CN112453421A - Reinforced material adding process based on arc fuse and mold reinforcing method - Google Patents
Reinforced material adding process based on arc fuse and mold reinforcing method Download PDFInfo
- Publication number
- CN112453421A CN112453421A CN202011315049.8A CN202011315049A CN112453421A CN 112453421 A CN112453421 A CN 112453421A CN 202011315049 A CN202011315049 A CN 202011315049A CN 112453421 A CN112453421 A CN 112453421A
- Authority
- CN
- China
- Prior art keywords
- fuse
- grid frame
- arc fuse
- arc
- additive
- 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
Links
- 239000000463 material Substances 0.000 title claims abstract description 75
- 238000000034 method Methods 0.000 title claims abstract description 40
- 230000008569 process Effects 0.000 title claims abstract description 29
- 230000003014 reinforcing effect Effects 0.000 title description 3
- 239000000654 additive Substances 0.000 claims abstract description 107
- 230000000996 additive effect Effects 0.000 claims abstract description 107
- 238000005728 strengthening Methods 0.000 claims abstract description 24
- 238000005496 tempering Methods 0.000 claims abstract description 16
- 238000010438 heat treatment Methods 0.000 claims abstract description 12
- 238000002844 melting Methods 0.000 claims abstract description 11
- 230000008018 melting Effects 0.000 claims abstract description 11
- 229910045601 alloy Inorganic materials 0.000 claims description 21
- 239000000956 alloy Substances 0.000 claims description 21
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 14
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 14
- 230000000694 effects Effects 0.000 claims description 8
- 238000010583 slow cooling Methods 0.000 claims description 8
- 229910000746 Structural steel Inorganic materials 0.000 claims description 7
- 229910052742 iron Inorganic materials 0.000 claims description 7
- 229910052759 nickel Inorganic materials 0.000 claims description 7
- 229910000734 martensite Inorganic materials 0.000 claims description 6
- 238000010146 3D printing Methods 0.000 claims description 4
- 239000004576 sand Substances 0.000 claims description 4
- 239000000155 melt Substances 0.000 claims description 3
- 230000009467 reduction Effects 0.000 claims description 3
- 238000001816 cooling Methods 0.000 claims description 2
- 238000009413 insulation Methods 0.000 claims 2
- 230000003416 augmentation Effects 0.000 claims 1
- 238000003466 welding Methods 0.000 abstract description 7
- 238000010891 electric arc Methods 0.000 description 7
- 238000005299 abrasion Methods 0.000 description 6
- 238000004321 preservation Methods 0.000 description 4
- 238000004088 simulation Methods 0.000 description 4
- 230000009471 action Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/24—After-treatment of workpieces or articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/08—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y10/00—Processes of additive manufacturing
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/0068—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/24—After-treatment of workpieces or articles
- B22F2003/248—Thermal after-treatment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
- B22F2007/068—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts repairing articles
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Composite Materials (AREA)
- Heat Treatment Of Articles (AREA)
Abstract
本发明公开了一种基于电弧熔丝的强化增材工艺，每熔丝增材形成一个电弧熔丝增材层，就对电弧熔丝增材层进行锤击；每电弧熔丝增材2~3层，就铺设网格框架；铺设网格框架后对网格框架进行锤击以使网格框架与电弧熔丝增材层贴合；铺设网格框架时，在电弧熔丝增材层上焊接钉子对网格进行定位；网格框架材料与钉子材料的硬度均大于熔丝材料的硬度，并且网格框架材料以及钉子材料的熔点均小于熔丝增材材料的熔点，从而使得网格框架与钉子随着熔丝增材的进行而逐渐熔化，最后与电弧熔丝增材层结合为整体。本发明的模具强化方法是对模具进行电弧熔丝增材强化后再进行回火热处理。本发明能够增强增材区的强度与硬度，消除残余应力，提高模具的韧性。
The invention discloses a strengthening and additive process based on an arc fuse. Each fuse is added to form an arc fuse additive layer, and the arc fuse additive layer is hammered; 3 layers, just lay the grid frame; after laying the grid frame, hammer the grid frame to make the grid frame and the arc fuse additive layer fit; when laying the grid frame, on the arc fuse additive layer Welding nails to position the grid; the hardness of the grid frame material and the nail material are both greater than the hardness of the fuse material, and the melting points of the grid frame material and the nail material are both lower than the melting point of the fuse additive material, so that the grid frame The nails gradually melt with the fuse additive process, and finally combine with the arc fuse additive layer as a whole. The mold strengthening method of the present invention is to carry out the arc fuse additive strengthening on the mold and then carry out tempering heat treatment. The invention can enhance the strength and hardness of the additive zone, eliminate residual stress, and improve the toughness of the mold.
Description
Technical Field
The invention relates to the technical field of die processing.
Background
The die needs to be repaired when worn, especially a large die. Arc fuse additive processes are commonly used in mold repair. The arc fuse wire material increase process generally adopts an arc fuse wire to increase materials, the arc fuse wire material increase is carried out layer by layer, and due to insufficient welding strength, the arc fuse wire material increase layers are stripped, and the strength of a material increase area is insufficient.
Disclosure of Invention
Aiming at the technical defects, the invention provides an enhanced material adding process based on an arc fuse, and solves the technical problem of how to improve the strength of an additive area.
In order to solve the technical problem, the invention provides an enhanced additive process based on an arc fuse, which comprises the following steps of:
hammering the arc fuse wire additive layer to flatten the surface of the arc fuse wire additive layer when each fuse wire additive layer forms an arc fuse wire additive layer;
each electric arc fuse wire additive layer comprises 2-3 electric arc fuse wire additive layers, a grid frame is laid on the electric arc fuse wire additive layer on the uppermost layer, and each time of lapping is horizontally rotated relative to the last lapping
(ii) a Hammering the grid frame after the grid frame is laid so that the grid frame is attached to the arc fuse additive layer;
the hardness of the grid framework material is greater than that of the fuse wire material, and the melting point of the grid framework material is less than that of the fuse wire material, so that the grid framework is gradually melted along with the fuse wire additive and finally integrated with the arc fuse wire additive layer.
Further, when the grid framework is laid, nails are welded on the arc fuse additive layer to position the grid;
the hardness of the grid frame material and the hardness of the nail material are both greater than that of the fuse wire material, and the melting points of the grid frame material and the nail material are both less than that of the fuse wire additive material, so that the grid frame and the nail are gradually melted along with the fuse wire additive material and are finally combined with the arc fuse wire additive layer into a whole.
Further, the fuse wire material is nickel-based alloy or iron-based alloy; the grid framework and the nail are made of high-alloy structural steel.
Furthermore, the hammering reduction of the arc fuse additive layer is 5-8 mm each time; the hammering acting force on the grid is between the minimum force for achieving the attaching effect and the maximum force for ensuring the integrity of the grid; the hammer insertion temperature range is 20-550 ℃.
The invention also provides a die strengthening method, and the arc fuse wire material increasing process based on the arc fuse wire is adopted to perform arc fuse wire material increasing on the part to be strengthened of the die or perform arc fuse wire material increasing on the whole surface of the die to form a strengthening region.
Compared with the prior art, the invention has the advantages that:
1. the invention utilizes the temperature of the arc fuse additive layer to melt the grid in the process of arc fuse additive material addition, thereby leading the grid frame and the arc fuse additive layer to be fused into a whole.
2. Hammering the arc fuse additive layer can not only enable the surface of the arc fuse additive layer to be smooth so as to facilitate lapping, but also play a stress eliminating effect, reduce the residual stress of the arc fuse additive layer and improve the strength of the arc fuse additive layer.
3. The mesh is laid by rotating the mesh, so that the nodes on the mesh are distributed relatively uniformly, and the shear can be effectively resisted when the whole die is subjected to the action of a shear force, thereby improving the strength and the hardness of the die.
4. The nails are melted together with the grid framework and fused with the arc fuse additive layer into a whole in the fuse additive process while positioning the grid, so that the strength of a positioning area is further enhanced; particularly, when the nail is welded on the arc fuse wire additive layer corresponding to a region with larger die abrasion, the intensity of the arc fuse wire additive layer corresponding to the region with larger die abrasion can be enhanced, and the arc fuse wire additive layer is more smooth.
5. The material of the arc fuse additive layer can be selected from nickel-based alloy or iron-based alloy, so that the added arc fuse additive layer has good strength, and the selection range of the material of the arc fuse additive layer is expanded.
6. According to the die strengthening method, tempering heat treatment is carried out after the electric arc fuse wire is subjected to material increase, so that stable tempered martensite is obtained, the effect of improving the structure stability is achieved, the die does not generate structure transformation in the using process, the geometric dimension and the performance of the die tend to be stable, the internal stress can be eliminated, and the toughness is improved.
Drawings
FIG. 1 is a schematic view of staggered lapping;
FIG. 2 is a schematic view of the welding of the nail;
FIG. 3 is a schematic structural view of a lattice frame;
FIG. 4 is a schematic view of peening a grid framework laid over an arc fuse additive layer;
FIG. 5 is a simulation of a pressurization experiment performed after a screen is applied to an arc fuse additive layer;
fig. 6 is a simulation of a pressurization experiment performed on an ungrid arc fuse additive layer.
Detailed Description
For a new mold, a material increase strengthening area can be reserved in a local part in advance, and then material increase strengthening treatment is carried out by the method; and for the failed die, after the failed part is cleaned, the method is used for additive strengthening treatment.
In a failure die, arc fuse additive strengthening is only needed in a local area where abrasion is generated for a large die, and arc fuse additive strengthening can be performed on the whole die surface for a small die. In the embodiment, the die subjected to the electric arc fuse material additive strengthening is further subjected to tempering heat treatment to obtain stable tempered martensite so as to achieve the effect of improving the structure stability, so that the die does not generate structure transformation in the using process, the geometric dimension and the performance of the die tend to be stable, the internal stress can be eliminated, and the toughness is improved. The arc fuse additive process and the tempering heat treatment are described below.
An enhanced additive process based on an arc fuse, comprising the steps of:
hammering the arc fuse wire additive layer to flatten the surface of the arc fuse wire additive layer when each fuse wire additive layer forms an arc fuse wire additive layer;
referring to fig. 1, for each 2-3 arc fuse additive layers 1, a grid frame 2 is laid on the uppermost arc fuse additive layer, and each time the net is laid, the net is horizontally rotated relative to the previous net, and the net is laid
(ii) a After the grid frame 2 is laid, hammering the grid frame 2 to enable the grid frame 2 to be attached to the arc fuse additive layer; the hardness of the grid frame 2 material is greater than the fuse material and the melting point of the grid frame 2 material is less than the melting point of the fuse material, so that the grid frame 2 gradually melts as the fuse additive progresses and is finally integrated with the arc fuse additive layer.
In this embodiment, the horizontal rotation angle of the lapping is 0 to 90 degrees, e.g., 30 degrees. The mesh is laid by rotating the mesh, so that the nodes on the mesh are distributed relatively uniformly, and the shear can be effectively resisted when the whole die is subjected to the action of a shear force, thereby improving the strength and the hardness of the die.
When the arc fuse wire is used for material increase, the diameter range of the fuse wire is 0.5-3.0 mm; the fuse material can be selected from nickel-based alloy or iron-based alloy according to requirements. The effect that regional whole reached of vibration material disk after the hammering: the residual stress is small, and the surface is smooth. The added arc fuse has good strength and expands the selection range of the materials of the added arc fuse layer.
Setting parameters of the arc fuse during material adding and hammering: arc fuse additive current: 400A; arc fuse additive voltage 32V; hammering pressure: 0.1-0.5 mpa; arc fuse material increase speed: 500 mm/min; hammering intervention temperature: 20-550 ℃; moving speed of the hammering head: 1000-2000 mm/min.
In order to prevent the grid framework 2 from sliding during the material increase of the arc fuse, nails are welded on the additive layer of the arc fuse to position the grid when the grid framework 2 is laid; the hardness of the grid framework 2 material and the nail material are both higher than that of the fuse wire material, and the melting points of the grid framework 2 material and the nail material are both lower than that of the fuse wire additive material, so that the grid framework 2 and the nails are gradually melted along with the fuse wire additive material and finally are integrated with the arc fuse wire additive layer.
Referring to fig. 2, more than one nail may be welded on the arc fuse additive layer corresponding to a region of greater die wear; for a new mold, reserving a material increase strengthening area in a local part in advance, and then determining the number of nails and welding positions according to the size of the mold; reinforcing a local area of a failed large-scale die, and welding a nail on the arc fuse additive layer; for overall arc fuse additive strengthening of small failed dies, the nail welding on the arc fuse additive layer corresponds to a region of greater die wear.
The nails are melted together with the grid framework 2 in the fuse wire additive process and are fused into a whole with the arc fuse wire additive layer while positioning the grid, so that the strength of a positioning area is further enhanced; particularly, when the nail is welded on the arc fuse wire additive layer corresponding to a region with larger die abrasion or a region with higher stress concentration degree, the intensity of the arc fuse wire additive layer corresponding to the die abrasion region and the stress concentration region can be enhanced, and the arc fuse wire additive layer is more smooth.
The high alloy structural steel grid frame 2 is printed by a 3D printer, as shown in figure 3, the length = width = a =300mm of the grid, a plurality of small squares are arranged in the grid, the side length of each small square is 37.45mm, the squares are separated by grid wires, and the diameter of each grid wire is 0.1 mm. In addition, the grid frame 2 can cover the wear area of the mold during reinforcement. The data is entered into the printer before 3D printing. The grid frame 2 is printed and laid on the surface for the next arc fuse build-up. While a nail of about 0.1mm diameter and about 0.5mm length was printed from the same raw material (high alloy structural steel).
The 3D printing method, the embedding of the grid frame 2 and the nails, the inputting of the electric arc fuse wire additive parameters, and the hammering after the electric arc fuse wire additive is added each time and the grid frame 2 is laid and the nails are welded, so that the quality and the precision of a welding part are improved.
The hammering reduction of the arc fuse additive layer is 5-8 mm each time. Referring to fig. 4, the hammering force on the grid frame 2 is between the minimum force for achieving the bonding effect and the maximum force for ensuring the integrity of the grid, and the hammering intervention temperature range is 20-550 ℃, so that the grid frame 2 can be well bonded with the arc fuse additive layer.
In order to verify the stress resistance effect of the expanded arc fuse additive layer, simulation is performed by Deform software, and the simulation result is shown in FIGS. 5 and 6, wherein both the graphs are the expanded arc fuse additive layer with the same material and thickness, the difference is that only the grid frame 2 is added in FIG. 5, and the grid frame is not added in FIG. 6. Then, the same stress is applied (i.e. the pressure of the fuse additive layers on the two figures is the same), and the fuse additive layer with the grid is found to resist the stress without deformation, while the fuse additive layer without the grid is directly flattened, thereby drawing the conclusion that the grid can resist certain stress.
After the arc fuse wire is added with materials, a strengthening area is formed on the part (stress concentration or abrasion area) to be strengthened of the mould or the whole surface of the mould; and then, forming tempered martensite on the die and the strengthening region through a tempering heat treatment process. The fuse wire material is nickel-based alloy or iron-based alloy, and the grid framework 2 and the nails are both made of high-alloy structural steel, so that the hardness of the strengthening area can be higher than that of the die.
The tempering heat treatment process comprises the following steps:
first stress relief tempering: after the arc fuse wire material increase is finished, immediately returning to the furnace to heat, wherein the charging temperature is less than or equal to 450 ℃, the heating time is 0.4h, and the heating temperature is 500-550 ℃; the heat preservation time is determined by the heat preservation time of 1h per 50mm of the maximum geometric size;
slow cooling for the first time: placing in a heat-preservation sand pit, measuring the temperature by using an infrared thermometer at about 180 ℃ for 12 hours or longer;
secondary stress relief tempering: after the first slow cooling is finished, immediately returning to the furnace and raising the temperature, wherein the technological parameters are the same as those of the first stress relief tempering;
and (3) slow cooling for the second time: after the secondary stress relief tempering, placing the product in a heat-preservation sand pit, measuring the temperature by using an infrared thermometer at about 180 ℃ for 12 hours or more;
air cooling: and after the second slow cooling is finished, the temperature is about 180 ℃, and the steel is air-cooled to room temperature in the air to obtain stable tempered martensite.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011315049.8A CN112453421B (en) | 2020-11-20 | 2020-11-20 | Reinforced material adding process based on arc fuse and mold reinforcing method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011315049.8A CN112453421B (en) | 2020-11-20 | 2020-11-20 | Reinforced material adding process based on arc fuse and mold reinforcing method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112453421A true CN112453421A (en) | 2021-03-09 |
| CN112453421B CN112453421B (en) | 2021-07-20 |
Family
ID=74799997
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011315049.8A Active CN112453421B (en) | 2020-11-20 | 2020-11-20 | Reinforced material adding process based on arc fuse and mold reinforcing method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112453421B (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013140147A1 (en) * | 2012-03-19 | 2013-09-26 | Bae Systems Plc | Additive layer manufacturing |
| US20140190942A1 (en) * | 2011-08-10 | 2014-07-10 | Bae Systems Plc | Forming a layered structure |
| EP2962789A2 (en) * | 2014-06-30 | 2016-01-06 | General Electric Company | Additive manufacturing methods and systems with fiber reinforcement |
| CN106216862A (en) * | 2016-07-20 | 2016-12-14 | 华中科技大学 | A kind of composite manufacturing method and device subtracting material based on electric arc increasing material and high energy beam current |
| CN107206500A (en) * | 2015-03-19 | 2017-09-26 | 哈里伯顿能源服务公司 | Netted reinforcement used in metal-base composites instrument |
| GB2553097A (en) * | 2016-08-18 | 2018-02-28 | Bae Systems Plc | Additive layer manufacturing |
| CN108340047A (en) * | 2018-02-08 | 2018-07-31 | 西安增材制造国家研究院有限公司 | A method of electric arc increasing material manufacturing almag structural member is strengthened in hammering |
| CN109874320A (en) * | 2015-08-31 | 2019-06-11 | 纯净新世界有限公司 | The increasing material manufacturing method of the enhancing of manufacture for composite material |
| CN110153350A (en) * | 2019-06-24 | 2019-08-23 | 重庆大学 | A large hot forging die and its manufacturing method |
| CN111151746A (en) * | 2019-12-31 | 2020-05-15 | 上海交通大学 | Additive manufacturing method of titanium matrix composites for self-generated ultrafine mesh structure reinforcements |
-
2020
- 2020-11-20 CN CN202011315049.8A patent/CN112453421B/en active Active
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140190942A1 (en) * | 2011-08-10 | 2014-07-10 | Bae Systems Plc | Forming a layered structure |
| WO2013140147A1 (en) * | 2012-03-19 | 2013-09-26 | Bae Systems Plc | Additive layer manufacturing |
| EP2962789A2 (en) * | 2014-06-30 | 2016-01-06 | General Electric Company | Additive manufacturing methods and systems with fiber reinforcement |
| CN107206500A (en) * | 2015-03-19 | 2017-09-26 | 哈里伯顿能源服务公司 | Netted reinforcement used in metal-base composites instrument |
| CN109874320A (en) * | 2015-08-31 | 2019-06-11 | 纯净新世界有限公司 | The increasing material manufacturing method of the enhancing of manufacture for composite material |
| CN106216862A (en) * | 2016-07-20 | 2016-12-14 | 华中科技大学 | A kind of composite manufacturing method and device subtracting material based on electric arc increasing material and high energy beam current |
| GB2553097A (en) * | 2016-08-18 | 2018-02-28 | Bae Systems Plc | Additive layer manufacturing |
| CN108340047A (en) * | 2018-02-08 | 2018-07-31 | 西安增材制造国家研究院有限公司 | A method of electric arc increasing material manufacturing almag structural member is strengthened in hammering |
| CN110153350A (en) * | 2019-06-24 | 2019-08-23 | 重庆大学 | A large hot forging die and its manufacturing method |
| CN111151746A (en) * | 2019-12-31 | 2020-05-15 | 上海交通大学 | Additive manufacturing method of titanium matrix composites for self-generated ultrafine mesh structure reinforcements |
Non-Patent Citations (2)
| Title |
|---|
| 何智等: "超声冲击电弧增材制造钛合金零件的各向异性研究 ", 《航天制造技术》 * |
| 权国政: "电弧熔丝单层单道积材残余应力模拟分析及锤击消除研究", 《材料导报》 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN112453421B (en) | 2021-07-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP4819183B2 (en) | Rail welded portion cooling method, rail welded portion cooling device, and rail welded joint | |
| US9199345B2 (en) | Method for producing a metal reinforcement for a turbine engine blade | |
| EP2753451B1 (en) | Isothermal structural repair of superalloy components including turbine blades | |
| JP6311969B2 (en) | Die for hot forging and hot forging method | |
| US9273562B2 (en) | Projection resistance welding of superalloys | |
| CN109079420A (en) | A kind of casting defect removing method | |
| EP2347850B1 (en) | A method of restoring a metallic component | |
| CN110180983A (en) | A kind of profile-followed reticular structure hot forged mould of type cavity surface layer and preparation method thereof | |
| CN113953624A (en) | Steel part crack welding repair method | |
| JP3934679B2 (en) | Cutting die and method for manufacturing the same | |
| CN112453421B (en) | Reinforced material adding process based on arc fuse and mold reinforcing method | |
| CN100389924C (en) | P91 steel welding method | |
| CN108213304B (en) | A large-scale hot forging die with a fist-type bionic structure and its manufacturing method | |
| JP5693075B2 (en) | Manufacturing method of bent product and combustor | |
| CN107470849A (en) | Mould corrosion location renovation technique | |
| CN112548104B (en) | Method for reducing hot cracking sensitivity in die steel laser additive repair process | |
| JP2007175707A (en) | Method of improving fatigue strength in rail weld zone | |
| KR102762989B1 (en) | Method for performing maintenance in bucket tenon welding of turbine | |
| CN100443242C (en) | Welding and deformation control method of large scale bulb tubular set and base | |
| JPH08155642A (en) | Overlay welding repair method for hot die | |
| KR102348528B1 (en) | Method of manufacturing clad steel plate | |
| CN109420837A (en) | Method for preventing welding cracks of high-carbon steel vacuum electron beam welding | |
| KR20240097311A (en) | Repair welding method of iron and steel making facility | |
| KR20240015900A (en) | Method for performing maintenance in bucket tenon welding of turbine | |
| CN117548983A (en) | Axle forging anvil repair welding method |
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 | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230830 Address after: 048000 Mishan Industrial Park, Gaoping economic and Technological Development Zone, Gaoping City, Jincheng City, Shanxi Province Patentee after: Kangshuo (Shanxi) Low Stress Manufacturing System Technology Research Institute Co.,Ltd. Address before: 230000 floor 1, building 2, phase I, e-commerce Park, Jinggang Road, Shushan Economic Development Zone, Hefei City, Anhui Province Patentee before: Dragon totem Technology (Hefei) Co.,Ltd. Effective date of registration: 20230830 Address after: 230000 floor 1, building 2, phase I, e-commerce Park, Jinggang Road, Shushan Economic Development Zone, Hefei City, Anhui Province Patentee after: Dragon totem Technology (Hefei) Co.,Ltd. Address before: 400044 No. 174 Sha Jie street, Shapingba District, Chongqing Patentee before: Chongqing University |