CN106435543B - The preparation method of aero titanium alloy - Google Patents

The preparation method of aero titanium alloy Download PDF

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Publication number
CN106435543B
CN106435543B CN201610837724.0A CN201610837724A CN106435543B CN 106435543 B CN106435543 B CN 106435543B CN 201610837724 A CN201610837724 A CN 201610837724A CN 106435543 B CN106435543 B CN 106435543B
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plating
titanium alloy
composite
preparation
electroless
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CN106435543A (en
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吴长应
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Hunan Tuoyong Intelligent Technology Co.,Ltd.
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Wuhu Yangzhan New Material Technology Service 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
    • C23C18/00Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
    • C23C18/16Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
    • C23C18/48Coating with alloys
    • C23C18/50Coating with alloys with alloys based on iron, cobalt or nickel
    • 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
    • C23C18/00Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
    • C23C18/16Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
    • C23C18/18Pretreatment of the material to be coated
    • C23C18/1803Pretreatment of the material to be coated of metallic material surfaces or of a non-specific material surfaces

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  • Chemical & Material Sciences (AREA)
  • General Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemically Coating (AREA)

Abstract

The invention discloses the preparation methods of aero titanium alloy, include the following steps:A, the cleaning step of titanium alloy;B, the electroless plating step of titanium alloy, the chemical plating are Ni P Si C composite electroless-platings, i.e., cleaned titanium alloy are put into composite plating bath and carry out chemical plating, the condition of chemical plating is:Plating temperature is 80 90 DEG C, and PH is 6.5 7.5, and mixing speed is 10 20 revs/min, and plating solution useful load is 0.8 1.5dm2/ L, plating time 0.5 1 hours.Compared with prior art, the present invention by selecting stabilizer, the phosphorus content of titanium alloy that chemistry plates out is 3.33 3.35%, and hardness is 840 900HV, and friction coefficient is 0.6 0.7, and the stability of plating solution is good, and the service life of prepared plating solution is 1 1.5 hours.

Description

The preparation method of aero titanium alloy
Technical field
The invention belongs to the preparation methods of alloy, particularly belong to the preparation method of titanium alloy.
Background technology
Titanium alloy is a kind of novel structural material, has the characteristics that light weight, specific strength are high, in titanium alloy The characteristics of Ti6Al4V (TC4) is the material of main part of aircraft industry, but it is easily aoxidized there are surface, and hardness is less than 600HV.
Invention content
The technical problems to be solved by the invention are to provide a kind of preparation method of titanium alloy of hardness more than 800HV.
The present invention solve technical problem technical solution be:The preparation method of aero titanium alloy, includes the following steps:
A, the cleaning step of titanium alloy;B, the electroless plating step of titanium alloy.
The chemical plating be Ni-P-Si-C composite electroless-platings, i.e., by cleaned titanium alloy be put into composite plating bath into Row chemical plating, the condition of chemical plating are:Plating temperature is 80-90 DEG C, PH 6.5-7.5, and mixing speed is 10-20 revs/min, plating Liquid useful load is 0.8-1.5dm2/ L, plating time 0.5-1 hours.
In the composite plating bath, following substance is contained in every liter of solution:
The ammonium hydroxide is used for adjusting the pH value of plating solution in plating process.
The cleaning step of the titanium alloy includes the following steps successively:Sand paper polishing step, deoiling step, pickling step Suddenly, activation step.
The deoiling step is the titanium alloy polished with ultrasonic cleaning sand paper, ultrasonic frequency 50-70KHz, Cleaning 10-30 minutes.
The titanium alloy is Ti6Al4V (TC4).
Compared with prior art, the present invention by selecting 2- amino -5- sulfydryls -1,3,4- thiadiazoles, D- (+)-hexichol first As stabilizer, the phosphorus content of titanium alloy that chemistry plates out is for one water object of acyl tartaric acid, 1,3- dimethyl -6- semicarbazides pyrimidine 3.33-3.35%, hardness 840-900HV, friction coefficient 0.6-0.7, the stability of plating solution is good, the longevity of prepared plating solution Order is 1-1.5 hours.
Specific embodiment
With reference to embodiment, the present invention is described in detail.
Embodiment 1:
The preparation method of aero titanium alloy, includes the following steps:
A, the cleaning step of titanium alloy:
The cleaning step of the titanium alloy includes the following steps successively:Sand paper polishing step, deoiling step, pickling step Suddenly, activation step.
The deoiling step is Ti6Al4V (TC4) titanium alloy polished with ultrasonic cleaning sand paper, ultrasonic frequency For 50KHz, clean 30 minutes.
B, the electroless plating step of titanium alloy.
The chemical plating be Ni-P-Si-C composite electroless-platings, i.e., by cleaned titanium alloy be put into composite plating bath into Row chemical plating, the condition of chemical plating are:Plating temperature is 80 DEG C, and the PH that plating solution is adjusted with ammonium hydroxide is 6.5-7, mixing speed 10 Rev/min, plating solution useful load is 0.8dm2/ L, plating time 1 hour.
In the composite plating bath, following substance is contained in every liter of solution:
Embodiment 2:
The preparation method of aero titanium alloy, includes the following steps:
A, the cleaning step of titanium alloy:
The cleaning step of the titanium alloy includes the following steps successively:Sand paper polishing step, deoiling step, pickling step Suddenly, activation step.
The deoiling step is Ti6Al4V (TC4) titanium alloy polished with ultrasonic cleaning sand paper, ultrasonic frequency For 60KHz, clean 20 minutes.
B, the electroless plating step of titanium alloy.
The chemical plating be Ni-P-Si-C composite electroless-platings, i.e., by cleaned titanium alloy be put into composite plating bath into Row chemical plating, the condition of chemical plating are:Plating temperature is 85 DEG C, and the PH that plating solution is adjusted with ammonium hydroxide is 6.8-7.2, and mixing speed is 15 revs/min, plating solution useful load is 1.2dm2/ L, plating time 0.8 hour.
In the composite plating bath, following substance is contained in every liter of solution:
Embodiment 3:
The preparation method of aero titanium alloy, includes the following steps:
A, the cleaning step of titanium alloy:
The cleaning step of the titanium alloy includes the following steps successively:Sand paper polishing step, deoiling step, pickling step Suddenly, activation step.
The deoiling step is Ti6Al4V (TC4) titanium alloy polished with ultrasonic cleaning sand paper, ultrasonic frequency For 70KHz, clean 10 minutes.
B, the electroless plating step of titanium alloy.
The chemical plating be Ni-P-Si-C composite electroless-platings, i.e., by cleaned titanium alloy be put into composite plating bath into Row chemical plating, the condition of chemical plating are:Plating temperature is 90 DEG C, and the PH that plating solution is adjusted with ammonium hydroxide is 7.2-7.5, and mixing speed is 20 revs/min, plating solution useful load is 1.5dm2/ L, plating time 0.5 hour.
In the composite plating bath, following substance is contained in every liter of solution:
Embodiment 4:
In addition to stabilizer is 1mg thiocarbamide, remaining is same as Example 1.
Embodiment 5:
Except being not added with 2- amino -5- sulfydryl -1,3,4- thiadiazoles, one water object of D- (+)-dibenzoyl tartaric acid, 1,3- diformazans Outside base -6- semicarbazides pyrimidines, remaining is same as Example 1.
Bath life refers to that by plating solution be 80-90 DEG C, PH 6.5-7.5 in temperature, and mixing speed is 10-20 revs/min, plating Liquid useful load is 0.8-1.5dm2In the case of/L, the time of selfdecomposition failure does not occur.
The technique effect of embodiment 1-5 is as shown in table 1:
Table 1:
Hardness (HV) Friction coefficient Phosphorus content (%) Bath life (h)
Embodiment 1 842 0.69 3.34 1.5
Embodiment 2 890 0.68 3.33 1.5
Embodiment 3 860 0.70 3.33 1.4
Embodiment 4 630 0.54 5.4 0.5
Embodiment 5 620 0.57 5.5 0.3

Claims (3)

1. the preparation method of aero titanium alloy, includes the following steps:
A, the cleaning step of titanium alloy;B, the electroless plating step of titanium alloy, it is characterised in that:
The chemical plating is Ni-P-Si-C composite electroless-platings, i.e., cleaned titanium alloy is put into composite plating bath and changed Plating is learned, the condition of chemical plating is:Plating temperature is 80-90 DEG C, PH 6.5-7.5, and mixing speed is 10-20 revs/min, plating solution dress Carrying capacity is 0.8-1.5dm2/ L, plating time 0.5-1 hours;
In the composite plating bath, following substance is contained in every liter of solution:
2. the preparation method of aero titanium alloy according to claim 1, it is characterised in that:
The cleaning step of the titanium alloy includes the following steps successively:Sand paper polishing step, deoiling step, acid pickling step, work Change step.
3. the preparation method of aero titanium alloy according to claim 2, it is characterised in that:
The deoiling step is the titanium alloy polished with ultrasonic cleaning sand paper, and ultrasonic frequency 50-70KHz is cleaned 10-30 minutes.
CN201610837724.0A 2016-09-21 2016-09-21 The preparation method of aero titanium alloy Active CN106435543B (en)

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CN201610837724.0A CN106435543B (en) 2016-09-21 2016-09-21 The preparation method of aero titanium alloy

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CN106435543B true CN106435543B (en) 2018-07-06

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2845922A1 (en) * 2013-09-04 2015-03-11 Rohm and Haas Electronic Materials LLC Electroless metallization of dielectrics with alkaline stable pyrimidine derivative containing catalysts

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