CN106825859B - A kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method - Google Patents
A kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method Download PDFInfo
- Publication number
- CN106825859B CN106825859B CN201710029181.4A CN201710029181A CN106825859B CN 106825859 B CN106825859 B CN 106825859B CN 201710029181 A CN201710029181 A CN 201710029181A CN 106825859 B CN106825859 B CN 106825859B
- Authority
- CN
- China
- Prior art keywords
- aluminum alloy
- welding
- junction component
- alloy junction
- electric arc
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K9/00—Arc welding or cutting
- B23K9/04—Welding for other purposes than joining, e.g. built-up welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K9/00—Arc welding or cutting
- B23K9/235—Preliminary treatment
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Mechanical Engineering (AREA)
- Arc Welding In General (AREA)
Abstract
A kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method.This method carries out the electric arc increasing material manufacturing of aluminum alloy junction component in such a way that welding machine provides heat source cooperative mechanical arm progress path planning.Electric current bottoming of three layers of the bottom using 20A~50A big compared with forming current or so;Entity is accumulated using forming current in top, and every road Ceng Nei and outer course arcing point are a pair of of angle steel joint, and and so on, final forming obtains multilayer two pass aluminum alloy junction component.Wherein, material is increased by the electric arc that 10mm~25mm wall thickness aluminum alloy junction component can be achieved in the adjustment of parameter, to meet specific size requirements.Electric arc increasing material manufacturing aluminum alloy junction component good mechanical properties proposed by the invention, surface roughness is small, flawless defect, and stock utilization is high, with short production cycle;It solves the problems, such as that big wall thickness aluminum alloy junction component quickly manufactures in the development stage, while solving the problems such as long production period that conventional casting methods need to make mold, also significantly reduce product cost.
Description
Technical field
The invention belongs to material increasing fields, and in particular to a kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing side
Method.
Background technique
Aluminium alloy has the advantages that low-density, corrosion-resistant, with can effectively mitigate its weight on aerospace flight vehicle, increases
Big thrust loading, so being widely used in aerospace etc. requires light-weighted field.Traditional aluminium alloy processing method mainly has
Casting and machining etc., although being able to satisfy the requirement such as machining accuracy, there are difficulty of processing greatly, process is tedious, material use
The deficiencies of rate is low, high production cost, long production cycle.Sometimes for product progress, design is tested repeatedly in practical development and production
Card, product size, structure etc. also need to change at any time, and traditional processing method not only has longer production cycle, cost
It is significantly increased.Meanwhile properties of product are directly influenced there are more gross imperfection and component segregation in mo(u)lded piece.It is existing
Manufacturing technology be difficult to meet the quick and various development and production demand of novel product.
As the key areas such as aerospace, rail traffic are to the performance of hardware, precision, production cycle and production
The requirement of cost is increasingly harsh, becomes research hotspot using increases material manufacturing technology direct forming metal parts.
In material increasing field, there is equipment for the electric arc increases material manufacturing technology of raw material using arc heat as heat source, silk material
The advantages that small investment, stock utilization are high, production cost is low, with short production cycle, metallurgical bonding performance is good, excellent combination property,
It is very suitable for quick, the inexpensive development and production of the fields such as aerospace small mount, multi items product.
Summary of the invention
Technical problem solved by the present invention is overcome the deficiencies in the prior art, proposes that a kind of aluminum alloy junction component multilayer is double
Road electric arc increasing material manufacturing method, using this method can realize in big wall thickness aluminum alloy junction component quick near-net-shape, structural member
Surface roughness is small, good mechanical performance, and production cost has been greatly reduced, has shortened the production cycle.
The technical solution of the present invention is as follows: a kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method, which is closed
Golden structural member is formed by electric arc increasing material manufacturing system 3D printing;Steps are as follows:
1) welding wire required for selection forming specific structure part, determines running parameter required for forming specific structure part, packet
Include wire feed rate, welding current, speed of welding, welding gun offset, single-pass welding width and weld bead height;
2) it will be fixed after the substrate of overpickling polishes flat and uses dehydrated alcohol or acetone wiped clean on the table,
Guarantee its level;
3) according to step 1) determine parameter bottoming is carried out on substrate, after the completion of bottoming, use instead forming parameters into
The accumulation of row entity part, the every road Ceng Nei of entity part and outer course arcing point are a pair of of angle steel joint, the direction of travel phase of adjacent layer
Instead, and so on until reaching the requirement of short transverse size, final forming obtains aluminum alloy junction component.
The 5A06 aluminum alloy plate materials that the substrate is selected with a thickness of 20-50mm.
The welding wire uses diameter for the 5B06 aluminium alloy welding wire of 0.8mm or 1.2mm or 1.6mm;The wire feed rate is 5
~10m/min;The welding current is 80~140A;The speed of welding is 7~12mm/s;The single-pass welding width 6~
10mm;1.3~the 1.8mm of weld bead height.
Increase material during use 99.999% high-purity argon to aluminum alloy junction component carry out front protecting, gas flow be 18~
20L/min。
It is all made of C+P mode in bottoming and entity part banking process, i.e. cold metal transfer+pulse mode, three layers of bottom
Using the welding current bottoming of 20~50A bigger than forming current, top is accumulated to obtain using forming parameters by planning path
Entity.
The every road Ceng Nei of entity part and outer course arcing point are a pair of of angle steel joint, 2n+1 layers with the 2nd (n+1) layer
Arcing point is identical, and adjacent layer welding gun direction of travel is opposite;Wherein n is zero-based integer, and when n is even number, arcing point is
One pair of them angle steel joint;When n is odd number, arcing point is another pair angle steel joint.
After finishing every road Ceng Nei, welding gun deviates certain offset and completes the accumulation of outer course again with good between realizing
Overlap joint, the width that welding gun offset is chosen for single-pass welding subtract 2~5mm.
The advantages of the present invention over the prior art are that:
Aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method proposed by the invention, equipment investment is few, material is sharp
It is high (close to 100%) with rate, it reduces production cost, shorten the production cycle;Its formation of parts is made of full seam organization, fine and close
Degree is high, and metallurgical bonding performance is good, and chemical component is uniform, and mechanical property is more than casting and reachable forging is horizontal.
Detailed description of the invention
Fig. 1 is that electric arc of the present invention increases material aluminum alloy junction component sectional view;Wherein 1 (a) is front view, and 1 (b) is side view
Figure;
Fig. 2 is that electric arc of the present invention increases material path schematic diagram.
Specific embodiment
Hereafter specific method of the invention is illustrated by example:
Example: 15mm thickness 5B06 aluminium alloy rectangular structural member multilayer two pass electric arc increasing material manufacturing
Specific implementation method are as follows: as shown in Figure 1, it is desirable that the aluminum alloy junction component wall thickness 15mm of manufacture, length and width and high difference
For 400mm, 200mm and 400mm, it is considered as multilayer two pass electric arc and increases material forming.The raw material used is ф 1.2mm 5B06
Aluminium alloy welding wire first passes through test and gropes to obtain one group of suitable forming parameters: welding current 120A, wire feed rate 7m/
Min, speed of welding 8mm/s, under this group of technological parameter, single-pass welding width 8mm, height 1.3mm, welding gun offset is 5mm, energy
Enough fusion and monolithic molding are good between guarantee road;Substrate through overpickling is polished flat and is wiped with dehydrated alcohol or acetone
It is fixed on the table after net, guarantees its level;Suitable position, which is chosen, in substrate carries out bottoming, bottoming parameter: welding current
159A, wire feed rate 9m/min, speed of welding 8mm/s;After the completion of three layers of bottoming, uses forming parameters instead and carry out entity part
Accumulation: as shown in Fig. 2, wherein arrow is mechanical arm walking path;1st road Ceng Nei arcing point is point 1, and outer course is point 3, walking side
To for counterclockwise;After completing the 1st layer, welding gun raises 1.3mm and carries out the 2nd layer heap product;2nd road Ceng Nei and outer course arcing point and the 1st
Outer course is identical in layer, but direction of travel is clockwise;After completing the 2nd layer, welding gun raises 1.3mm and carries out the 3rd layer heap product;3rd layer
Interior road arcing point is point 2, and outer course is point 4, and direction of travel is counterclockwise;After completing the 3rd layer, welding gun raises 1.3mm and carries out the 4th layer
Accumulation;4th road Ceng Nei is identical as outer course in outer course arcing point and the 3rd layer, but direction of travel is clockwise;Four layers are followed for one
Ring, and so on until reaching the requirement of short transverse size, final forming obtains aluminum alloy junction component.
Claims (2)
1. a kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method, the aluminum alloy junction component is by electric arc increasing material manufacturing
System 3D printing is formed;It is characterized by the following steps:
1) welding wire required for selection forming specific structure part, determines running parameter required for forming specific structure part, including send
Silk speed, welding current, speed of welding, welding gun offset, single-pass welding width and weld bead height;
2) it will fix on the table, guarantee after the substrate of overpickling polishes flat and uses dehydrated alcohol or acetone wiped clean
It is horizontal;
3) bottoming is carried out on substrate according to the parameter that step 1) determines, after the completion of bottoming, uses forming parameters instead and carry out in fact
Body portion accumulation, the every road Ceng Nei of entity part and outer course arcing point are a pair of of angle steel joint, and the direction of travel of adjacent layer is on the contrary, such as
This is reciprocal until reaching the requirement of short transverse size, and final forming obtains aluminum alloy junction component;Every layer of the entity part it is interior
Road and outer course arcing point are a pair of of angle steel joint, and 2n+1 layers identical as the arcing point of the 2nd (n+1) layer, adjacent layer welding gun walking side
To opposite;Wherein n is zero-based integer, and when n is even number, arcing point is one pair of them angle steel joint;When n is odd number,
Arcing point is another pair angle steel joint;
The 5A06 aluminum alloy plate materials that the substrate is selected with a thickness of 20-50mm;
The welding wire uses diameter for the 5B06 aluminium alloy welding wire of 0.8mm or 1.2mm or 1.6mm;The wire feed rate be 5~
10m/min;The welding current is 80~140A;The speed of welding is 7~12mm/s;The single-pass welding width 6~
10mm;1.3~the 1.8mm of weld bead height;
It is all made of C+P mode in bottoming and entity part banking process, i.e. cold metal transfer+pulse mode, the use of three layers of bottom
The welding current bottoming of 20~50A bigger than forming current, top are accumulated to obtain entity by planning path using forming parameters;
After finishing every road Ceng Nei, welding gun deviates certain offset and completes the accumulation of outer course again with well taking between realizing
It connects, the width that welding gun offset is chosen for single-pass welding subtracts 2~5mm.
2. a kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method according to claim 1, it is characterised in that:
Increase material uses 99.999% high-purity argon to carry out front protecting to aluminum alloy junction component in the process, and gas flow is 18~20L/min.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710029181.4A CN106825859B (en) | 2017-01-16 | 2017-01-16 | A kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710029181.4A CN106825859B (en) | 2017-01-16 | 2017-01-16 | A kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method |
Publications (2)
Publication Number | Publication Date |
---|---|
CN106825859A CN106825859A (en) | 2017-06-13 |
CN106825859B true CN106825859B (en) | 2019-07-16 |
Family
ID=59123254
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710029181.4A Active CN106825859B (en) | 2017-01-16 | 2017-01-16 | A kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106825859B (en) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107876938A (en) * | 2017-10-16 | 2018-04-06 | 北京航星机器制造有限公司 | Bridging method between a kind of electric arc increasing material manufacturing road based on mechanical arm swing |
CN107944154B (en) * | 2017-11-29 | 2021-03-30 | 西南交通大学 | Automatic calculation method for variables of electric arc wire filling additive manufacturing layered slicing process |
CN108098112A (en) * | 2017-12-14 | 2018-06-01 | 上海工程技术大学 | A kind of method of electric arc increasing material manufacturing heterogeneity aluminum alloy composite material |
CN108161178A (en) * | 2018-01-30 | 2018-06-15 | 北京理工大学 | A kind of aluminum alloy junction component electric arc increases material forming method |
CN108340057A (en) * | 2018-03-09 | 2018-07-31 | 上海工程技术大学 | A kind of aluminum alloy thick wall structure Rapid Shaping Technology of Arc Welding |
CN109332860B (en) * | 2018-11-23 | 2021-01-05 | 大连理工大学 | Arc additive manufacturing method of 5083 aluminum alloy/TC 4 titanium alloy structure |
CN109530858B (en) * | 2018-12-26 | 2021-09-07 | 北京航星机器制造有限公司 | Method for improving aluminum alloy electric arc additive metallurgy strength |
CN109530859A (en) * | 2018-12-26 | 2019-03-29 | 北京航星机器制造有限公司 | A kind of GH4099 high temperature alloy structural member electric arc increasing material manufacturing method |
CN110508901B (en) * | 2019-09-16 | 2021-01-19 | 西安交通大学 | Method for emergency repair of damaged Al-Mg series aluminum alloy component of ship through electric arc additive manufacturing |
CN110899905B (en) * | 2019-12-03 | 2024-04-16 | 天津工业大学 | Correction method for polygonal member sharp angle path based on arc additive manufacturing |
CN110919135B (en) * | 2019-12-03 | 2021-07-13 | 哈尔滨电机厂有限责任公司 | Preparation method for Babbitt metal composite welding on surface of curved surface bearing bush |
CN110814467A (en) * | 2019-12-03 | 2020-02-21 | 天津工业大学 | Path correction method for eliminating edge collapse of arc additive manufacturing component |
CN112276296B (en) * | 2020-09-09 | 2022-10-14 | 北京航星机器制造有限公司 | Path planning method for improving internal quality of arc additive structural part |
CN112846445B (en) * | 2020-12-31 | 2022-04-15 | 南京英尼格玛工业自动化技术有限公司 | Metal structure multilayer multi-channel composite electric arc additive manufacturing method and system |
CN113695709A (en) * | 2021-09-06 | 2021-11-26 | 上海航天精密机械研究所 | Aerospace force-bearing structure arc fuse additive path planning method for designing tail stock |
CN115555683B (en) * | 2022-08-11 | 2023-10-24 | 南京联空智能增材研究院有限公司 | Arc material-increasing method for aluminum alloy die |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102962547A (en) * | 2012-11-23 | 2013-03-13 | 首都航天机械公司 | Manufacturing method of arc additive of titanium alloy structural part |
CN106002277A (en) * | 2016-05-25 | 2016-10-12 | 华中科技大学 | Electric arc additive and milling composite machining method and product thereof |
CN106141373A (en) * | 2016-07-18 | 2016-11-23 | 南京航空航天大学 | The electric arc 3D printing device of aluminum alloy junction component and Method of printing |
-
2017
- 2017-01-16 CN CN201710029181.4A patent/CN106825859B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102962547A (en) * | 2012-11-23 | 2013-03-13 | 首都航天机械公司 | Manufacturing method of arc additive of titanium alloy structural part |
CN106002277A (en) * | 2016-05-25 | 2016-10-12 | 华中科技大学 | Electric arc additive and milling composite machining method and product thereof |
CN106141373A (en) * | 2016-07-18 | 2016-11-23 | 南京航空航天大学 | The electric arc 3D printing device of aluminum alloy junction component and Method of printing |
Non-Patent Citations (3)
Title |
---|
基于CMT的铝合金电弧增材制造(3D打印)技术及工艺研究;张瑞;《CNKI优秀硕士学位论文》;20160630;正文第12,27-32页 |
复合铣削的电弧增材制造路径规划方法与应用研究;樊建勋;《CNKI优秀硕士学位论文》;20160531;正文第11-16页 |
电弧增材制造与铣削复合加工系统与工艺研究;夏然飞等;《制造业自动化》;20160925(第09期);第79-83页第79-83页 |
Also Published As
Publication number | Publication date |
---|---|
CN106825859A (en) | 2017-06-13 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106825859B (en) | A kind of aluminum alloy junction component multilayer two pass electric arc increasing material manufacturing method | |
EP3674018A1 (en) | Method for controlling deformation and precision of parts in parallel during additive manufacturing process | |
CN106392270B (en) | With the method for electric arc increasing material manufacturing aluminium alloy multilayer single track closing structure part | |
CN105252145B (en) | A kind of method and apparatus of sheet metal superposition manufacture complicated shape part | |
TWI498439B (en) | Tubular target and production method | |
CN107876938A (en) | Bridging method between a kind of electric arc increasing material manufacturing road based on mechanical arm swing | |
CN108637504A (en) | A kind of electric arc fills silk and rolls compound increasing material manufacturing method and apparatus | |
CN106944715A (en) | A kind of method of highly efficient multi-position electric arc increasing material manufacturing aluminum alloy junction component | |
CN104209484B (en) | Narrow-face copper plate for chamfer crystallizer | |
CN107052520A (en) | A kind of single track electric arc, which is swung, increases the method that material shapes big wall thickness aluminum alloy junction component | |
CN106735802A (en) | A kind of titanium alloy cylindrical structural member plasma arc increasing material manufacturing method | |
CN108580638A (en) | A kind of big L/D ratio thin-wall aluminum alloy abnormity component spin forming method | |
CN102489952A (en) | Method for manufacturing titanium alloy thick-wall pressure-resistant cylinder body | |
CN102172665A (en) | High-precision aluminum alloy rectangular tube forming method | |
CN104191092B (en) | The laser-TIG hybrid silk filling seal weld method of L-type aluminium alloy structure | |
CN109530851A (en) | A kind of aluminium alloy hanging structure part electric arc increasing material manufacturing method | |
CN106513675A (en) | Laser additive manufacturing forming method of titanium alloy thin-walled component | |
CN110004311A (en) | It is a kind of for directly manufacturing the preparation method of the TC4 titan alloy casting ingot of seamless pipe | |
CN105414297A (en) | Asynchronous stagger spinning machining method | |
CN105665468A (en) | Preparation method for high-precision large-diameter thin-walled titanium tube | |
CN106001903A (en) | Friction stir welding method for butt-lap joint composite connector aluminum alloy hollow extruded profile | |
CN106311836A (en) | Forming method and device for large-pipe-diameter thin-wall pipeline moving towards complex space | |
CN110539000B (en) | Titanium alloy member and method for producing same | |
CN105063367A (en) | Preparation method for smelting electrodes | |
CN104959503A (en) | Preparation process of modern track low-floor motor train large-scale integral forging axle |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |