CN1386917A - Micro-are Ti alloy oxidizing technology - Google Patents

Micro-are Ti alloy oxidizing technology Download PDF

Info

Publication number
CN1386917A
CN1386917A CN 01113982 CN01113982A CN1386917A CN 1386917 A CN1386917 A CN 1386917A CN 01113982 CN01113982 CN 01113982 CN 01113982 A CN01113982 A CN 01113982A CN 1386917 A CN1386917 A CN 1386917A
Authority
CN
China
Prior art keywords
titanium alloy
anodic oxidation
micro
arc
film
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
Application number
CN 01113982
Other languages
Chinese (zh)
Other versions
CN1137291C (en
Inventor
周英杰
王伟
王学连
王少刚
王向荣
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.)
Shenyang Liming Aero Engine Group Co Ltd
Original Assignee
Shenyang Liming Aero Engine Group 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 Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CNB01113982XA priority Critical patent/CN1137291C/en
Publication of CN1386917A publication Critical patent/CN1386917A/en
Application granted granted Critical
Publication of CN1137291C publication Critical patent/CN1137291C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

A micro-arc oxidizing process for preparing oxidized film on the surface of Ti alloy includes putting workpiece as anode in the acidic liquid prepared from sulfuric acid, regulating pulse width and tracking frequency of pulse power supply at low temp, and raising voltage to 120 V to generate 2-12 microns oxided film. Said film has features of high hardness (700 HV), high resistivity (5X10 to the power 6 ohms) and high antisticking and antiwear performance.

Description

A kind of micro-are Ti alloy oxidizing technology
The invention belongs to the titanium alloy surface treatment technology, be specifically related to titanium alloy component, particularly titanium alloy fastener surface electrochemistry conversion film processing method.
As everyone knows, the specific tenacity height of titanium alloy, proportion are little, good heat resistance, and corrosion stability is good, has been widely used in space flight, aviation, shipbuilding and chemical industry.But because titanium alloy is the alloy that is formed by the titanium more than 90%, its electropotential is negative (1.75V), with aluminium, magnesium alloy parts, when zinc-plated, as to plate Cadmium steel part and other metal or coating contact, can produce transfer transport, electrochemistry crevice corrosion take place easily cause bonding; In addition, titanium alloy hardness ratio higher temperatures alloy, stainless steel etc. are much lower again, and wear resistance is relatively poor.These characteristics have all limited the use range of titanium alloy.Aircraft industry press 1993 publish " aviation manufacturing engineering handbook (surface treatment fascicle) mentions that the conversion film on titanium or titanium alloy surface handles, and points out that this conversion film can be used for the anti-viscous of threaded fastener, wear-resisting, the anti-scratch that is used to be rotatably assorted is surperficial.But titanium alloy is the film forming difficulty under common voltage, and requirement will make titanium alloy be in the plasma arc state of oxidation under the condition of continuous boosted voltage, and oxide film is thickened.And this handbook there is no concrete scheme.The 3rd phase " material protection " that material protection periodical publisher published in 1988 is published the article of " differential arc oxidation and the material surface potteryization " of writing in Liu Feng mountain range, one piece of Beijing Research Inst. of Aeronautic Material, has mainly introduced aluminium alloy plasma micro-arc ceramic technology.Just in foreword, mention metal and the alloy thereof that contains titanium, also do not have the particular content of titanium alloy differential arc oxidation in its text.
The object of the present invention is to provide a kind of titanium alloy component, especially titanium alloy fastener utilizes the pulse differential arc oxidation to make the surface form the processing method of high rigidity, high resistance protective film.
Technical solution of the present invention is as follows: in the technical process that comprises visual inspection, oil removing, clamping, washing, anodic oxidation, washes, dries up, checks, in the anodic oxidation operation, place the acid tank liquor of mainly forming to do anode part by sulfuric acid, adopt the direct current pulse power source intermittent power supply, at low temperatures by regulating impulse time and tracking frequency, progressively boost to and be higher than behind the 120v film forming under the plasma micro-arc state.Wherein, can contain a spot of phosphoric acid in the tank liquor, its prescription is H 2SO 4(ρ=1.84) 50~250ml/l; H 3PO 4(ρ=1.7) 0~20ml/l; The temperature of tank liquor belongs to low temperature for≤30 ℃, generally is taken as-10~30 ℃.The pulse current density that is adopted is 1-12A/dm 2Pulse duration is 0.02-0.8S; Tracking frequency is 0.25-2.95HZ; Be 10-50min pressure rising time.Certainly, in the above-mentioned flow process, oil removing process is that common process both can comprise electrochemical deoiling, also can comprise Solvent degreasing.And the voltage of anodic oxidation when finishing then depends on the requirement of drawing to the part thickness, is generally 120-300V.In addition, the pulsed current ripple of employing both can be zigzag wave, sine wave, can be again rectangular wave.
See embodiment below in conjunction with accompanying drawing.
Accompanying drawing 1 is a process method flow chart.
Accompanying drawing 2 is the oxide film microscopic appearance figure of compact structure.
Accompanying drawing 3 is another oxide film microscopic appearance figure.
Embodiment one, is T to certain engine material trade mark at first C6, BT20 nut, nut, screws etc. have blind hole, 840 of the parts of screw thread and groove carry out visual inspection, dip in acetone wiping gently with absorbent cotton, and in carry out electrochemical deoiling behind the clamping in the electrochemical deoiling tank liquor.At this moment, as follows except that oil formula:
NaoH 30-70?g/L
Na 2CO 3·10H 2O 20-25g/L
Na 3Po 4 5-15g/L
Na 3sio 4 3-5g/L
Temperature 40-80 ℃
Part after the oil removing is through washing laggard horizontal pulse anodic oxidation.At this moment, the part that is contained on the titanium alloy anchor clamps will closely contact with anchor clamps, guarantees not to be shifted when trembling.The prescription and the oxidizing process of this oxidation tank liquor are as follows:
H 2SO 4 (p=1.84)?180-220ml/L
H 3PO 4 (P=1.7) 5-15ml/L
Tank liquor temperature 0-30 ℃
Current density 1-6A/dm 2
Time length 0.3-0.8S
Tracking frequency 1.20-0.25HZ
In the process of boosting, the surface to be machined of part all differential of the arc phenomenon can occur.After the process of boosting continues for some time, keep final magnitude of voltage to specific time.Because present embodiment will be made anti-bonding conversion film, so get 10-20min pressure rising time, termination voltage is got 120-150V.Oxidation is closed pulse after finishing, step-down then, and part is taken out in outage, carries out follow-up washing, dries up and inspection process.Final pieces O.K. records through scanning electron microscope, and the oxide thickness of compact structure is 2-3 μ m, sees shown in the accompanying drawing 2.Adopt microhardness tester, by calculating as can be known, this oxide film hardness is a little more than matrix hardness, and this is to be subjected to owing to film is extremely thin due to the matrix support influences.In anti-bonding simultaneous test, adopt the part rete of this art breading complete, piece surface is such as the smooth no bonding phenomenon in screw thread place, and the nut of oxide skin does not then come in contact corrosion already, even the rotation difficulty.840 of this batches, by the technical process passed examination, through installation by 300 hours endurance tests of engine and be delivered for use.
Embodiment two, certain engine pressing plate, pad, pin, a wall, ear muff etc., material mark T C4, T C11Amount to 1500.In the implementing process flow process, check part, oil removing, operations such as washing are with embodiment one, and just in the anodic oxidation operation, its tank liquor prescription and oxidizing process are as follows:
H 2SO 4 (p=1.84) 50-250ml/L
H 3PO 4 (P=1.7) 0-20ml/L
Tank liquor temperature-10-10 ℃
Current density 2-12A/dm 2
Time length 0.02-0.4S
Tracking frequency 2.95-0.8HZ
The purpose of present embodiment is to make attrition resistant conversion film, so get 20-50min pressure rising time, termination voltage is got 140-300V.Operation after the anodic oxidation is also with embodiment one.Final pieces O.K. detects through eddy current thickness meter, and oxide thickness is 5-12 μ m.The same microhardness tester that adopt calculate by test, and its oxide film hardness reaches 600-700HV.Use scanning electron microscopic observation, this oxide film microcosmic fenestra is very abundant, is suitable for retaining solid lubricant, sees accompanying drawing 3.Also be delivered for use after 1500 of this batches are qualified on inspection.
The invention has the advantages that the pulse power supply mode that adopts, overcome the key of titanium alloy film forming difficulty, realized that especially the titanium alloy fastener surface forms high rigidity (can reach 700HV) to titanium alloy, high resistance (can reach 5 * 106Ω) The purpose of protecting film. Owing to utilize at low temperatures pulse current intermittent power supply liter Press therefore relatively direct current method anodic oxidation, its oxide-film hardness height, wearability Want to do well, and be conducive to the melting of rete---solidify, make rete smooth, no Reduce Endurance limits of material. In a word, the present invention makes titanium alloy surface form one The protecting film of layer 2-12 μ m has hindered the electronics transmission, has suppressed electrochemistry The generation of reaction reached anti-bonding purpose, also improved material simultaneously Anti-wear performance can improve part service life more than 3 times. Because the present invention Realization, greatly expanded titanium alloy particularly titanium alloy fastener, contact And the range of application of sleeve member. Aircraft engine, marine engine, automobile is sent out Motivation, the high temperature alloy on aerospace craft and some civilian goods, stainless steel part, Under the condition that operating temperature allows, can get with titanium alloy anode oxidation spare Generation, thereby the weight of mitigation system greatly. The boat of extremely valuing for thrust-weight ratio Empty space industry, prospect is especially wide.

Claims (3)

1, a kind of titanium alloy micro-arc anodic oxidation method, comprise: oil removing, clamping, anodic oxidation and washing is characterized in that: in anodic oxidation, part is placed mainly in the acid tank liquor of being made up of sulfuric acid, at low temperatures, adopt direct current pulse power source,, progressively boost to and be higher than behind the 120V film forming under the plasma micro-arc state by regulating impulse time and tracking frequency.
2, titanium alloy micro-arc anodic oxidation method according to claim 1 is characterized in that the prescription of acid tank liquor and temperature are as follows:
H 2SO 4(p=1.84) 50-250ml/L
H 3PO 4(P=1.7) 0-20ml/L
Tank liquor temperature-10-30 ℃
3, titanium alloy micro-arc anodic oxidation method according to claim 1 and 2, it is characterized in that: the pulse power supply parameter is as follows:
Current density 1-12A/dm 2
Time length 0.02-0.8S
Tracking frequency 0.25-2.95HZ
Pressure rising time 10-50min
Termination voltage 120-300V
CNB01113982XA 2001-05-22 2001-05-22 Micro-are Ti alloy oxidizing technology Expired - Fee Related CN1137291C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNB01113982XA CN1137291C (en) 2001-05-22 2001-05-22 Micro-are Ti alloy oxidizing technology

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB01113982XA CN1137291C (en) 2001-05-22 2001-05-22 Micro-are Ti alloy oxidizing technology

Publications (2)

Publication Number Publication Date
CN1386917A true CN1386917A (en) 2002-12-25
CN1137291C CN1137291C (en) 2004-02-04

Family

ID=4660676

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB01113982XA Expired - Fee Related CN1137291C (en) 2001-05-22 2001-05-22 Micro-are Ti alloy oxidizing technology

Country Status (1)

Country Link
CN (1) CN1137291C (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100346845C (en) * 2004-01-16 2007-11-07 清华大学 Metal surface constructional gradient biological layer and its preparation and usage
CN100390320C (en) * 2004-06-23 2008-05-28 中国科学院金属研究所 Surface treatment for implant material of titanium or titanium alloy from electrochemical method
CN101812715A (en) * 2010-03-24 2010-08-25 西安北方光电有限公司 Titanium alloy black anode oxidation process
CN102425000A (en) * 2011-11-29 2012-04-25 哈尔滨工业大学 Method for preparing biologically active titanium dioxide film on NiTi alloy surface
CN104195616A (en) * 2014-09-04 2014-12-10 攀钢集团成都钢钒有限公司 Micro-arc oxidation treatment method of titanium alloy tubing coupling surface
CN106637349A (en) * 2016-11-08 2017-05-10 北京星航机电装备有限公司 Treatment method before coating of titanium alloy surface coating
CN108103552A (en) * 2017-11-28 2018-06-01 中国航发西安动力控制科技有限公司 For the technique of TA2 titanium alloy material thick film anodes
CN109594080A (en) * 2017-09-30 2019-04-09 宝鸡市金海源钛标准件制品有限公司 A kind of surface treatment method of titanium alloy
CN110863227A (en) * 2019-11-07 2020-03-06 西安工业大学 Titanium alloy pulse-direct current anodic oxidation surface treatment method
CN113061895A (en) * 2021-03-04 2021-07-02 中国兵器科学研究院宁波分院 Micro-arc oxidation treatment method for surface of titanium alloy fastener
CN115044859A (en) * 2022-06-17 2022-09-13 中国船舶重工集团公司第七二五研究所 Titanium alloy material surface treatment method

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100454742C (en) * 2004-09-21 2009-01-21 沈阳黎明航空发动机(集团)有限责任公司 Large capacity titanium alloy pulse micro arc anode oxidation dynamic control power source
CN1974876B (en) * 2006-11-02 2010-07-07 华南理工大学 Bioactive film on titanium metal surface and its sand blasting-micro arc oxidizing compounding process

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100346845C (en) * 2004-01-16 2007-11-07 清华大学 Metal surface constructional gradient biological layer and its preparation and usage
CN100390320C (en) * 2004-06-23 2008-05-28 中国科学院金属研究所 Surface treatment for implant material of titanium or titanium alloy from electrochemical method
CN101812715A (en) * 2010-03-24 2010-08-25 西安北方光电有限公司 Titanium alloy black anode oxidation process
CN101812715B (en) * 2010-03-24 2011-12-07 西安北方光电有限公司 Titanium alloy black anode oxidation process
CN102425000A (en) * 2011-11-29 2012-04-25 哈尔滨工业大学 Method for preparing biologically active titanium dioxide film on NiTi alloy surface
CN104195616A (en) * 2014-09-04 2014-12-10 攀钢集团成都钢钒有限公司 Micro-arc oxidation treatment method of titanium alloy tubing coupling surface
CN106637349A (en) * 2016-11-08 2017-05-10 北京星航机电装备有限公司 Treatment method before coating of titanium alloy surface coating
CN109594080A (en) * 2017-09-30 2019-04-09 宝鸡市金海源钛标准件制品有限公司 A kind of surface treatment method of titanium alloy
CN108103552A (en) * 2017-11-28 2018-06-01 中国航发西安动力控制科技有限公司 For the technique of TA2 titanium alloy material thick film anodes
CN110863227A (en) * 2019-11-07 2020-03-06 西安工业大学 Titanium alloy pulse-direct current anodic oxidation surface treatment method
CN113061895A (en) * 2021-03-04 2021-07-02 中国兵器科学研究院宁波分院 Micro-arc oxidation treatment method for surface of titanium alloy fastener
CN113061895B (en) * 2021-03-04 2023-04-28 中国兵器科学研究院宁波分院 Micro-arc oxidation treatment method for surface of titanium alloy fastener
CN115044859A (en) * 2022-06-17 2022-09-13 中国船舶重工集团公司第七二五研究所 Titanium alloy material surface treatment method

Also Published As

Publication number Publication date
CN1137291C (en) 2004-02-04

Similar Documents

Publication Publication Date Title
CN1137291C (en) Micro-are Ti alloy oxidizing technology
Zhang et al. Wear and corrosion resistance of cold-sprayed Cu-based composite coatings on magnesium substrate
CN100450769C (en) Composite article comprising a ceramic coating
Ivanou et al. Plasma anodized ZE41 magnesium alloy sealed with hybrid epoxy-silane coating
Chen et al. Corrosion resistance of T-ZnOw/PDMS-MAO composite coating on the sintered NdFeB magnet
CN114318465B (en) Micro-arc oxidation preparation method for 7-series aluminum alloy black surface
Singh et al. Establishing environment friendly surface treatment for AZ91 magnesium alloy for subsequent electroless nickel plating
Liang et al. Galvanic corrosion behavior of AZ31 Mg alloy coupled with mild steel: Effect of coatings
Wang et al. Effect of cerium on the microstructure and anti-corrosion performance of Al-Zn coatings
Baiocco et al. Sustainable coating solutions: a comparative life cycle analysis of electrophoretic deposition and electroplating for graphene-reinforced anti-wear coatings
Qiao et al. Corrosion behavior and microstructure of 2024 aluminum alloy sheets by shot peen forming in a salt spray environment
Chen et al. Effects of tartaric acid on the structure and corrosion resistance for anodizing films of aerospace aluminium alloys
Hao et al. The effects of P and metal elements in electroless nickel-based alloys on the formation of Ti/Zr conversion coating
Xia et al. Effect of Cu2+ on the corrosion behavior and mechanism of Al-2% Zn coatings in 3.5% NaCl solution
Wang et al. Effect of cerium nitrate and salicylic acid on the titanium–zirconium chemical conversion coating of 6061 aluminum alloy
DeForce et al. Application of aluminum coatings for the corrosion protection of magnesium by cold spray
Abdivakhidov Application and removing protective metal coatings
Zhichun et al. Effects of addition of polyvinyl pyrrolidone (PVP) as a corrosion inhibitor to Zr/V-based conversion coating on aluminum alloy
CN101418460B (en) Method for preparing composite coating by surface differential arc oxidation/chemical conversion of Mg-Li alloy
Godja et al. Plasma electrolytic oxidation treatments for bimetallic substrates enabling sustainable procedures for automotive painting
Uma Rani et al. Comparison of corrosion performance of various conversion coatings on magnesium alloy using electrochemical techniques
Yang et al. Study on diffusion of NaOH solution in zinc-rich epoxy coating using EIS
Ahmadia et al. NASF/AESF University Funded Research Transitioned to Industry: Practical Performance Improvements in Functional REACH-Compliant Trivalent Chromium Plating
Baiocco et al. Investigating tribological properties of electrophoretically deposited graphene nanoplatelets coatings on mild steel
Palraj et al. Effect of pretreatments on electrodeposited epoxy coatings for electronic industries.

Legal Events

Date Code Title Description
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20040204

Termination date: 20130522