CN105562648B - A kind of method for shaping connecting integration with aluminium alloy semi-solid for titanium alloy - Google Patents

A kind of method for shaping connecting integration with aluminium alloy semi-solid for titanium alloy Download PDF

Info

Publication number
CN105562648B
CN105562648B CN201610131234.9A CN201610131234A CN105562648B CN 105562648 B CN105562648 B CN 105562648B CN 201610131234 A CN201610131234 A CN 201610131234A CN 105562648 B CN105562648 B CN 105562648B
Authority
CN
China
Prior art keywords
alloy
semi
titanium alloy
aluminium alloy
solid
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.)
Expired - Fee Related
Application number
CN201610131234.9A
Other languages
Chinese (zh)
Other versions
CN105562648A (en
Inventor
陈刚
韩柳娜
宋晓国
赵洪运
韩飞
冯吉才
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.)
Harbin Institute of Technology Weihai
Original Assignee
Harbin Institute of Technology Weihai
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 Harbin Institute of Technology Weihai filed Critical Harbin Institute of Technology Weihai
Priority to CN201610131234.9A priority Critical patent/CN105562648B/en
Publication of CN105562648A publication Critical patent/CN105562648A/en
Application granted granted Critical
Publication of CN105562648B publication Critical patent/CN105562648B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D17/00Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
    • B22D17/007Semi-solid pressure die casting

Abstract

The invention discloses a kind of method for shaping connecting integration with aluminium alloy semi-solid for titanium alloy, it be divided into by the titanium alloy of pre-connection be prepared into the titanium alloy tube of certain size and shape, titanium alloy tube is put into preheated together in mould, aluminium alloy is prepared to semi-solid blank or semi solid slurry that liquid fraction is 50-60%, aluminium alloy semi-solid state blank or semi solid slurry be moved into the titanium alloy tube in mould, punch-pin is rapid descending and is pressurizeed, and realizes that die forging connects the several steps of monolithic molding.The good fluidity that the present invention possesses when being in semisolid using aluminium alloy, realizes aluminium alloy Accurate Shaping;The formation of big thickness brittle compound layer is avoided, can react to form stable interface by the liquid phase in aluminium alloy semi-solid state blank and titanium alloy, connection reliability is high.In addition, this method is simple and easy to apply without special equipment, it is that titanium alloy and aluminium alloy shaping connecting integration can be achieved using common hydraulic press.

Description

A kind of method for shaping connecting integration with aluminium alloy semi-solid for titanium alloy
Technical field
Closed the present invention relates to a kind of method of semi-solid-state shaping connecting integration, more particularly to a kind of titanium alloy that is used for aluminium The method of golden semi-solid-state shaping connecting integration, belongs to material connection and forming technique field.
Background technology
Material attachment structure has the premium properties that multiple material is integrated, thus in Aero-Space, space technology, core work The fields such as industry, microelectronics, automobile, petrochemical industry are widely used.Due to the physical property and chemistry of pre-connection material There is very big difference in performance, the requirement to connection is harsher.
Semi-solid-state shaping includes rheological molding and thixotropic forming.Obtained semisolid non-dendritic slurry is directly formed Processing, referred to as rheological molding;And this slurry is first frozen into ingot casting, it is certain big further according to needing to cut into cast metals It is small, make its be reheated to semi-solid temperature it is interval and carry out be processed into thixotropic forming.Due to Solid-phase welding between titanium aluminium It is more difficult, the shortcomings of there is low efficiency, very flexible;And titanium aluminium melting welding is present that weld crack tendency is big, welding deformation is big, crisp The problems such as property metallic compound is serious, the reliability of connection is not high, the uniformity of bond strength and joint between connecting material It is difficult to meet and requires.
The content of the invention
In order to solve the weak point present in above-mentioned technology, it is used for titanium alloy and aluminium alloy half the invention provides one kind The method of solid molding connecting integration.
In order to solve the above technical problems, the technical solution adopted by the present invention is:One kind is used for titanium alloy and aluminium alloy half The method of solid molding connecting integration, it is divided into following steps:
A, geomery and performance requirement according to part formed thereby, by the titanium alloy of pre-connection be prepared into certain size and The titanium alloy tube of shape;
B, titanium alloy tube is put into mould preheated together, the temperature of preheating is 300-350 DEG C;
C, aluminium alloy is prepared into certain size and the aluminum alloy blank of shape, aluminum alloy blank is then used into electromagnetism sense Heater is answered to be preheated to 600-630 DEG C, be incubated 15-25 minutes, it is 50-60% to enable aluminum alloy to blank and be converted into liquid fraction Semi-solid blank;
Or using metal molten stove by aluminum alloy melting, smelting temperature is 700-730 DEG C, after progress after aluminum alloy melting Cooling, and electromagnetic agitation is applied to it in aluminium alloy cooling procedure, it is the partly solid of 50-60% to enable aluminum alloy to be converted to liquid fraction State slurry;
D, it will preheat and be incubated the aluminium alloy semi-solid state blank of completion or aluminium alloy semi-solid slurry is moved into mould In titanium alloy tube in, it is ensured that aluminium alloy semi-solid state blank is adjacent with titanium alloy tube;
E, punch-pin are rapid descending and are pressurizeed, and realize that die forging connects monolithic molding;After die forging completion, on punch-pin OK, be about to aluminium alloy and the good product ejection of two kinds of material joint formings of titanium alloy on push rod, complete whole Semi solid bonding into The process of shape integration.
The downward pressure of punch-pin of the present invention is 180-200kN, and descending speed is 10mm/s, and the dwell time is 10-20s. Titanium alloy is any of TA2, TA7, TB2, TC4 titanium alloy;Aluminium alloy is in 6063,6061,7075,2024 aluminium alloy It is any.
The present invention combines joint forming technology and semi-solid forming technology, has when being in semisolid using aluminium alloy Standby good fluidity, realizes aluminium alloy Accurate Shaping;Aluminium alloy semi-solid state blank temperature is low relative to melting welding, so as to avoid The formation of big thickness brittle compound layer, therefore can react to form steady by the liquid phase in aluminium alloy semi-solid state blank and titanium alloy Demarcation face, connection reliability is high.In addition, this method is simple and easy to apply without special equipment, it is that titanium can be achieved using common hydraulic press Alloy shapes connecting integration with aluminium alloy.
Brief description of the drawings
The present invention is further detailed explanation with reference to the accompanying drawings and detailed description.
Fig. 1, Fig. 2 are operating method schematic diagram of the embodiment of the present invention one to example IV.
Fig. 3 is operating method schematic diagram of the embodiment of the present invention five to embodiment eight.
In figure:1st, punch-pin;2nd, mould;4th, titanium alloy tube;5th, product;6th, cushion block;7th, push rod;31st, aluminium alloy semi-solid base Material;32nd, aluminium alloy semi-solid slurry.
Embodiment
As shown in FIG. 1 to 3, it is used for titanium alloy and aluminium alloy semi-solid shaping connecting integration the invention provides one kind Method, be specifically divided into following steps:
A, geomery and performance requirement according to part formed thereby, by the titanium alloy of pre-connection be prepared into certain size and The titanium alloy tube 4 of shape;
B, titanium alloy tube 4 is put into mould 2 preheated together, the temperature of preheating is 300-350 DEG C;
C, aluminium alloy is prepared into certain size and the aluminum alloy blank of shape, aluminum alloy blank is then used into electromagnetism sense Heater is answered to be preheated to 600-630 DEG C, be incubated 15-25 minutes, it is 50-60% to enable aluminum alloy to blank and be converted into liquid fraction Aluminium alloy semi-solid state blank 31;
Or using metal molten stove by aluminum alloy melting, smelting temperature is 700-730 DEG C, after progress after aluminum alloy melting Cooling, and electromagnetic agitation is applied to it in aluminium alloy cooling procedure, enable aluminum alloy to be converted to the aluminium conjunction that liquid fraction is 50-60% Golden semi solid slurry 32;
D, it will preheat and be incubated the aluminium alloy semi-solid state blank 31 of completion or be moved into aluminium alloy semi-solid slurry 32 In titanium alloy tube 4 in mould 2;The aluminium alloy semi-solid state blank 31 is adjacent with titanium alloy tube 4;
E, punch-pin 1 are rapid descending and are pressurizeed, and realize that die forging connects monolithic molding;After die forging completion, on punch-pin 1 OK, it is about to aluminium alloy on push rod 7 and the good product 5 of two kinds of material joint formings of titanium alloy is ejected, completes whole Semi solid bonding Forming integrated process.
The downward pressure of above-mentioned steps d convex moulds 1 is 180-200kN, and descending speed is 10mm/s, and the dwell time is 10-20s。
Contemplate present invention firstly provides titanium alloy and aluminium alloy shaping connecting integration, i.e., using aluminium alloy under semisolid The good fluidity and reactivity being had, while aluminium alloy Accurate Shaping is ensured, realize aluminium alloy and titanium alloy it Between be reliably connected.The present invention is applied to conventional most of titanium alloys and aluminium alloy, and be particularly suitable for use in TA2, TA7, TB2, TC4 Titanium alloy and 6063,6061,7075,2024 aluminium alloys.Titanium alloy and aluminium alloy below with regard to this several model combines specific real Example is applied to be further elaborated the present invention, but the invention is not limited in the titanium alloy of cited embodiment, aluminium alloy model.
Embodiment one:TA2 titanium alloys and 6063 aluminium alloys
A, for the ease of the aluminium alloy semi-solid state blank after preheating is put into titanium alloy tube, it is considered to thermal coefficient of expansion is 2.3×10-5Factor, by TA2 titanium alloy pipes be processed into size be φ 50mm × 5mm × h40mm TA2 titanium alloy tubes;Will 6063 aluminium alloy bars are processed into 6063 aluminum alloy blanks that size is φ 39mm × h50.6mm;
B, TA2 titanium alloy tubes are put into mould preheated together, preheating temperature is 300 DEG C;
C, using electromagnetic induction heater 6063 aluminum alloy blanks are preheated to 620 DEG C, are incubated 20 minutes, 6063 aluminium are closed Golden blank is converted into the semi-solid blank that liquid fraction is 60%;
D, it will preheat and be incubated 6063 aluminium alloy semi-solid state blanks 3 of completion and move into the TA2 titanium alloy tubes in mould, protect Demonstrate,prove 6063 aluminium alloy semi-solid state blanks adjacent with TA2 titanium alloy tubes;
The rapid descending and 196KN that pressurizes of e, punch-pin, punch-pin downstream rate is 10mm/s, and the dwell time is 10s, makes semisolid 6063 aluminium alloy semi-solid state blanks of humidity province complete die forging joint forming;Then punch-pin 1 is up, is about on push rod 7 by 6063 The product 5 of aluminium alloy and TA2 titanium alloys two sections of material composition is ejected together, takes out product 5.
Embodiment two:TA7 titanium alloys and 7075 aluminium alloys
A, TA7 titanium alloy pipes are processed into the TA7 titanium alloy tubes that size is φ 60mm × 5mm × h45mm.
B, TA7 titanium alloy tubes are put into mould preheated together, preheating temperature is 320 DEG C;
C, 7075 aluminium alloy bars are processed into the blank that size is φ 49mm × h62mm, filled using electromagnetic induction heating Put and 7075 aluminum alloy blanks are preheated to 620 DEG C, be incubated 18 minutes, 7075 aluminum alloy blanks are converted into half that liquid fraction is 56% Solid blank;
D, will preheat and be incubated 7075 aluminium alloy semi-solid state blanks of completion move into mould in TA7 titanium alloy tubes in, protect Demonstrate,prove 7075 aluminium alloy semi-solid state blanks adjacent with TA7 titanium alloy tubes;
The rapid descending and 190KN that pressurizes of e, punch-pin, punch-pin downstream rate is 10mm/s, and the dwell time is 15s, makes semisolid 7075 aluminium alloy semi-solid state blanks of humidity province complete die forging joint forming;Then, punch-pin 1 is up, is about on push rod 7 by 7075 The product 5 of aluminium alloy and TA7 titanium alloys two sections of material composition is ejected together, takes out product 5.
Embodiment three:TB2 titanium alloys and 2024 aluminium alloys
A, TB2 titanium alloy pipes are processed into the TB2 titanium alloy tubes that size is φ 40mm × 5mm × h35mm;
B, TB2 titanium alloy tubes are put into mould preheated together, preheating temperature is 350 DEG C;
C, 2024 aluminium alloy bars are processed into the blank that size is φ 29mm × h50mm, filled using electromagnetic induction heating Put and 2024 aluminum alloy blanks are preheated to 630 DEG C, be incubated 15 minutes, 2024 aluminum alloy blanks are converted into half that liquid fraction is 50% Solid blank;
D, will preheat and be incubated 2024 aluminium alloy semi-solid state blanks of completion move into mould in TB2 titanium alloy tubes in, protect Demonstrate,prove 2024 aluminium alloy semi-solid state blanks adjacent with TB2 titanium alloy tubes;
The rapid descending and 180KN that pressurizes of e, punch-pin, punch-pin downstream rate is 10mm/s, and the dwell time is 20s, makes semisolid 2024 aluminium alloy semi-solid state blanks of humidity province complete die forging joint forming;Then, punch-pin is up, is about on push rod by 2024 aluminium The product of alloy and TB2 titanium alloys two sections of material composition is ejected together, takes out product.
Example IV:TC4 titanium alloys and 6061 aluminium alloys
A, TC4 titanium alloy pipes are processed into the TC4 titanium alloy tubes that size is φ 55mm × 5mm × h45mm;
B, TC4 titanium alloy tubes are put into mould preheated together, preheating temperature is 300 DEG C;
C, 6061 aluminium alloy bars are processed into the blank that size is φ 44mm × h60mm, filled using electromagnetic induction heating Put and 6061 aluminum alloy blanks are preheated to 600 DEG C, be incubated 25 minutes, 6061 aluminum alloy blanks are converted into half that liquid fraction is 55% Solid blank;
D, it will preheat and be incubated 6061 aluminium alloy semi-solid state blanks 3 of completion and move into the TC4 titanium alloy tubes in mould, protect Demonstrate,prove 6061 aluminium alloy semi-solid state blanks adjacent with TC4 titanium alloy tubes;
The rapid descending and 200KN that pressurizes of e, punch-pin, punch-pin downstream rate is 10mm/s, and the dwell time is 18s, makes semisolid The aluminium alloy semi-solid state blank of humidity province completes die forging joint forming;Then, punch-pin 1 is up, is about to be closed by 6061 aluminium on push rod 7 The product 5 that gold and TC4 titanium alloys two sections of material are constituted is ejected together, takes out product 5.
Embodiment five:TA2 titanium alloys and 6061 aluminium alloys
A, TA2 titanium alloy pipes are processed into the TA2 titanium alloy tubes that size is φ 45mm × 5mm × h50mm;
B, TA2 titanium alloy tubes are put into mould preheated together, the temperature of preheating is 350 DEG C;
C, using metal molten stove by 6061 aluminum alloy meltings, smelting temperature is 730 DEG C, treats that 6061 aluminum alloy meltings are laggard Row cooling, and apply electromagnetic agitation to it in 6061 aluminium alloy cooling procedures, it is 50% that 6061 aluminium alloys, which are converted to liquid fraction, Semi solid slurry;
D, by 6061 aluminium alloy semi-solid slurries move into mould in TA2 titanium alloy tubes in;
E, punch-pin are rapid descending and carry out pressurization 190KN, and punch-pin downstream rate is 10mm/s, and the dwell time is 10s, make half 6061 aluminium alloy semi-solid slurries in solid state temperature area complete die forging joint forming;After die forging completion, punch-pin is up, push rod On be about to 6061 aluminium alloys and the good product ejection of two kinds of material joint formings of TA2 titanium alloys, complete whole Semi solid bonding into The process of shape integration.
Embodiment six:TC4 titanium alloys and 7075 aluminium alloys
A, TC4 titanium alloy pipes are processed into the TC4 titanium alloy tubes that size is φ 47mm × 5mm × h45mm;
B, TC4 titanium alloy tubes are put into mould preheated together, the temperature of preheating is 330 DEG C;
C, using metal molten stove by 7075 aluminum alloy meltings, smelting temperature is 720 DEG C, treats that 7075 aluminum alloy meltings are laggard Row cooling, and apply electromagnetic agitation to it in 7075 aluminium alloy cooling procedures, it is 58% that 7075 aluminium alloys, which are converted to liquid fraction, Semi solid slurry;
D, by 7075 aluminium alloy semi-solid slurries move into mould in TC4 titanium alloy tubes in;
E, punch-pin are rapid descending and carry out pressurization 180KN, and punch-pin downstream rate is 10mm/s, and the dwell time is 16s, make half 7075 aluminium alloy semi-solid slurries in solid state temperature area complete die forging joint forming;After die forging completion, punch-pin is up, push rod On be about to 7075 aluminium alloys and the good product ejection of two kinds of material joint formings of TC4 titanium alloys, complete whole Semi solid bonding into The process of shape integration.
Embodiment seven:TA7 titanium alloys and 2024 aluminium alloys
A, TA7 titanium alloy pipes are processed into the TA7 titanium alloy tubes that size is φ 65mm × 5mm × h55mm;
B, TA7 titanium alloy tubes are put into mould preheated together, the temperature of preheating is 300 DEG C;
C, using metal molten stove by 2024 aluminum alloy meltings, smelting temperature is 710 DEG C, treats that 2024 aluminum alloy meltings are laggard Row cooling, and apply electromagnetic agitation to it in 2024 aluminium alloy cooling procedures, it is 52% that 2024 aluminium alloys, which are converted to liquid fraction, Semi solid slurry;
D, by 2024 aluminium alloy semi-solid slurries move into mould in TA7 titanium alloy tubes in;
E, punch-pin are rapid descending and carry out pressurization 196KN, and punch-pin downstream rate is 10mm/s, and the dwell time is 10s, make half 2024 aluminium alloy semi-solid slurries in solid state temperature area complete die forging joint forming;After die forging completion, punch-pin is up, push rod On be about to 2024 aluminium alloys and the good product ejection of two kinds of material joint formings of TA7 titanium alloys, complete whole Semi solid bonding into The process of shape integration.
Embodiment eight:TB2 titanium alloys and 6063 aluminium alloys
A, TB2 titanium alloy pipes are processed into the TB2 titanium alloy tubes that size is φ 60mm × 4mm × h45mm;
B, TB2 titanium alloy tubes are put into mould preheated together, the temperature of preheating is 310 DEG C;
C, using metal molten stove by 6063 aluminum alloy meltings, smelting temperature is 700 DEG C, treats that 6063 aluminum alloy meltings are laggard Row cooling, and apply electromagnetic agitation to it in 6063 aluminium alloy cooling procedures, it is 60% that 6063 aluminium alloys, which are converted to liquid fraction, Semi solid slurry;
D, by 6063 aluminium alloy semi-solid slurries move into mould in TB2 titanium alloy tubes in;
E, punch-pin are rapid descending and carry out pressurization 200KN, and punch-pin downstream rate is 10mm/s, and the dwell time is 20s, make half 6063 aluminium alloy semi-solid slurries in solid state temperature area complete die forging joint forming;After die forging completion, punch-pin is up, push rod On be about to 6063 aluminium alloys and the good product ejection of two kinds of material joint formings of TB2 titanium alloys, complete whole Semi solid bonding into The process of shape integration.
Above-mentioned embodiment is not limitation of the present invention, and the present invention is also not limited to the example above, this technology neck The variations, modifications, additions or substitutions that the technical staff in domain is made in the range of technical scheme, also belong to this hair Bright protection domain.

Claims (3)

1. a kind of method for shaping connecting integration with aluminium alloy semi-solid for titanium alloy, it is characterised in that it is divided into following Step:
A, geomery and performance requirement according to part formed thereby, certain size and shape are prepared into by the titanium alloy of pre-connection Titanium alloy tube (4);
B, titanium alloy tube (4) is put into mould (2) preheated together, the temperature of preheating is 300-350 DEG C;
C, aluminium alloy is prepared into certain size and the aluminum alloy blank of shape, then added aluminum alloy blank using electromagnetic induction Thermal is preheated to 600-630 DEG C, is incubated 15-25 minutes, enables aluminum alloy to blank and is converted into the aluminium conjunction that liquid fraction is 50-60% Golden semi-solid blank (31);
Or using metal molten stove by aluminum alloy melting, smelting temperature is 700-730 DEG C, cold after being carried out after aluminum alloy melting But, and in aluminium alloy cooling procedure to it apply electromagnetic agitation, enable aluminum alloy to be converted to the aluminium alloy that liquid fraction is 50-60% Semi solid slurry (32);
D, it will preheat and be incubated the aluminium alloy semi-solid state blank (31) of completion or be moved into aluminium alloy semi-solid slurry (32) In titanium alloy tube (4) in mould (2);The aluminium alloy semi-solid state blank (31) is adjacent with titanium alloy tube (4);
E, punch-pin (1) are rapid descending and are pressurizeed, and realize that die forging connects monolithic molding;After die forging completion, on punch-pin (1) OK, it is about to aluminium alloy and good product (5) ejection of two kinds of material joint formings of titanium alloy on push rod (7), completes whole semisolid The process of joint forming integration.
2. the method according to claim 1 for shaping connecting integration with aluminium alloy semi-solid for titanium alloy, its feature It is:The downward pressure of the punch-pin (1) is 180-200kN, and descending speed is 10mm/s, and the dwell time is 10-20s.
3. the method according to claim 1 for shaping connecting integration with aluminium alloy semi-solid for titanium alloy, its feature It is:The titanium alloy is any of TA2, TA7, TB2, TC4 titanium alloy;The aluminium alloy be 6063,6061,7075, Any of 2024 aluminium alloys.
CN201610131234.9A 2016-03-09 2016-03-09 A kind of method for shaping connecting integration with aluminium alloy semi-solid for titanium alloy Expired - Fee Related CN105562648B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610131234.9A CN105562648B (en) 2016-03-09 2016-03-09 A kind of method for shaping connecting integration with aluminium alloy semi-solid for titanium alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610131234.9A CN105562648B (en) 2016-03-09 2016-03-09 A kind of method for shaping connecting integration with aluminium alloy semi-solid for titanium alloy

Publications (2)

Publication Number Publication Date
CN105562648A CN105562648A (en) 2016-05-11
CN105562648B true CN105562648B (en) 2017-09-29

Family

ID=55873584

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610131234.9A Expired - Fee Related CN105562648B (en) 2016-03-09 2016-03-09 A kind of method for shaping connecting integration with aluminium alloy semi-solid for titanium alloy

Country Status (1)

Country Link
CN (1) CN105562648B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108746565B (en) * 2018-06-05 2020-06-16 宁波海威汽车零件股份有限公司 Preparation method of semi-solid slurry
CN109763006B (en) * 2019-02-01 2020-08-11 哈尔滨工业大学(威海) Forming and connecting integrated method for aluminum-magnesium composite component
CN109732054A (en) * 2019-02-02 2019-05-10 东营源纳合金科技有限公司 It is a kind of special type aluminium alloy semi-solid material preparation and automatic forming device
CN109807272B (en) * 2019-02-18 2020-11-10 哈尔滨工业大学(威海) Aluminum steel bimetal component thixotropic soft core composite forging forming method

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4771818A (en) * 1979-12-14 1988-09-20 Alumax Inc. Process of shaping a metal alloy product
CN1772414A (en) * 2004-11-10 2006-05-17 北京有色金属研究总院 Composite electromagnetic stirring process of preparing semi-solid metal slurry continuously
CN101077522A (en) * 2007-06-21 2007-11-28 北京科技大学 Semi-solid composite connecting forming process for preparing compound structures parts
CN101121184A (en) * 2007-09-07 2008-02-13 宝鸡市亚钛新金属有限公司 Method for manufacturing titanium base composite pipe-rod materials
CN103231218A (en) * 2013-05-11 2013-08-07 哈尔滨工业大学(威海) Rapid production technology of titanium alloy pipes
CN104085485A (en) * 2014-07-09 2014-10-08 黄启达 Optimization connecting structure of metal pipe fittings and implementation method thereof

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4771818A (en) * 1979-12-14 1988-09-20 Alumax Inc. Process of shaping a metal alloy product
CN1772414A (en) * 2004-11-10 2006-05-17 北京有色金属研究总院 Composite electromagnetic stirring process of preparing semi-solid metal slurry continuously
CN101077522A (en) * 2007-06-21 2007-11-28 北京科技大学 Semi-solid composite connecting forming process for preparing compound structures parts
CN101121184A (en) * 2007-09-07 2008-02-13 宝鸡市亚钛新金属有限公司 Method for manufacturing titanium base composite pipe-rod materials
CN103231218A (en) * 2013-05-11 2013-08-07 哈尔滨工业大学(威海) Rapid production technology of titanium alloy pipes
CN104085485A (en) * 2014-07-09 2014-10-08 黄启达 Optimization connecting structure of metal pipe fittings and implementation method thereof

Also Published As

Publication number Publication date
CN105562648A (en) 2016-05-11

Similar Documents

Publication Publication Date Title
CN105562648B (en) A kind of method for shaping connecting integration with aluminium alloy semi-solid for titanium alloy
CN102626821B (en) Method for connecting semi-solid materials into whole
CN109807272B (en) Aluminum steel bimetal component thixotropic soft core composite forging forming method
CN107186139B (en) The H profile steel manufacturing method of nuclear fusion stack magnet support
CN104475698B (en) A kind of liquid forging method of many areas exerted pressure on
CN104708192A (en) Diffusion welding method for W-Ti alloy target assembly
CN110394410A (en) A method of preparing big specification male sportsman fine grain bar
CN105499304A (en) Semi-solid forming method of composite pipe
CN102676855A (en) Method for preparing high magnesium aluminium alloy ingot used for forging hubs
CN105441844A (en) Extrusion blooming method for high-deformation superalloy ingot casting
CN106890917A (en) Super large ratio of height to diameter steel billet upset forging process and equipment
CN102441585A (en) Preparation method of aluminium alloy composite pipe
CN101540221A (en) Preparation method and mould of liquid-solid composite forming copper cladding aluminum bus duct platoon blank
CN108723110A (en) A method of pipeline assembly is made using marmem
CN104550838B (en) The technique that a kind of radial forging strain-induced method prepares semisolid iron and steel camshaft
CN106623580B (en) A kind of hot extrusion and the method for expansive forming composite manufacturing bathroom faucet branch pipe
CN110961560A (en) Forging method for one-time upsetting forming of large-height-diameter-ratio bar
CN103464976A (en) Nut machining method
CN101722257A (en) Pseudo-plastic forming method for processing metal-based composite materials
TWI314077B (en)
CN104550837A (en) CIM (Computer Integrated Manufacturing)-process-based hot-work die steel material surface modification method
CN104476128A (en) Method of manufacturing high-temperature alloy pipe blanks
CN102728945A (en) Liquid phase connected die forging integral forming method of material
CN113059020A (en) Bimetal composite pipe and preparation method thereof
CN101480710B (en) Method for producing internally casting cooling water pipe melt-through-preventing high alloy cast steel

Legal Events

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

Granted publication date: 20170929

Termination date: 20190309