CN104005059A - Method for electroplating chromium on TC1 titanium alloy and TC2 titanium alloy - Google Patents

Method for electroplating chromium on TC1 titanium alloy and TC2 titanium alloy Download PDF

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Publication number
CN104005059A
CN104005059A CN201410257959.3A CN201410257959A CN104005059A CN 104005059 A CN104005059 A CN 104005059A CN 201410257959 A CN201410257959 A CN 201410257959A CN 104005059 A CN104005059 A CN 104005059A
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Prior art keywords
titanium alloy
chromium
temperature
solution
described step
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Chinese (zh)
Inventor
于海
于宽深
沙春鹏
汤智慧
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Shenyang Aircraft Industry Group Co Ltd
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Shenyang Aircraft Industry Group Co Ltd
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Priority to CN201410257959.3A priority Critical patent/CN104005059A/en
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Abstract

The invention discloses a method for electroplating chromium on TC1 titanium alloy and TC2 titanium alloy. The method includes the first step of removing oil on the TC1 titanium alloy and the TC2 titanium alloy, the second step of conducting sand blasting on the TC1 titanium alloy and the TC2 titanium alloy after oil removal, the third step of activating the TC1 titanium alloy and the TC2 titanium alloy after sand blasting, the fourth step of hydrogenating the TC1 titanium alloy and the TC2 titanium alloy after activation, the fifth step of plating milky-white chromium on the TC1 titanium alloy and the TC2 titanium alloy after hydrogenation, and the sixth step of plating hard chromium on the TC1 titanium alloy and the TC2 titanium alloy. Through the method, the influences of oxidation films on the chromium electroplating of the TC1 titanium alloy and the TC2 titanium alloy are eliminated, the performance of base materials of the TC1 titanium alloy and the TC2 titanium alloy is guaranteed, and the excellent performance of the TC1 titanium alloy and the TC2 titanium alloy is effectively developed.

Description

A kind of on TC1, TC2 titanium alloy the method for electrodeposited chromium
Technical field
The present invention relates to a kind of method at titanium alloy surface electrodeposited chromium, be specifically related to a kind of method at TC1, TC2 titanium alloy surface electrodeposited chromium.
Background technology
TC1, TC2 titanium alloy have many good performances, and often so that light specific gravity, erosion resistance be good etc., advantage is widely used in Aeronautics and Astronautics, navigation and Chemicals.Yet its wear resistance is poor, the heat conduction of, surface film responsive to hot salt corrosion and electroconductibility is low, welding difficulty etc., also makes it in application, be restricted.The advantages such as chromium coating has microhardness high (HV > 700), wear resistance is good, coating is stable, have been widely used in the protection of aircraft high-duty steel part.Yet TC1, TC2 titanium alloy substrate be very easily rapid natural oxidation in air, the oxide film that surface produces has seriously hindered normally carrying out of electroplating, therefore, how to eliminate the impact of TC1, TC2 oxidation film on titanium alloy surface, at TC1, TC2 titanium alloy surface, carry out electrodeposited chromium, to guarantee the premium properties of titanium alloy self, solve again the poor shortcoming of its surface abrasion resistance, and then to improve its over-all properties be the problem that those skilled in the art need solution badly.
Summary of the invention
The problem and shortage existing for solving prior art, the invention provides a kind of on TC1, TC2 titanium alloy the method for electrodeposited chromium, the method has not only been eliminated the impact of oxide film on TC1, TC2 titanium alloy electrodeposited chromium, also guaranteed the performance of TC1, TC2 titanium alloy base material, make TC1, TC2 titanium alloy premium properties be effectively played.
For the technical solution adopted in the present invention that achieves the above object is,
On TC1, TC2 titanium alloy, a method for electrodeposited chromium, comprises the steps:
1) by TC1, the oil removing in removing oil solution of TC2 titanium alloy, till Ex-all;
Preferably, oil removing solution composition is: sodium hydroxide 60g/L-80g/L, and sodium carbonate 30g/L-50g/L, tertiary sodium phosphate 30g/L-50g/L, water glass 10g/L-30g/L, surplus is water, temperature is 75 ℃-95 ℃.
2) TC1 after oil removing, TC2 titanium alloy are adopted to quartz sand or emergy sandblast, blasting pressure is 0.3MPa-0.5MPa;
3) TC1 after sandblast, TC2 titanium alloy being put into temperature is the standing 30s-45s of acidic solution of 18 ℃-25 ℃, activates and makes TC1, TC2 titanium alloy remove thickness 2 μ m-3 μ m;
Preferably, acidic solution consists of: hydrochloric acid (ρ=1.19g/ml) 40ml/L-50ml/L, and 40% (v/v) hydrofluoric acid 25ml/L-30ml/L, surplus is water.
4) by TC1, TC2 titanium alloy after activation, in temperature, be standing 60min-90min in the sulfuric acid of 18 ℃-25 ℃ and hydrochloric acid, carry out hydrogenation;
Preferably, by volume, sulfuric acid (ρ=1.84g/ml): hydrochloric acid (ρ=1.19g/ml)=65:35.
5) TC1 after hydrogenation, TC2 titanium alloy are plated to milky white chromium;
Solution composition is as follows:
Condition:
Temperature 70 degree-80 degree
Current density 30A/dm 2-40A/dm 2
Time 1h.
6) again to TC1 or TC2 titanium alloy hard chrome plating
Solution composition is as follows:
Condition:
Temperature 50 degree-60 degree
Current density 45A/dm 2-55A/dm 2
Time sedimentation rate: 20 μ m/h-30 μ m/h.
Adopt the present invention a kind of on TC1, TC2 titanium alloy the method for electrodeposited chromium, not only effectively eliminated the impact of oxide film on TC1, TC2 titanium alloy electrodeposited chromium, the performance that has guaranteed TC1, TC2 titanium alloy base material, is not fully exerted the over-all properties of TC1, TC2 titanium alloy.
Embodiment
The method of 1 one kinds of electrodeposited chromiums on TC1, TC2 titanium alloy of embodiment
(1) step is as follows:
1) by TC1, TC2 titanium alloy following except oil removing in oil solution, till Ex-all;
Remove oil solution: sodium hydroxide 70g/L, sodium carbonate 40g/L, tertiary sodium phosphate 40g/L, water glass 20g/L, surplus is water, temperature is 75 degree-95 degree.
2) TC1 after oil removing, TC2 titanium alloy are adopted to quartz sand or emergy sandblast, blasting pressure is 0.4MPa;
3) TC1 after sandblast, TC2 titanium alloy being put into temperature is 18 ℃-25 ℃, by hydrochloric acid (ρ=1.19g/ml) 45ml/L, hydrofluoric acid 40% (v/v) 25ml/L, surplus is water, standing 30s-45s in the acidic solution forming, activates and makes TC1, TC2 titanium alloy remove thickness 2 μ m-3 μ m;
4) by TC1, TC2 titanium alloy after activation, in temperature, be 18 ℃-25 ℃, standing 60min-90min in sulfuric acid (ρ=1.84g/ml) and hydrochloric acid (ρ=1.19g/ml) mixing solutions that 65:35 forms by volume, carries out hydrogenation;
5) TC1 after hydrogenation, TC2 titanium alloy are plated to milky white chromium under following component solution and condition,
Solution composition:
Condition: temperature 70 degree-80 degree; Current density 30A/dm 2-40A/dm 2; Time 1h.
6) again to TC1, TC2 titanium alloy hard chrome plating hard chrome plating under following component solution and condition,
Solution composition:
Condition: temperature 50 degree-60 degree; Current density 45A/dm 2-55A/dm 2; Sedimentation rate: 20 μ m/h-30 μ m/h.That is: electroplate 30min-45min during thickness 10 μ m-20 μ m; During thickness 20 μ m-40 μ m, electroplate 60min-90min; During thickness 40 μ m-80 μ m, electroplate 120min-180min.
(2) result
According to this method, electroplate, solved in titanium alloy air after spontaneous oxide film cannot plating a difficult problem, increase substantially the bonding force of titanium alloy substrate and chromium coating, make chromium coating can effectively exercise its function.Coating surface is for being slightly with bright grey azury, and coating is fine and close, evenly, and smooth surface, smooth, has metalluster, without coarse, bubble, come off, the defect such as ingotism, surperficial after grinding (grind, bore and grind), coating is without peeling or come off.
According to said method after electrodeposited chromium.TC1, two kinds of titanium alloy material self performance impacts of TC2 are all met the requirements, and hydrogen embrittlement test is pressed ASTM F519 method, and the hydrogen content after plating is about 0.0120%, meets material requirements; Tensile strength properties is pressed HB5214 test, and elongation reduces by 15.7%, and relative reduction in area reduces by 21.3%, but tensile strength is substantially constant; Fatigue property is pressed HB5152 test and is reduced about 379MPa.

Claims (6)

1. a method for electrodeposited chromium on TC1, TC2 titanium alloy, is characterized in that, comprises the steps:
1) oil removing in removing oil solution by TC1 or TC2 titanium alloy;
2) TC1 after oil removing, TC2 titanium alloy are adopted to quartz sand or emergy sandblast, blasting pressure is 0.3MPa-0.5MPa;
3) TC1 after sandblast or TC2 titanium alloy being put into temperature is the standing 30s-45s of acidic solution of 18 ℃-25 ℃, activates and makes TC1 or TC2 titanium alloy remove thickness 2 μ m-3 μ m;
4) by the TC1 after activation or TC2 titanium alloy, in temperature, be standing 60min-90min in the mixed solution of the sulfuric acid of 18 ℃-25 ℃ and hydrochloric acid, carry out hydrogenation;
5) TC1 after hydrogenation or TC2 titanium alloy are plated to milky white chromium;
6) again to TC1 or TC2 titanium alloy hard chrome plating.
2. method according to claim 1, is characterized in that, described step 1) in oil removing solution composition be: sodium hydroxide 60g/L-80g/L, sodium carbonate 30g/L-50g/L, tertiary sodium phosphate 30g/L-50g/L, water glass 10g/L-30g/L, surplus is water, and temperature is 75 ℃-95 ℃.
3. method according to claim 1, is characterized in that, described step 3) in acidic solution consist of: hydrochloric acid 40ml/L-50ml/L, the hydrofluoric acid 25ml/L-30ml/L that volumetric concentration is 40%, surplus is water.
4. method according to claim 1, is characterized in that, described step 4) in by volume, sulfuric acid: hydrochloric acid=65:35.
5. method according to claim 1, is characterized in that, described step 5) be specially and under following component solution and condition, plate milky white chromium,
Condition: temperature: 70 ℃-80 ℃; Current density 30A/dm 2-40A/dm 2; Time 1h.
6. method according to claim 1, is characterized in that, described step 6) be specially hard chrome plating under following component solution and condition,
Chromic trioxide 200g/L-250g/L
Sulfuric acid ρ=1.84g/ml 2.0g/L-2.5g/L
Chromium sesquioxide 3g/L-8g/L
Condition: temperature: 50 ℃-60 ℃; Current density 45A/dm 2-55A/dm 2; Sedimentation rate: 20 μ m/h-30 μ m/h.
CN201410257959.3A 2014-06-11 2014-06-11 Method for electroplating chromium on TC1 titanium alloy and TC2 titanium alloy Pending CN104005059A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104372392A (en) * 2014-11-28 2015-02-25 沈阳飞机工业(集团)有限公司 Method for improving uniformity of small-curvature semiarc-surface chromium coating
CN104404578A (en) * 2014-11-28 2015-03-11 沈阳飞机工业(集团)有限公司 Method for electrochromism processing of workpiece
CN107313079A (en) * 2017-07-31 2017-11-03 安徽沃德气门制造有限公司 A kind of automobile air valve rapid chrome plating technique
CN111005045A (en) * 2019-12-31 2020-04-14 西安西工大超晶科技发展有限责任公司 Preparation method of titanium and titanium alloy surface coating

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104372392A (en) * 2014-11-28 2015-02-25 沈阳飞机工业(集团)有限公司 Method for improving uniformity of small-curvature semiarc-surface chromium coating
CN104404578A (en) * 2014-11-28 2015-03-11 沈阳飞机工业(集团)有限公司 Method for electrochromism processing of workpiece
CN107313079A (en) * 2017-07-31 2017-11-03 安徽沃德气门制造有限公司 A kind of automobile air valve rapid chrome plating technique
CN111005045A (en) * 2019-12-31 2020-04-14 西安西工大超晶科技发展有限责任公司 Preparation method of titanium and titanium alloy surface coating

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Application publication date: 20140827