CN102069295A - Method for preparing Fe3Al/Al composite structure by diffusion bonding of reinforcing layer - Google Patents

Method for preparing Fe3Al/Al composite structure by diffusion bonding of reinforcing layer Download PDF

Info

Publication number
CN102069295A
CN102069295A CN 201010580640 CN201010580640A CN102069295A CN 102069295 A CN102069295 A CN 102069295A CN 201010580640 CN201010580640 CN 201010580640 CN 201010580640 A CN201010580640 A CN 201010580640A CN 102069295 A CN102069295 A CN 102069295A
Authority
CN
China
Prior art keywords
alloy
strengthening layer
composite construction
diffusion
preparation
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 201010580640
Other languages
Chinese (zh)
Other versions
CN102069295B (en
Inventor
任江伟
徐培全
韦媛
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.)
Shanghai University of Engineering Science
Original Assignee
Shanghai University of Engineering Science
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 Shanghai University of Engineering Science filed Critical Shanghai University of Engineering Science
Priority to CN 201010580640 priority Critical patent/CN102069295B/en
Publication of CN102069295A publication Critical patent/CN102069295A/en
Application granted granted Critical
Publication of CN102069295B publication Critical patent/CN102069295B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The invention discloses a method for preparing a Fe3Al/Al composite structure by diffusion bonding of a reinforcing layer. The method comprises the following steps of: preparing the reinforcing layer consisting of superfine crystal or nano crystal on an alloy surface by shot blasting or grinding with a surface machine, then performing diffusion bonding by using the reinforcing layer as a middle layer to obtain the Fe3Al/Al composite structure, and forming a transition layer with thickness of about 10 to 30 microns on the interface between the Fe3Al alloy and the Al alloy, wherein cracks are not formed at the joint. The method has simple operation, short treatment time, low equipment investment and low requirement for surface pretreatment of materials.

Description

The strengthening layer diffusion connects preparation Fe 3The method of Al/Al composite construction
Technical field
The present invention relates to the metal material processing field, be specially the solder technology of non-ferrous metal, the especially diffusion method of attachment between non-ferrous metal specifically is that the strengthening layer diffusion connects preparation Fe 3The method of Al/Al composite construction.
Background technology
Structural material is the important foundation in modern industry field, and its performance has determined the level of industrial equipment.Novel colored metal material is an important class material.Aluminium alloy is the non-ferrous metal that present industrial circle extensively adopts, and has characteristics such as low-density, high specific strength, easy processing.Fe 3Al is a kind of novel non-ferrous metal, has higher specific strength, good wearability and characteristic such as corrosion-resistant, is the material that fields such as Aero-Space, automobile, chemical industry have potentiality.With Fe 3Al and Al alloy couple together, and can make full use of Fe 3The good plasticity of the high strength of Al, wearability and Al alloy obtains the Fe of excellent combination property 3The Al/Al composite construction.In addition, Fe 3Al alloy and Al alloy all have decay resistance preferably, so Fe 3The reliability that the Al/Al composite construction is on active service under corrosive environment is also better.
Present Fe 3The method of attachment that Al is commonly used mainly is SMAW, argon tungsten-arc welding, electron beam welding and diffusion welding (DW).Adopt TIG weldering and electron beam welding welding Fe 3During Al, be easy to generate fire check.For fear of producing fire check, should control elements such as B, Zr in the wlding, Mo, and increase carbide formers such as Cr, Nb, C.But elements such as B, Zr, Mo are Fe 3The Strengthening and Toughening element that the Al alloy is commonly used.Adopt SMAW and argon tungsten-arc welding welding Fe 3The cold crack problem appears during Al easily.Airborne steam at high temperature decomposites atomic hydrogen, can be directly and the reaction of the Al in the molten bath generate atomic hydrogen, be Fe 3Produce one of principal element of cold crack during the weldering of Al alloy melting.Fe 3The thermal conductivity of Al alloy is little, thermal coefficient of expansion is big, forms bigger residual stress in joint area easily in the melting process, helps diffusion, the gathering of hydrogen.Therefore, at Fe 3What Al alloy and foreign material (as Q235, Cr18-Ni8 etc.) mainly adopted when being connected is diffusion welding (DW).The subject matter that exists during diffusion welding (DW) is the boundary zone that is difficult to obtain the heterogeneous microstructure even transition, often occurs high rigidity fragility phase easily in the boundary zone, causes the mechanical property of connector area to worsen.At present also not with Fe 3The Al alloy is connected preparation Fe with the Al alloy 3The report of Al/Al composite construction.
Fe 3Have significant difference between the physicochemical properties of Al and Al alloy, this makes Fe3Al and Al alloy be easy to generate stress in the diffusion welding (DW) process, makes to form crackle at the interface.For this reason, must adopt certain technological measure to strengthen the Diffusion Welding of Fe3Al and Al alloy.
Through the literature search of prior art being found two patents of invention of applications such as Zhou Yuan: the mode that " a kind of method of diffusion connecting titanium alloy at low temperature and vacuum (application number 200810172468.3) " and " a kind of is that the method (application number 200810172471.5) that the diffusion of high temperature alloy vacuum is connected is carried out in the intermediate layer with the film " proposition prepares film at surface of the work employing magnetically controlled sputter method is improved the Diffusion Welding of titanium alloy or high temperature alloy.The method of employing magnetron sputtering prepares film and has following deficiency: at first be to sputter the restriction that film size is subjected to the magnetic control target area; Next is the magnetron sputtering process more complicated; The equipment price that is magnetron sputtering at last is higher.
Summary of the invention
The present invention aims to provide a kind of strengthening layer diffusion connection Fe that utilizes 3Al alloy and Al alloy, preparation Fe 3The method of Al/Al composite construction.
The present invention is directed to and strengthen Fe 3The Diffusion Welding of Al alloy and Al alloy has proposed a kind of mode that adopts surface plastic deformation, prepares strengthening layer with shot-peening or surface mechanical attrition at alloy surface, spreads connection with strengthening layer as the intermediate layer then, obtains Fe 3The Al/Al composite construction.
This strengthening layer diffusion connects preparation Fe 3The method of Al/Al composite construction may further comprise the steps:
(1) to Fe 3Al or Al alloy carry out surface plastic deformation, in surface preparation by ultra-fine crystalline substance or the nanocrystalline strengthening layer that constitutes;
Strengthening layer thickness 10~30um, nanocrystalline particle diameter 20~50nm; Particle diameter 100~the 120nm of ultra-fine crystalline substance.
At Fe 3The mode that Al or Al alloy surface prepare strengthening layer is shot-peening or surface mechanical attrition, adopts steel ball shot-peening 5~20min of diameter 2~8mm, perhaps steel ball surface mechanical lapping 5~20min of diameter 2~8mm.
To not passing through the Al alloy or the Fe of surface plastic deformation 3Mechanical chipping and Chemical cleaning and dry are carried out in the surface of Al alloy; After available sand paper is polished step by step, dry up after can cleaning with alcohols (as ethanol) or acetone again;
Used Fe 3In the Al alloy, the atomic percent of Fe is 65~75%, and the atomic percent of Al is 22~28%;
The percentage by weight of Al is 99.0~99.9% in the Al alloy;
(2) with Fe 3Al alloy and Al alloy workpiece compress with pressure head,, are placed on and spread connection in the vacuum chamber as the intermediate layer with strengthening layer, and the diffusion welding craft parameter of employing is: 500~640 ℃ are incubated 30~90min, Fe down 3Al alloy and Al alloy pressure 15~20MPa, vacuum is 10 -2Pa~10 -3Pa;
Distribute in order to obtain even temperature in the heating process, adopt heat temperature raising speed and the step mode of heating of 5~10 ℃/min, promptly be incubated 8~15min down at 195~205 ℃ and 395~405 ℃ respectively;
After reaching temperature retention time, workpiece is taken out after vacuum chamber is cooled to 80~110 ℃, obtain Fe 3The Al/Al composite construction.
Fe 3The transition zone that forms the about 10-30 μ of thickness m at the interface between Al alloy and the Al alloy, joint do not have crackle to form.
Characteristics of the present invention are to adopt the mode of shot-peening or surface mechanical attrition at Fe 3Al or Al alloy surface prepare strengthening layer by plastic deformation, and the binding ability of strengthening layer and matrix is good.As the intermediate layer of strengthening diffusion, strengthen Fe with strengthening layer 3Al/Al dissimilar metal Diffusion Welding, needed pressure in the time of can reducing diffusion welding (DW) shortens the Diffusion Welding capitiform and becomes the needed time.By the rapid diffusion passage of nanocrystalline in the strengthening layer or ultra-fine crystalline substance, can accelerate the diffusion of atom, realize Fe 3The Al alloy welds the formation mutually of regulating joint median surface transition region with the rapid diffusion of Al alloy.In addition, this method is simple to operate, and the processing time is short, and equipment investment is little, and surface treatment in earlier stage requires lower to material.
The specific embodiment
Embodiment 1
(1) Fe 3The preliminary treatment of Al alloy and Al alloy:
Get the Fe that chemical composition is 73Fe-25Al-2Cr at.% 3The Al alloy, surface plastic deformation is directly carried out without mechanical chipping in the surface, and with diameter 2~8mm steel ball, surface mechanical attrition 15min can be at Fe 3The Al alloy surface prepares the strengthening layer of thickness 10~30 μ m, and the crystal grain on strengthening layer top layer is the nanocrystalline of particle diameter 20~50nm.
The surface of 1060Al alloy (Al 99.6wt%) adopts 200Cw, 400Cw and 600Cw waterproof abrasive paper to polish step by step.Again with Fe 3Al alloy and Al alloy surface use ethanol (or acetone) to carry out drying up after the Chemical cleaning respectively.
(2) with Fe 3Al alloy and Al alloy workpiece compress with pressure head, and strengthening layer is positioned at Fe as the intermediate layer 3Between Al alloy and the Al alloy workpiece, be placed on and carry out diffusion welding (DW) in the vacuum chamber.
The diffusion welding craft parameter that adopts is: 550 ℃ are incubated 90min, Fe down 3Al alloy and Al alloy pressure are 19MPa, vacuum 10 -2Pa~10 -3Pa.10 ℃/the min of programming rate of heating is incubated 10min at 200 ℃ and 400 ℃ respectively in the heating process.
After reaching temperature retention time, by water circulation cooling, when vacuum chamber is cooled to 100 ℃, with Fe 3Al/Al composite construction joint takes out.
With ESEM to Fe 3The observation of Al/Al joint shows, has formed the transition zone of thickness 11-30 μ m, transition zone and Fe 3The matrix bond of Al and Al alloy is good, and the joint does not have crackle to form.
Embodiment 2
(1) gets the Fe that chemical composition is 73Fe-25Al-2Cr at.% 3The Al alloy, surface plastic deformation is directly carried out without mechanical chipping in the surface, with diameter 2~8mm steel ball shot-peening 5min, can be at Fe 3The Al alloy surface obtains the strengthening layer of thickness 10~30 μ m, and the strengthening layer top layer is local for particle diameter is the ultra-fine crystalline substance of 100~120nm, and remainder is the nanocrystalline of particle diameter 20~50nm.
The surface of 1060Al alloy (Al 99.6wt%) adopts 200Cw, 400Cw and 600Cw waterproof abrasive paper to polish step by step.Again with Fe 3Al alloy and Al alloy surface use ethanol (or acetone) to carry out drying up after the Chemical cleaning respectively.
(2) Fe3Al alloy and Al alloy workpiece are compressed with pressure head, strengthening layer, is placed on and carries out diffusion welding (DW) in the vacuum chamber between Fe3Al alloy and Al alloy workpiece as the intermediate layer.
The diffusion welding craft parameter that adopts is: 640 ℃ are incubated 30min, Fe down 3Al alloy and Al alloy pressure are 19MPa, vacuum 10 -2Pa~10 -3Pa.5 ℃/the min of programming rate of heating is incubated 10min at 200 ℃ and 400 ℃ respectively in the heating process.
After reaching temperature retention time, by water circulation cooling, when vacuum chamber is cooled to 100 ℃, with Fe 3Al/Al composite construction joint takes out.
With ESEM to Fe 3The observation of Al/Al joint shows, has formed the transition zone of thickness 11-22 μ m, transition zone and Fe 3The matrix bond of Al and Al alloy is good, and the joint does not have crackle to form.

Claims (9)

1. the strengthening layer diffusion connects preparation Fe 3The method of Al/Al composite construction is characterized in that, may further comprise the steps:
(1) to Fe 3Al or Al alloy carry out surface plastic deformation, in surface preparation by ultra-fine crystalline substance or the nanocrystalline strengthening layer that constitutes;
To not passing through the Al alloy or the Fe of surface plastic deformation 3Mechanical chipping and Chemical cleaning and dry are carried out in the surface of Al alloy; After polishing step by step with sand paper, dry up after using alcohols (as ethanol) or acetone to clean again;
(2) with Fe 3Al alloy and Al alloy workpiece compress with pressure head,, are placed on and spread connection in the vacuum chamber as the intermediate layer with strengthening layer, and the diffusion welding craft parameter of employing is: 500~640 ℃ are incubated 30~90min, Fe down 3Al alloy and Al alloy pressure 15~20MPa, vacuum is 10 -2Pa~10 -3Pa;
(3) reach temperature retention time after, workpiece is taken out after vacuum chamber is cooled to 80~110 ℃, obtain Fe 3The Al/Al composite construction.
2. the described strengthening layer diffusion of claim 1 connects preparation Fe 3The method of Al/Al composite construction is characterized in that, the strengthening layer thickness 10~30um described in the step (1), and nanocrystalline particle diameter is 20~50nm; Ultra-fine grain directly is 100~120nm.
3. the described strengthening layer diffusion of claim 1 connects preparation Fe 3The method of Al/Al composite construction is characterized in that, described in the step (1) at Fe 3The mode that Al or Al alloy surface prepare strengthening layer is shot-peening or surface mechanical attrition.
4. the described strengthening layer diffusion of claim 3 connects preparation Fe 3The method of Al/Al composite construction is characterized in that, adopts steel ball shot-peening 5~20min of diameter 2~8mm.
5. the described strengthening layer diffusion of claim 3 connects preparation Fe 3The method of Al/Al composite construction is characterized in that, adopts steel ball surface mechanical lapping 5~20min of diameter 2~8mm.
6. the described strengthening layer diffusion of claim 1 connects preparation Fe 3The method of Al/Al composite construction is characterized in that, the described mechanical chipping of step (1) is for to polish step by step with sand paper, and the solvent that described Chemical cleaning is used is alcohols or acetone.
7. the described strengthening layer diffusion of claim 1 connects preparation Fe 3The method of Al/Al composite construction is characterized in that, described Fe 3In the Al alloy, the atomic percent of Fe is 65~75%, and the atomic percent of Al is 22~28%.
8. the described strengthening layer diffusion of claim 1 connects preparation Fe 3The method of Al/Al composite construction is characterized in that, the percentage by weight of Al is 99.0~99.9% in the described Al alloy.
9. the described strengthening layer diffusion of claim 1 connects preparation Fe 3The method of Al/Al composite construction is characterized in that, the described heat temperature raising speed of step (2) is 5~10 ℃/min, and is incubated 8~15min down at 95~205 ℃ and 395~405 ℃ respectively.
CN 201010580640 2010-12-09 2010-12-09 Method for preparing Fe3Al/Al composite structure by diffusion bonding of reinforcing layer Expired - Fee Related CN102069295B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201010580640 CN102069295B (en) 2010-12-09 2010-12-09 Method for preparing Fe3Al/Al composite structure by diffusion bonding of reinforcing layer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201010580640 CN102069295B (en) 2010-12-09 2010-12-09 Method for preparing Fe3Al/Al composite structure by diffusion bonding of reinforcing layer

Publications (2)

Publication Number Publication Date
CN102069295A true CN102069295A (en) 2011-05-25
CN102069295B CN102069295B (en) 2012-12-12

Family

ID=44028169

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201010580640 Expired - Fee Related CN102069295B (en) 2010-12-09 2010-12-09 Method for preparing Fe3Al/Al composite structure by diffusion bonding of reinforcing layer

Country Status (1)

Country Link
CN (1) CN102069295B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107775168A (en) * 2017-09-20 2018-03-09 西安理工大学 A kind of connection method of chromiumcopper and stainless steel
CN109604802A (en) * 2019-01-03 2019-04-12 中国兵器工业第五九研究所 The connection method of tungsten or tungsten alloy and steel, the connection method of profile and sectional material joint
CN112626378A (en) * 2020-11-30 2021-04-09 湖南金天铝业高科技股份有限公司 Iron-aluminum alloy composite reinforced aluminum-based material, and preparation method and application thereof
CN112719569A (en) * 2020-12-31 2021-04-30 昆山哈工万洲焊接研究院有限公司 Method for preparing dissimilar metal composite structure by strong deformation and strong pressure assisted cold welding

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1251329A (en) * 1999-05-20 2000-04-26 北京科技大学 Method welding ferro-trialuminous group metallic meta-compound
US20040050913A1 (en) * 2002-01-24 2004-03-18 Siemens Westinghouse Power Corporation High strength diffusion brazing utilizing nano-powders
CN1559740A (en) * 2004-02-25 2005-01-05 山东大学 Diffusion welding technology of activity increasing intermediate layer of iron trialuminium alloy and steel
US20050230042A1 (en) * 2004-01-05 2005-10-20 Nobuaki Hashimoto Bonding structure and method for bonding members
WO2008009670A1 (en) * 2006-07-20 2008-01-24 Technische Universität Ilmenau Method for the creation of a soldered joint or a diffusion seal
CN101244483A (en) * 2008-03-20 2008-08-20 重庆大学 Self-nano-structure diffusion welding technique for titanium alloy and stainless steel surface
US20090224027A1 (en) * 2008-03-10 2009-09-10 Turbine Overhaul Services Pte Ltd Method for diffusion bonding metallic components with nanoparticle foil

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1251329A (en) * 1999-05-20 2000-04-26 北京科技大学 Method welding ferro-trialuminous group metallic meta-compound
US20040050913A1 (en) * 2002-01-24 2004-03-18 Siemens Westinghouse Power Corporation High strength diffusion brazing utilizing nano-powders
US20050230042A1 (en) * 2004-01-05 2005-10-20 Nobuaki Hashimoto Bonding structure and method for bonding members
CN1559740A (en) * 2004-02-25 2005-01-05 山东大学 Diffusion welding technology of activity increasing intermediate layer of iron trialuminium alloy and steel
WO2008009670A1 (en) * 2006-07-20 2008-01-24 Technische Universität Ilmenau Method for the creation of a soldered joint or a diffusion seal
US20090224027A1 (en) * 2008-03-10 2009-09-10 Turbine Overhaul Services Pte Ltd Method for diffusion bonding metallic components with nanoparticle foil
CN101244483A (en) * 2008-03-20 2008-08-20 重庆大学 Self-nano-structure diffusion welding technique for titanium alloy and stainless steel surface

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107775168A (en) * 2017-09-20 2018-03-09 西安理工大学 A kind of connection method of chromiumcopper and stainless steel
CN109604802A (en) * 2019-01-03 2019-04-12 中国兵器工业第五九研究所 The connection method of tungsten or tungsten alloy and steel, the connection method of profile and sectional material joint
CN112626378A (en) * 2020-11-30 2021-04-09 湖南金天铝业高科技股份有限公司 Iron-aluminum alloy composite reinforced aluminum-based material, and preparation method and application thereof
CN112719569A (en) * 2020-12-31 2021-04-30 昆山哈工万洲焊接研究院有限公司 Method for preparing dissimilar metal composite structure by strong deformation and strong pressure assisted cold welding
CN112719569B (en) * 2020-12-31 2022-06-17 昆山哈工万洲焊接研究院有限公司 Method for preparing dissimilar metal composite structure through strong-deformation and strong-pressure auxiliary cold welding

Also Published As

Publication number Publication date
CN102069295B (en) 2012-12-12

Similar Documents

Publication Publication Date Title
CN101254572B (en) Method for diffusion welding titanium alloy and copper alloy using niobium central layer
Zhao et al. Microstructural evolutions and mechanical characteristics of Ti/steel clad plates fabricated through cold spray additive manufacturing followed by hot-rolling and annealing
CN101786898B (en) Method for connecting Cf/SiC composite material and Ni-based high-temperature alloy
CN108817083B (en) Preparation method for realizing strong metallurgical bonding of dissimilar metal interface
CN100436029C (en) Expansion connecting method for titanium and aluminium dissimillar non-ferrous metal
CN108118338B (en) A kind of method of high-frequency induction heating cladding TiC enhancing high entropy alloy coating
CN102069295B (en) Method for preparing Fe3Al/Al composite structure by diffusion bonding of reinforcing layer
CN108714695B (en) Preparation method of component and tissue dual gradient composite material
CN102677046B (en) Alloy composite special for laser cladding of rolling mill housings
CN100467186C (en) Fast expansion welding connection method for magnesium and aluminium dissimillar metals
Zhao et al. Influence of annealing on the microstructure and mechanical properties of Ti/steel clad plates fabricated via cold spray additive manufacturing and hot-rolling
CN107570830B (en) Method for auxiliary brazing of foam copper intermediate layer enhanced by CuO nano structure
CN109468638B (en) Preparation method of diamond-enhanced high-entropy alloy composite coating
CN107096994A (en) The diffusion welding (DW) fitting and its production method of a kind of high-purity zirconia composite ceramics and red copper
CN109277576B (en) Steel-carbide/iron-steel multilayer composite wear-resistant material and preparation method thereof
CN112323060A (en) Powder steel laser cladding cutter and production process thereof
CN113564576A (en) Ceramic phase gradient single-phase high-entropy alloy coating material and preparation method thereof
CN104099540A (en) Preparation method of NiTi fiber reinforced intermetallic compound-based laminar composite material for vibration and noise reduction
CN110450477B (en) Reinforced aluminum alloy composite board and preparation method thereof
CN102069290B (en) Process for preparing Fe3Al/Al composite structure by diffusion bonding
CN109267062B (en) Niobium alloy surface MoSi2Method for producing a coating
CN111005015A (en) Method for preparing gradient coating by steel surface cold spraying/laser gas nitriding compounding
Yi et al. Brazing of SiO 2 ceramic
CN111020557A (en) Ceramic-based buffer thermal insulation layer assisted magnesium alloy surface laser cladding composite coating and preparation method thereof
CN112663050B (en) In-situ synthesized nano core-shell structure TiC/Ti 5 Si 3 Particle-reinforced composite coating and preparation 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
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20121212

Termination date: 20151209

EXPY Termination of patent right or utility model