treatment:
According to the mass body volume concentrations, the solution that deoxidation treatment adopts contains Cr + 6Concentration be 24g/L, HNO 3Concentration be 90g/l, by add hydrofluoric acid adjust erosion rate 24 μ m/ single faces/hour, at room temperature, reaction 1min, the surface after cold wash reached moisture film continuous 30 seconds through the test of moisture film method.
Workpiece carries out anodizing, and technique is: adopt boric acid-sulphuric acid soln, 27 ℃ of temperature; Volts DS 16V; Time is 21min; Voltage from 0V, increases with 3V/min speed, progressively reaches 16V; Do not contain chromic acid in this boric acid-sulfuric acid,, according to the mass body volume concentrations, comprise 48g/L sulfuric acid, 8g/L boric acid, the content 800ppm of Sodium Benzoate additive;
Adopt rare chromatedsolution to carry out sealing treatment through anodized workpiece, rare chromatedsolution contains the Cr of 49mg/L + 6, the pH value is 3.5, temperature is controlled at 90 ± 2 ℃, time 25min.
Adopt in the above-described embodiments the power supply model: Sorensen DCS40-30E.
Experimental example 1
The rete test
Rete after boric acid-sulfur acid anodizing in above-described embodiment is carried out the test of weight:
Untight anodizing rete weight 〉=21.5mg/dm on 2024 naked aluminium alloys 2
Untight anodizing rete weight≤75.3mg/dm on 7075 naked aluminium alloys 2This result is to guarantee certain thicknesses of layers, because rete after 2000 series aluminum material anodizing is thinner, for guaranteeing certain solidity to corrosion, so require rete weight 〉=21.5mg/dm 2Because rete after 7000 series material anodizing is thicker, but this material is used as bearing member often, and rete is thicker can affect fatigability, requires rete weight≤75.3mg/dm 2Result shows and all reaches requirement.
Experimental example 2
Boric acid-sulfur acid anodizing membranous layer corrosion resistance test
In embodiment 3,4,53 groups of aluminium test pieces through the boric acid-sulfur acid anodizing of sealing according to ASTM B117 carry out respectively 336,360, hour salt-fog test (testing surface is in vertical direction with 6 degree angles) after, in arbitrary test piece, no more than 5 of the independent spot that presents or spot corrosion, diameter is not more than 0.8mm; Amounting to 90 square inches of (5.8dm 2) test area on, no more than 9 of the independent spot that presents or spot corrosion, diameter is not more than 0.8mm; Except those zones in distance edge, sign seal or point of contact 1.6mm scope.Illustrate that the solidity to corrosion result is good, corrosion resisting property is to represent with the hours that neutral salt spray test can reach.Can be suitable with the chromic acid anodizing membranous layer corrosion resistance by the salt-fog test of 336 hours.The present invention, by 360 hours, has good solidity to corrosion.
Experimental example 3
Boric acid-sulfur acid anodizing membranous layer binding force experiment:
To the boric acid of the workpiece in embodiment 3,4,5 sealing-sulfur acid anodizing rete, pressing BAC5736 coating epoxy primer (the base-material trade mark: 515K011, the solidifying agent trade mark: 910-012, manufacturer: PRC-De-Soto International, Inc.) film thickness is after after (8-20 μ m) at room temperature dry 8 hours, press BSS7225, when 1 type 1 class was carried out dried tape test, coating was not peeled off.2024 alclad alloys after the inventive method is processed,, through combining power test, prove that the bonding force of rete is good, the rete difficult drop-off.
Experimental example 4
The bonding force test
To untight boric acid in embodiment 1 and 2-sulfur acid anodizing rete primer coating: after priming paint solidifies fully, adopt 250 adhesive tapes of 3M company to carry out cross cut test by the cross cut test standard of ISO2409 paint and varnish, film adhesion all reaches 0 grade of level.

Claims (4)

1. an aluminum alloy surface protection processing method, is characterized in that, comprises following step:
Step 1: carry out to workpiece to be handled pre-treatment and deoxidation treatment, make workpiece surface reach moisture film continuous 30 seconds;
Step 2: the workpiece through step 1 carries out anodizing, and technique is: adopt boric acid-sulphuric acid soln, 21~29 ℃ of temperature; Volts DS 14~16V; Time is 19~21 min; Voltage from 0V, increases with 3V/min speed, progressively reaches 14~16V; Do not contain chromic acid in this boric acid-sulfuric acid,, according to the mass body volume concentrations, comprise 37.5~52.0g/L sulfuric acid, 5.2~10.7g/L boric acid, the content of Sodium Benzoate additive is not more than 1000ppm;
3) through workpiece seasoning under room temperature after cold wash of step 2.
2., according to the aluminum alloy surface protection processing method of claim 1, it is characterized in that, the pre-treatment of step 1 is:
1) adopt acetone to carry out solution and clean to workpiece to be handled, during workpiece surface visual inspection after cleaning, workpiece surface is answered free from dust, grease and external residue; The workpiece dress is hung;
2) adopting mass concentration is the basic solution alkali cleaning of 45-60 g/L, and the dipping alkaline solution cleans at least 10 min, and water temperature 30-50 ℃ is carried out Warm Wash, then the surface after cold wash should reach moisture film continuous 30 seconds;
3) deoxidation treatment, according to the mass body volume concentrations, the solution that deoxidation treatment adopts contains Cr + 6Concentration be 22.5~26 g/L, HNO 3Concentration be 75~105g/l, by add hydrofluoric acid adjust erosion rate 20~25 μ m/ single faces/hour, at room temperature, reaction 1~3min, the surface after cold wash reached moisture film continuous 30 seconds.
3. according to the aluminum alloy surface protection processing method of claim 1, it is characterized in that, adopt rare chromatedsolution to carry out sealing treatment through the anodized workpiece of step 2, described rare chromatedsolution contains according to the mass body volume concentrations Cr that concentration is 45 ~ 100mg/L + 6, the pH value is between 3.2~3.8, temperature is controlled at 90 ± 2 ℃, time 23 ~ 28min.
4., according to the aluminum alloy surface protection processing method of claim 4, it is characterized in that, the mixing solutions that rare chromatedsolution is comprised of Sodium chromate and chromic anhydride, preparation is according to chromic anhydride CrO 3The mass body volume concentrations is 70mg/L; Sodium chromate Na 2CrO 3The mass body volume concentrations is 49mg/L, and surplus is water.
CN2013103649531A 2013-08-18 2013-08-18 Protective treatment method of aluminum alloy surface Pending CN103388167A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2013103649531A CN103388167A (en) 2013-08-18 2013-08-18 Protective treatment method of aluminum alloy surface

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2013103649531A CN103388167A (en) 2013-08-18 2013-08-18 Protective treatment method of aluminum alloy surface

Publications (1)

Publication Number Publication Date
CN103388167A true CN103388167A (en) 2013-11-13

Family

ID=49532584

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2013103649531A Pending CN103388167A (en) 2013-08-18 2013-08-18 Protective treatment method of aluminum alloy surface

Country Status (1)

Country Link
CN (1) CN103388167A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103774146A (en) * 2014-01-09 2014-05-07 南昌航空大学 Deoxidation treatment method for chemical milling pretreatment of aluminum alloy
CN105937046A (en) * 2016-06-28 2016-09-14 苏州有色金属研究院有限公司 Treatment method for improving corrosion resistance of aluminum alloy
CN106501480A (en) * 2016-11-30 2017-03-15 江西洪都航空工业集团有限责任公司 A kind of method for differentiating aluminium lithium alloy chromic acid anodizing deoxidation effect
CN112342587A (en) * 2020-10-20 2021-02-09 天长市京发铝业有限公司 Aluminum plate anodic oxidation method

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3733291A (en) * 1971-07-23 1973-05-15 Sprague Electric Co Formation process for producing dielectric aluminum oxide films
US6149795A (en) * 1998-10-27 2000-11-21 The Boeing Company Fungus resistant boric acid-sulfuric acid anodizing
CN1958847A (en) * 2006-11-21 2007-05-09 广东华昌铝厂有限公司 Chemical treating liquid of shining sand face for surface of aluminum product and alloy, and treating technique
CN101280449A (en) * 2007-04-06 2008-10-08 北京化工大学 Mixed acid anodic oxidation method for aluminum alloy structure bonding

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3733291A (en) * 1971-07-23 1973-05-15 Sprague Electric Co Formation process for producing dielectric aluminum oxide films
US6149795A (en) * 1998-10-27 2000-11-21 The Boeing Company Fungus resistant boric acid-sulfuric acid anodizing
CN1958847A (en) * 2006-11-21 2007-05-09 广东华昌铝厂有限公司 Chemical treating liquid of shining sand face for surface of aluminum product and alloy, and treating technique
CN101280449A (en) * 2007-04-06 2008-10-08 北京化工大学 Mixed acid anodic oxidation method for aluminum alloy structure bonding

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
张金生等: "脱氧工艺对铝合金表面粘接性能的影响", 《材料工程》 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103774146A (en) * 2014-01-09 2014-05-07 南昌航空大学 Deoxidation treatment method for chemical milling pretreatment of aluminum alloy
CN103774146B (en) * 2014-01-09 2016-05-18 南昌航空大学 A kind of deoxidation treatment method in Aluminium Alloy after Chemical Milling pre-treatment
CN105937046A (en) * 2016-06-28 2016-09-14 苏州有色金属研究院有限公司 Treatment method for improving corrosion resistance of aluminum alloy
CN106501480A (en) * 2016-11-30 2017-03-15 江西洪都航空工业集团有限责任公司 A kind of method for differentiating aluminium lithium alloy chromic acid anodizing deoxidation effect
CN112342587A (en) * 2020-10-20 2021-02-09 天长市京发铝业有限公司 Aluminum plate anodic oxidation method

Similar Documents

Publication Publication Date Title
US5304257A (en) Trivalent chromium conversion coatings for aluminum
US5374347A (en) Trivalent chromium solutions for sealing anodized aluminum
AU2016363456B2 (en) Chromium-free surface-treated tinplate, production method and surface treating agent therefor
CN100552086C (en) Normal temperature fast filming fluid for aluminium alloy surface and using method thereof
WO2017000315A1 (en) Titanium-zirconium coloured chromium-free passivation solution for surface treatment of aluminium alloy, method for treating aluminium alloy surface using same, and use thereof
CN102586769B (en) A kind of phosphate-free metal surface treatment agent and using method thereof
CN103388167A (en) Protective treatment method of aluminum alloy surface
CN105112904B (en) A kind of mechanical copper facing and copper alloy coating aggradation accelerant and application
CN109943836A (en) A kind of aluminum alloy surface chrome-free tanning agent and its application
CN103710688A (en) Weakly acidic non-phosphorus transforming agent
WO2012082353A2 (en) Process and seal coat for improving paint adhesion
CN101525747B (en) Clean rare-earth salt passivation solution
CN103272749A (en) Surface treatment method of zinc alloy die casting
CN104451636A (en) Chromium-free passivation solution for tin-plated steel plate and preparation method of chromium-free passivation solution
CN116373410A (en) Preparation process of high-punching-depth corrosion-resistant aluminum plastic film
WO2004050581A2 (en) Passivating of tin, zinc and steel surfaces
CN103254782A (en) Corrosion resistant metal surface silane treatment agent and preparation method thereof
CN101386982A (en) Magnesium alloy corrosion proof calcium salt processing solution
US3400058A (en) Electrochemical process for andic coating of metal surfaces
CN104250755A (en) Passivation technology of aluminum alloy cylinder cover
CN103254778A (en) Salt spray resistant metal surface silane treatment agent and preparation method thereof
CN106086852A (en) A kind of surface processes uses economical passivating solution
CN104988562B (en) A kind of cast member electrophoretic process method
CN103254771A (en) Acidproof metal surface silane treatment agent and preparation method thereof
WO2019000441A1 (en) Silane coating, metal workpiece and coating treatment method thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20131113