CN114525501A - Magnesium alloy sealing reinforcing agent and sealing reinforcing treatment process - Google Patents

Magnesium alloy sealing reinforcing agent and sealing reinforcing treatment process Download PDF

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CN114525501A
CN114525501A CN202111642372.0A CN202111642372A CN114525501A CN 114525501 A CN114525501 A CN 114525501A CN 202111642372 A CN202111642372 A CN 202111642372A CN 114525501 A CN114525501 A CN 114525501A
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magnesium alloy
sealing
treatment
acid
agent
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温远文
熊豪
况金权
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Bo Luo Xian Domin Chemical Co ltd
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Bo Luo Xian Domin Chemical Co ltd
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    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C22/00Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C22/05Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C22/00Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C22/78Pretreatment of the material to be coated

Abstract

The invention belongs to the technical field of metal surface treatment, and discloses a magnesium alloy sealing reinforcing agent and a sealing reinforcing treatment process, wherein the magnesium alloy sealing reinforcing agent comprises the following components: 1-50 g/L of fatty acid, 2-100 g/L of alcohol, 5-100 g/L of organic amine, 0.1-5 g/L of complexing agent, 0.5-10 g/L of inorganic base and 0.2-10 g/L of vanadium salt. Under the synergistic effect of the components, the corrosion resistance of the magnesium alloy workpiece, the resistance stability of the surface of the magnesium alloy workpiece and the adhesion stability of the coating or auxiliary materials on the surface of the magnesium alloy can be obviously enhanced after the magnesium alloy workpiece is treated by the sealing reinforcing agent.

Description

Magnesium alloy sealing reinforcing agent and sealing reinforcing treatment process
Technical Field
The invention relates to the technical field of metal surface treatment, in particular to a magnesium alloy sealing reinforcing agent and a sealing reinforcing treatment process.
Background
AZ91D belongs to cast magnesium alloy, and is characterized in that: the high-strength high-impact-resistance heat dissipation alloy has the advantages of small density, high strength, large elastic modulus, good heat dissipation, good shock absorption, larger impact load bearing capacity than aluminum alloy, and good organic matter and alkali corrosion resistance, is widely applied to the industries of aviation, aerospace, automobiles, high-speed rails, 3C and the like, and is mainly used for shells of electric products in the 3C industry as follows due to quite excellent heat dissipation effect: electronic products such as mobile phones and computers, or special-shaped supports and the like.
In production and application, the magnesium alloy has extremely active metallicity and low electrode potential, so the magnesium alloy has extremely high chemical and electrochemical activity and is very easy to corrode in air, and although the surface formation treatment technology of the magnesium alloy is greatly improved in recent years, the problems of large resistance variation after salt spray, poor salt spray corrosion resistance, more white spots on the surface of a product after salt spray, unstable adhesion of an adhesive auxiliary material/paint adhesion and the like of the magnesium alloy are still not well solved, so the excellent performance of the magnesium alloy cannot be fully exerted.
Therefore, how to further enhance the mechanical properties and electrochemical properties of the surface of the magnesium alloy is a problem that researchers in the field need to solve.
Disclosure of Invention
In order to overcome the defects of the prior art, the invention mainly aims to provide a magnesium alloy sealing reinforcing agent, which can remarkably enhance the salt spray resistance and the paint adhesion of the magnesium alloy after the magnesium alloy is used, and can ensure that the surface resistance stability of the magnesium alloy is maintained.
The invention also aims to provide a sealing and strengthening treatment process using the magnesium alloy sealing and strengthening agent.
In order to achieve the purpose, the invention adopts the following technical scheme:
a magnesium alloy sealing reinforcing agent comprises the following components: 1-50 g/L of fatty acid, 2-100 g/L of alcohol, 5-100 g/L of organic amine, 0.1-5 g/L of complexing agent, 0.5-10 g/L of inorganic base and 0.2-10 g/L of vanadium salt.
Further, the fatty acid is at least one of saturated fatty acid and unsaturated fatty acid; the saturated fatty acid is at least one of dodecanoic acid, tetradecanoic acid, hexadecanoic acid, octadecanoic acid, eicosanoic acid and the like; the unsaturated fatty acid is at least one of linolenic acid, linoleic acid, oleic acid and the like.
Further, the alcohol is at least one of ethanol, ethylene glycol, secondary alcohol and the like.
Further, the complexing agent is at least one of sodium citrate, potassium sodium tartrate, disodium ethylene diamine tetraacetate, hydroxyethylidene diphosphonic acid and the like.
Further, the organic amine is at least one of monoethanolamine, diethanolamine, triethanolamine and the like.
Further, the inorganic base is at least one of sodium hydroxide, potassium hydroxide, sodium carbonate, potassium carbonate and the like.
Further, the vanadium salt is at least one of amine metavanadate, sodium metavanadate and the like.
The invention also provides a closed reinforced treatment process, which comprises the following steps: sequentially carrying out oil removal treatment, acid pickling activation treatment, neutralization treatment, formation treatment, sealing treatment and sealing enhancement treatment on the magnesium alloy workpiece;
and the sealing and reinforcing treatment is to immerse the magnesium alloy workpiece subjected to the sealing treatment into the magnesium alloy sealing and reinforcing agent at the temperature of 15-60 ℃ for treatment for 5-120 s.
Further, the oil removing treatment is to place the magnesium alloy workpiece into an oil removing agent at 50-60 ℃ for ultrasonic soaking for 3-10 min, wherein the oil removing agent comprises the following components: 5-10 g/L of sodium hydroxide, 5-10 g/L of trisodium phosphate, 5-10 g/L of sodium tripolyphosphate, 3-6 g/L of sodium gluconate, 1-10 g/L of sodium metasilicate pentahydrate, 2-4 g/LTX-10 and 2-4 g/L of AEO-9.
Further, the pickling activation treatment is to put the magnesium alloy workpiece subjected to the oil removal treatment into a pickling agent at 50-60 ℃ for soaking for 1-2 min, wherein the pickling agent comprises the following components: 10-30 g/L citric acid, 10-20 g/L lactic acid, 1-5 g/L malic acid and 0.2-2 ml/L2-ethylhexyl sodium sulfate.
Further, the neutralization treatment is to put the magnesium alloy workpiece subjected to the pickling activation treatment into a neutralizer at the temperature of 70-80 ℃ for soaking for 2-3 min, wherein the neutralizer comprises the following components: 50-100 g/L sodium hydroxide, 10-50 g/L sodium nitrate, 1-5 g/L EDTA-2 Na.
Further, the formation treatment is to place the magnesium alloy workpiece subjected to neutralization treatment into a formation agent at normal temperature for treatment for 30-60 s. The formation agent comprises the following components: 10-20 g/L phosphoric acid, 5-10 g/L maruzu salt, 10-20 g/L calcium dihydrogen phosphate and 0.2-2 ml/L2-ethylhexyl sodium sulfate.
Further, the sealing treatment is to place the magnesium alloy workpiece subjected to formation treatment into a sealing agent at 40-60 ℃ for treatment for 1-5 min, wherein the sealing agent comprises the following components: 1-10 g/L amine metavanadate, 0.5-2 ml/L ammonia water, and 0.2-2 ml/L2-ethylhexyl sodium sulfate.
Compared with the prior art, the invention has the following advantages;
(1) the magnesium alloy sealing reinforcing agent provided by the invention comprises the following components: 1-50 g/L of fatty acid, 2-100 g/L of alcohol, 5-100 g/L of organic amine, 0.1-5 g/L of complexing agent, 0.5-10 g/L of inorganic base and 0.2-10 g/L of vanadium salt. Under the synergistic effect of the components, the magnesium alloy workpiece can form a uniform fatty acid-vanadium mixed film on the surface after being treated by the sealing reinforcing agent, the corrosion resistance of the magnesium alloy workpiece can be obviously enhanced by the mixed film, and meanwhile, the existence of vanadium ions in the mixed film can enable the magnesium alloy workpiece to still keep stable resistance after being treated by salt spray and can also improve the adhesion performance of subsequent coatings or auxiliary materials on the surface of the magnesium alloy.
(2) The closed reinforcement treatment process provided by the invention has the advantages of simple operation, mild conditions and short process time, and the corrosion resistance, the resistance stability and the adhesion stability of auxiliary materials/coatings on the surface of the magnesium alloy workpiece are obviously enhanced under the mutual cooperation of all treatment steps.
Drawings
FIG. 1 is a graph of the effects of magnesium alloy workpieces of examples 1, 2, 3 and 1 after 24h salt spray test;
FIG. 2 is a resistance test chart of the magnesium alloy workpieces of example 1 and comparative example 1 after 24h salt spray test;
FIG. 3 is a Dainipen test chart of the magnesium alloy workpieces of example 1 and comparative example 1 of the present invention;
FIG. 4 is a graph showing the effect of the salt spray test for 12 hours on the magnesium alloy workpieces of example 1 and comparative example 2 of the present invention;
FIG. 5 is a graph showing the effect of the magnesium alloy workpieces of example 1 and comparative example 1 of the present invention after 24h salt spray test;
FIG. 6 is a graph showing the effect of paint adhesion test on magnesium alloy workpieces according to example 1 and comparative example 1 of the present invention.
Detailed Description
The present invention will be described in further detail below with reference to specific embodiments and examples in conjunction with the accompanying drawings, but the embodiments of the present invention are not limited thereto. All the raw materials and reagents used in the present invention are commercially available raw materials and reagents, unless otherwise specified. In the examples, the components are used in g and mL in parts by mass.
Example 1
Preparing a magnesium alloy sealing reinforcing agent: weighing 0.5g of EDTA-2Na to dissolve in 200ml of pure water, weighing 3g of oleic acid, dissolving in 6ml of ethanol, adding into 200ml of pure water in which the EDTA-2Na is dissolved, adding 6g of triethanolamine, stirring, dissolving, adding 2g of sodium hydroxide, stirring, dissolving for later use, weighing 3g of ammonium metavanadate, dissolving in 200ml of 80 ℃ hot water, adding into the prepared solution, stirring, mixing uniformly, and finally adding pure water to 1L.
The magnesium alloy sealing and reinforcing treatment process comprises the following steps:
oil removal treatment: taking a magnesium alloy AZ91D mobile phone middle plate product, deoiling (temperature is 50 ℃, time is 5 minutes, treatment mode is ultrasonic wave soaking) by using deoiling agent (the content of sodium hydroxide is 10g/L, the content of trisodium phosphate is 10g/L, the content of sodium tripolyphosphate is 5g/L, the content of sodium gluconate is 3g/L, the content of sodium metasilicate pentahydrate is 5g/L, the content of TX-10 is 2g/L, and the content of AEO-9 is 3g/L), washing for 3 times, and each time lasts for 20 seconds;
acid pickling and activating treatment: pickling the degreased magnesium alloy product with a pickling agent (the citric acid content is 20g/L, the lactic acid content is 20g/L, the malic acid content is 5g/L, and the 2-ethylhexyl sodium sulfate content is 0.5ml/L) (the temperature is 55 ℃, the time is 60s, the treatment mode is soaking), and washing for 3 times, each time for 20 seconds;
and (3) neutralization treatment: neutralizing and dedusting the magnesium alloy product after the pickling by using a neutralizer (the content of sodium hydroxide is 50g/L, the content of sodium nitrate is 20g/L, and the content of EDTA-2Na is 2g/L) (the temperature is 75 ℃, the time is 3min, the treatment mode is ultrasonic soaking), and washing for 3 times and 20 seconds each time;
formation treatment: carrying out chemical treatment (temperature: normal temperature, time: 45s, treatment mode: soaking) on the neutralized magnesium alloy product by using a chemical agent (the content of phosphoric acid is 15g/L, the content of Marshall salt is 5g/L, the content of monocalcium phosphate is 10g/L, and the content of 2-ethylhexyl sodium sulfate is 0.2ml/L), and washing with pure water for 3 times, each time for 20 s;
sealing treatment: sealing the formed magnesium alloy product by using a sealing agent (the content of ammonium metavanadate is 3.5g/L, the content of 28% ammonia water is 0.3ml/L, and the content of 2-ethylhexyl sodium sulfate is 0.2g/L) (the temperature is 50 ℃, the time is 3min, the treatment mode is soaking), and washing with pure water for 3 times, wherein each time lasts for 20 seconds;
sealing and reinforcing treatment: and (2) putting the magnesium alloy product into the prepared sealing reinforcing agent for treatment, wherein the treatment parameters are as follows: temperature: 25 ℃, time: and (3) washing with pure water at normal temperature for 20 seconds for 30 seconds. Heated (60 ℃) and cleaned by pure water for 1 time and 5 seconds, and then baked at a temperature of 130 ℃ for 20 min.
Example 2
Preparing a magnesium alloy sealing reinforcing agent: weighing 0.5g of EDTA-2Na to dissolve in 200ml of pure water, weighing 4g of oleic acid, dissolving in 8ml of ethanol, adding into 200ml of pure water in which the EDTA-2Na is dissolved, adding 8g of triethanolamine, stirring, dissolving, adding 0.5g of sodium hydroxide, stirring, dissolving 3g of ammonium metavanadate, dissolving in 200ml of 80-DEG hot water, adding into the prepared solution, stirring, mixing uniformly, and finally adding pure water to 1L.
Wherein the technological parameters of oil removal, acid washing activation, neutralization, formation and sealing are the same as those of the example 1.
Sealing and reinforcing treatment: and (2) putting the magnesium alloy product into the prepared sealing reinforcing agent for treatment, wherein the treatment parameters are as follows: temperature: 25 ℃, time: 80s, washing with pure water at normal temperature for 3 times, 20s each time, washing with warm (60 deg.C) pure water for 1 time, 5s, and baking at 130 deg.C for 20 min.
Example 3
Preparing a magnesium alloy sealing reinforcing agent: weighing 0.5g of EDTA-2Na to dissolve in 200ml of pure water, weighing 5g of oleic acid, dissolving in 10ml of ethanol, adding into 200ml of pure water in which the EDTA-2Na is dissolved, adding 10g of triethanolamine, stirring, dissolving, adding 5g of sodium hydroxide, stirring, dissolving for later use, weighing 5g of ammonium metavanadate, dissolving in 400ml of 80 ℃ hot water, adding into the prepared solution, stirring, mixing uniformly, and finally adding pure water to 1L.
Wherein the technological parameters of oil removal, acid washing activation, neutralization, formation and sealing are the same as those of the example 1.
Sealing and reinforcing treatment: and (2) putting the magnesium alloy product into the prepared sealing reinforcing agent for treatment, wherein the treatment parameters are as follows: temperature: 50 ℃, time: 30s, washing with pure water at normal temperature for 3 times, 20 seconds each time, washing with warm (60 deg.C) pure water for 1 time, 5 seconds, and baking at 130 deg.C for 20 min.
Example 4
Preparing a magnesium alloy sealing reinforcing agent: weighing 3g of sodium citrate and dissolving the sodium citrate into 200ml of pure water, weighing 10g of dodecanoic acid, mixing and dissolving the dodecanoic acid with 30ml of ethylene glycol, adding the mixture into 200ml of pure water in which the sodium citrate is dissolved, adding 6g of monoethanolamine and stirring and mixing, adding 6g of potassium hydroxide and stirring and mixing for later use, weighing 8g of sodium metavanadate, dissolving the sodium metavanadate with 200ml of hot water at 80 ℃, adding the solution prepared before, stirring and mixing uniformly, and finally adding the pure water to 1L.
Wherein the technological parameters of degreasing, acid washing activation, neutralization, formation, sealing and sealing enhancement are the same as those of the embodiment 1.
Example 5
Preparing a magnesium alloy sealing reinforcing agent: weighing 2g of potassium sodium tartrate and dissolving the potassium sodium tartrate in 200ml of pure water, weighing 8g of linolenic acid, mixing and dissolving the linolenic acid with 30ml of secondary alcohol, adding the mixture into 200ml of pure water in which the potassium sodium tartrate is dissolved, adding 15g of diethanolamine and stirring and mixing, adding 0.5g of sodium carbonate and stirring and mixing for later use, weighing 3g of ammonium metavanadate, dissolving the ammonium metavanadate in 200ml of hot water at 80 ℃, adding the mixture into the prepared solution, stirring and mixing uniformly, and finally adding pure water to 1L.
Wherein the technological parameters of degreasing, acid washing activation, neutralization, formation, sealing and sealing enhancement are the same as those of the embodiment 1.
Comparative example 1
The magnesium alloy product is treated according to the following process (without sealing and strengthening treatment).
The treatment process comprises the following steps: oil removal, water washing, acid washing, water washing, neutralization, water washing, formation, water washing, sealing, water washing and drying at 130 ℃ for 20 min.
Wherein the technological parameters of oil removal, acid washing activation, neutralization, formation and sealing are the same as those of the example 1.
Comparative example 2
Preparing a magnesium alloy sealing reinforcing agent: weighing 0.5g of EDTA-2Na to dissolve in 200ml of pure water, weighing 3g of oleic acid, dissolving in 6ml of ethanol, adding into 200ml of pure water in which the EDTA-2Na is dissolved, adding 6g of triethanolamine, stirring, dissolving, adding 2g of sodium hydroxide, stirring, mixing uniformly, and finally adding pure water to 1L.
The technological parameters of oil removal, acid washing activation, neutralization, formation, sealing and sealing enhancement are the same as those of the example 1, and the main difference from the example 1 is that the magnesium alloy sealing enhancer does not contain vanadium salt.
The magnesium alloy workpieces treated in examples 1 to 5 and comparative examples 1 to 2 were subjected to a salt spray test, a resistance test and a paint adhesion stability test, and the specific results are shown in table 1.
The salt spray test method comprises the following steps: and (5) continuously spraying 5% sodium chloride neutral salt mist for 24 hours to observe whether white spots and corrosion spots exist on the surface of the magnesium alloy workpiece.
And (3) resistance testing: and (3) carrying out resistance test on the magnesium alloy workpiece subjected to the salt spray test by adopting a resistance tester.
Testing the dyne pen: marking on the surface of the magnesium alloy workpiece by using a 36# dyne pen before the salt spray test, and observing whether the mark is diffused within 10 min.
And (3) testing the spraying adhesion of the coating: and (4) spraying paint on the treated magnesium alloy workpiece, and testing the adhesive force of the magnesium alloy workpiece.
TABLE 1 Effect of various treatment groups on the Performance of magnesium alloy conversion coatings
Figure BDA0003442830330000061
Figure BDA0003442830330000071
As can be seen from the test results in Table 1, the experimental results: in the same salt spray (24h) test conditions, the combined effects of the salt spray corrosion resistance effect, the surface white point, the surface resistance after salt spray, the 36# dyne pen test and the paint adhesion stability test of example 1 are the best, and are the best example 1 of the present invention; examples 2-5 formula proportions and treatment parameters of the magnesium alloy reinforcing treatment agent are correspondingly adjusted compared with example 1, and it is found that a few white spots or salt spray corrosion resistance is slightly reduced after salt spray, surface resistance and dyne test are not changed greatly, and coating adhesion stability is not changed greatly; comparative example 1 is a blank comparative item which is not treated by a sealing reinforcing agent, salt spray corrosion resistance effect is passed, but a large number of white dots are generated on the surface of a workpiece after salt spray, the surface resistance of the workpiece after salt spray is unstable, most of the dots are larger than 5 omega, the white dot part resistance is larger, and the 36# before salt spray begins to diffuse after 10s of pen test, which shows that after the magnesium alloy sealing reinforcing agent is carried out, various physical properties of the magnesium alloy workpiece can be obviously enhanced; the comparative example 2 shows that the sealing reinforcing agent is not added with vanadium salt, the salt mist corrosion resistant effect of the sealing reinforcing agent is passed, the surface of a workpiece generates more white spots after salt mist, the surface resistance of the workpiece is unstable, most spots are larger than 5 omega, the resistance of white spot parts is larger, and 36# dyne pen tests and paint adhesion stability tests pass, which indicate that the sealing reinforcing agent for the magnesium alloy disclosed by the invention is a multi-component synergistic effect, and particularly, the salt mist resistance and the resistance stability of the surface of the magnesium alloy workpiece can be further enhanced by the mutual matching of the vanadium salt and the fatty acid.
As can be seen from fig. 1, fig. 1A, 1B, 1C, and 1D are the appearance images of the magnesium alloy workpieces of example 1, example 2, example 3, and comparative example 1 after 24h salt spray test, respectively, and it is apparent that comparative example 1 without the magnesium alloy strengthening treatment process generates a large number of white spots.
As can be seen from fig. 2, fig. 2A and 2B are resistance test results of the magnesium alloys of example 1 and comparative example 1 after 24h salt spray test, respectively, wherein the surface resistance of example 1 is 0.1 Ω, and the surface resistance of comparative example 1 is 6.3 Ω.
As can be seen in FIG. 3, the magnesium alloy of example 1 is compared before and after the Dainipen test in FIGS. 3A1 and 3A2, and it can be seen that the mark of example 1 is not significantly changed; the magnesium alloys of comparative example 1 of fig. 3B1, 3B2 were compared before and after the dyne test, beginning to diffuse after 10 s. The surface tension is large due to the fact that the pen test scratches appear in 10s and are diffused or shrunk, the adhesive effect of the auxiliary materials is influenced, and the auxiliary materials are not firm to adhere and are easy to warp edges or fall off; the scratch 10s is unchanged in the pen test, so that the surface tension is small, and the auxiliary materials are firmly adhered and are not easy to fall off.
As can be seen from fig. 4, fig. 4A and 4B are the effects of surface white spots of comparative example 2 and example 1 after the 12-h salt spray test, respectively, and it is clearly seen that example 1 has no white spots, while comparative example 2 has a small amount of white spots.
As can be seen from fig. 5, fig. 5A and 5B show the effect of surface white spots (using another magnesium alloy workpiece) after 24h salt spray test of example 1 and comparative example 1, respectively, and it is obvious that the surface of example 1 is uniform and has no white spots, while the surface of the un-nucleated reduced workpiece of comparative example 1 is significantly mottled and has more white spots.
As can be seen from fig. 6, fig. 6A and 6B respectively show the paint adhesion test effects of comparative example 1 and example 1, and it is obvious that the paint-dropping phenomenon does not occur when the magnesium alloy paint of example 1 is sprayed after the sealing and reinforcing treatment, and the paint-dropping phenomenon occurs to different degrees at the edge of the test knife-edge after the magnesium alloy paint of comparative example 1 is sprayed.
The above embodiments are the best mode for carrying out the present invention, but the embodiments of the present invention are not limited to the above embodiments, and any other changes, modifications, substitutions, combinations, and simplifications which do not depart from the spirit and principle of the present invention should be regarded as equivalent substitutions and are included in the scope of the present invention.

Claims (10)

1. The magnesium alloy sealing reinforcing agent is characterized by comprising the following components: 1-50 g/L of fatty acid, 2-100 g/L of alcohol, 5-100 g/L of organic amine, 0.1-5 g/L of complexing agent, 0.5-10 g/L of inorganic base and 0.2-10 g/L of vanadium salt.
2. The magnesium alloy sealing enhancer according to claim 1, wherein the fatty acid is at least one of a saturated fatty acid and an unsaturated fatty acid; the saturated fatty acid is at least one of dodecanoic acid, tetradecanoic acid, hexadecanoic acid, octadecanoic acid and eicosanoic acid; the unsaturated fatty acid comprises at least one of linolenic acid, linoleic acid and oleic acid.
3. The magnesium alloy sealing enhancer as claimed in claim 1, wherein the alcohol is at least one selected from the group consisting of ethanol, ethylene glycol and secondary alcohol.
4. The magnesium alloy sealing enhancer as set forth in claim 1, wherein said complexing agent is at least one selected from the group consisting of sodium citrate, potassium sodium tartrate, disodium ethylenediaminetetraacetate, hydroxyethylidene diphosphonic acid, and the like.
5. The magnesium alloy sealing enhancer as claimed in claim 1, wherein the organic amine is at least one selected from the group consisting of monoethanolamine, diethanolamine, triethanolamine.
6. The magnesium alloy sealing enhancer according to claim 1, wherein the inorganic base is at least one of sodium hydroxide, potassium hydroxide, sodium carbonate and potassium carbonate.
7. The magnesium alloy sealing enhancer as claimed in claim 1, wherein the vanadium salt is at least one of amine metavanadate and sodium metavanadate.
8. A closed reinforcement treatment process is characterized by comprising the following steps: sequentially carrying out oil removal treatment, acid pickling activation treatment, neutralization treatment, formation treatment, sealing treatment and sealing enhancement treatment on the magnesium alloy workpiece;
and the sealing and reinforcing treatment is to immerse the magnesium alloy workpiece subjected to the sealing treatment into the magnesium alloy sealing and reinforcing agent at the temperature of 15-60 ℃ for treatment for 5-120 s.
9. The closed reinforcement treatment process according to claim 8, wherein the formation treatment is to place the magnesium alloy workpiece subjected to neutralization treatment in a normal-temperature formation agent for 30-60 s. The formation agent comprises the following components: 10-20 g/L phosphoric acid, 5-10 g/L maruzu salt, 10-20 g/L calcium dihydrogen phosphate and 0.2-2 ml/L2-ethylhexyl sodium sulfate.
10. The sealing and reinforcing treatment process according to claim 8, wherein the sealing treatment is to place the magnesium alloy workpiece subjected to the formation treatment in a sealing agent at 40-60 ℃ for 1-5 min, and the sealing agent comprises the following components: 1-10 g/L amine metavanadate, 0.5-2 ml/L ammonia water, and 0.2-2 ml/L2-ethylhexyl sodium sulfate.
CN202111642372.0A 2021-12-29 2021-12-29 Magnesium alloy sealing reinforcing agent and sealing reinforcing treatment process Pending CN114525501A (en)

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CN111962053A (en) * 2020-08-12 2020-11-20 博罗县东明化工有限公司 AZ91D magnesium alloy white point inhibition sealant and using method thereof
CN113337812A (en) * 2021-04-26 2021-09-03 博罗县东明化工有限公司 Magnesium alloy conversion film enhancement treatment agent and magnesium alloy surface treatment method

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