CN117282968B - High-flux preparation method and device for high-temperature alloy block - Google Patents
High-flux preparation method and device for high-temperature alloy block Download PDFInfo
- Publication number
- CN117282968B CN117282968B CN202311578107.XA CN202311578107A CN117282968B CN 117282968 B CN117282968 B CN 117282968B CN 202311578107 A CN202311578107 A CN 202311578107A CN 117282968 B CN117282968 B CN 117282968B
- Authority
- CN
- China
- Prior art keywords
- temperature alloy
- alloy block
- blocks
- block
- static pressure
- 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
- 239000000956 alloy Substances 0.000 title claims abstract description 146
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 142
- 238000002360 preparation method Methods 0.000 title claims abstract description 30
- 238000009413 insulation Methods 0.000 claims abstract description 53
- 229910052751 metal Inorganic materials 0.000 claims abstract description 38
- 230000003068 static effect Effects 0.000 claims abstract description 38
- 239000002184 metal Substances 0.000 claims abstract description 37
- 239000011812 mixed powder Substances 0.000 claims abstract description 37
- 238000010438 heat treatment Methods 0.000 claims abstract description 32
- 238000000034 method Methods 0.000 claims abstract description 32
- 238000001816 cooling Methods 0.000 claims abstract description 30
- 230000008569 process Effects 0.000 claims abstract description 30
- 229910000601 superalloy Inorganic materials 0.000 claims description 19
- 238000004321 preservation Methods 0.000 claims description 17
- 238000003825 pressing Methods 0.000 claims description 14
- 238000000465 moulding Methods 0.000 claims description 11
- 238000007906 compression Methods 0.000 claims description 8
- 230000006835 compression Effects 0.000 claims description 7
- 229910000975 Carbon steel Inorganic materials 0.000 claims description 6
- 239000000378 calcium silicate Substances 0.000 claims description 6
- 229910052918 calcium silicate Inorganic materials 0.000 claims description 6
- OYACROKNLOSFPA-UHFFFAOYSA-N calcium;dioxido(oxo)silane Chemical compound [Ca+2].[O-][Si]([O-])=O OYACROKNLOSFPA-UHFFFAOYSA-N 0.000 claims description 6
- 239000010962 carbon steel Substances 0.000 claims description 6
- 239000000835 fiber Substances 0.000 claims description 6
- 239000005995 Aluminium silicate Substances 0.000 claims 2
- PZZYQPZGQPZBDN-UHFFFAOYSA-N aluminium silicate Chemical compound O=[Al]O[Si](=O)O[Al]=O PZZYQPZGQPZBDN-UHFFFAOYSA-N 0.000 claims 2
- 229910000323 aluminium silicate Inorganic materials 0.000 claims 2
- 235000012211 aluminium silicate Nutrition 0.000 claims 2
- 238000012545 processing Methods 0.000 abstract description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- 238000001513 hot isostatic pressing Methods 0.000 description 5
- YKTSYUJCYHOUJP-UHFFFAOYSA-N [O--].[Al+3].[Al+3].[O-][Si]([O-])([O-])[O-] Chemical compound [O--].[Al+3].[Al+3].[O-][Si]([O-])([O-])[O-] YKTSYUJCYHOUJP-UHFFFAOYSA-N 0.000 description 4
- 230000004907 flux Effects 0.000 description 4
- 230000005855 radiation Effects 0.000 description 4
- 230000017525 heat dissipation Effects 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- 102000004169 proteins and genes Human genes 0.000 description 3
- 108090000623 proteins and genes Proteins 0.000 description 3
- 230000002706 hydrostatic effect Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- TVEXGJYMHHTVKP-UHFFFAOYSA-N 6-oxabicyclo[3.2.1]oct-3-en-7-one Chemical compound C1C2C(=O)OC1C=CC2 TVEXGJYMHHTVKP-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 239000000110 cooling liquid Substances 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010353 genetic engineering Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
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
- B22F3/12—Both compacting and sintering
- B22F3/14—Both compacting and sintering simultaneously
- B22F3/15—Hot isostatic pressing
-
- 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
- B22F3/003—Apparatus, e.g. furnaces
-
- 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
- B22F3/005—Loading or unloading powder metal objects
-
- 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
- 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
- B22F3/12—Both compacting and sintering
- B22F3/14—Both compacting and sintering simultaneously
- B22F3/15—Hot isostatic pressing
- B22F2003/153—Hot isostatic pressing apparatus specific to HIP
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Powder Metallurgy (AREA)
Abstract
The invention belongs to the technical field of high-temperature alloy material processing, and particularly relates to a high-throughput preparation method and device for a high-temperature alloy block. The method comprises the following steps: step S1: adding metal mixed powder into a high-flux forming die of a high-temperature alloy block in a vacuum chamber, and vacuumizing the vacuum chamber; step S2: the high-temperature alloy block high-flux forming die is subjected to die assembly, static pressure and heating, so that metal mixed powder is formed into a high-temperature alloy block; step S3: opening a high-flux forming die of the high-temperature alloy block, and jacking up the high-temperature alloy block; step S4: the vacuum manipulator places the high-temperature alloy blocks into the gradient cooling area one by one; step S5: sleeving a heat insulation sleeve on each high-temperature alloy block by the vacuum manipulator; step S6: and carrying out different heat treatment processes on each high-temperature alloy block through the gradient cooling area, and finally obtaining a plurality of high-temperature alloy blocks with different grain sizes. The invention can efficiently obtain high-temperature alloy blocks with different grain sizes, realizes high-flux preparation of the high-temperature alloy blocks, and has high efficiency and low cost.
Description
Technical Field
The invention belongs to the technical field of high-temperature alloy material processing, and particularly relates to a high-throughput preparation method and device for a high-temperature alloy block.
Background
At present, in the high-temperature alloy material processing industry, alloy blocks are prepared by genetic engineering of vacuum, isothermal and static pressure high-temperature alloy materials at high flux, and the heat treatment process, the establishment of a vacuum environment, the high temperature and the static pressure time are long. In one production cycle, M rows by N columns of high-temperature alloy blocks are prepared by M rows by N columns of process cycles, and the problems of low working efficiency and high production cost exist. Meanwhile, in the processing process, the cooling effect is poor. Therefore, it is necessary to design a high-throughput preparation method and device for high-temperature alloy blocks.
Disclosure of Invention
Aiming at the problems, the invention aims to provide a high-flux preparation method and a device for high-temperature alloy blocks, which effectively realize gradient heat treatment of metal mixed powder, can efficiently obtain high-temperature alloy blocks with different grain sizes, and realize high-flux preparation of the high-temperature alloy blocks with high efficiency and low cost.
In order to achieve the above purpose, the present invention adopts the following technical scheme:
the invention provides a high-flux preparation method of a high-temperature alloy block, which comprises the following steps:
step S1: adding metal mixed powder into a high-flux forming die of a high-temperature alloy block in a vacuum chamber, and vacuumizing the vacuum chamber;
step S2: the high-temperature alloy block high-flux forming die is subjected to die assembly, static pressure and heating, so that metal mixed powder is formed into a high-temperature alloy block;
step S3: opening a high-flux forming die of the high-temperature alloy block, and jacking up the high-temperature alloy block;
step S4: the vacuum manipulator places the high-temperature alloy blocks into the gradient cooling area one by one;
step S5: sleeving a heat insulation sleeve on each high-temperature alloy block by the vacuum manipulator;
step S6: and carrying out different heat treatment processes on each high-temperature alloy block through the gradient cooling area, and finally obtaining a plurality of high-temperature alloy blocks with different grain sizes.
In one possible implementation manner, the gradient cooling area includes a cold plate and a plurality of thermal insulation stacks arranged on the cold plate in a gradient manner, each thermal insulation stack is formed by stacking different numbers of thermal insulation blocks along the height direction, and one high-temperature alloy block is placed on the top of each thermal insulation stack.
In one possible implementation, the thermal insulation block is made of aluminum silicate fiber; the heat insulation sleeve is made of microporous calcium silicate plates; the cold plate is made of carbon steel.
In one possible implementation, in step S1, metal mixed powder is added into each groove of a hot static pressure die of the high-temperature alloy block high-throughput forming die;
in step S2, the high-throughput molding die of the superalloy block descends through a compression bar and provides static pressure for the metal mixed powder in each groove of the hot static pressure die, and simultaneously heats the metal mixed powder through the compression bar, the hot static pressure die and a jacking rod positioned at the bottom of the hot static pressure die;
in step S3, the high-temperature alloy block high-throughput molding die lifts the high-temperature alloy block through a lifting rod.
The invention also provides a high-flux preparation device for the high-temperature alloy blocks, which comprises a vacuum chamber, a high-flux forming die for the high-temperature alloy blocks, a vacuum mechanical arm and a gradient cooling zone, wherein the high-flux forming die for the high-temperature alloy blocks is arranged in the vacuum chamber, and a plurality of high-temperature alloy blocks are obtained by carrying out static pressure, heating and forming on metal mixed powder; the vacuum manipulator is used for conveying the high-temperature alloy blocks into a gradient cooling area, and the gradient cooling area is used for completing different heat treatment processes of each high-temperature alloy block, so that each high-temperature alloy block has different grain sizes finally.
In one possible implementation manner, the high-throughput molding die of the high-temperature alloy block comprises a compression bar, a hot static pressure die and a lifting rod, wherein the upper surface of the hot static pressure die is provided with a plurality of grooves for adding metal mixed powder with different components, and the bottom of each groove is provided with the lifting rod capable of lifting;
the pressing rods are arranged right above the hot static pressure die and correspond to the grooves one by one, the pressing rods can be lifted, and static pressure can be provided for metal mixed powder in the grooves when the pressing rods are lifted.
In one possible implementation, the metal mixed powder in the groove is heated by the pressing rod, the hot hydrostatic die and the jacking rod.
In one possible implementation manner, the gradient cooling zone comprises a cold plate and a plurality of heat preservation stacks arranged on the cold plate in a gradient arrangement, wherein one high-temperature alloy block is placed on the top of each heat preservation stack, and a heat insulation sleeve is sleeved on each high-temperature alloy block.
In one possible implementation, each of the stacks is formed by stacking a different number of thermal blocks in the height direction.
In one possible implementation, the thermal insulation block is made of aluminum silicate fiber; the heat insulation sleeve is made of microporous calcium silicate plates; the cold plate is made of carbon steel.
The invention has the advantages and beneficial effects that: the high-flux preparation method of the high-temperature alloy block provided by the invention effectively realizes gradient heat treatment of metal mixed powder, can efficiently obtain high-temperature alloy blocks with different grain sizes, and realizes high-flux preparation of the high-temperature alloy block, and has high efficiency and low cost.
The high-flux preparation device for the high-temperature alloy blocks provided by the invention has the advantages that the structure is simple, the realization is easy, M rows by N columns of high-temperature alloy blocks can be obtained in one process cycle, the heat treatment process of each high-temperature alloy block is different, the high-flux preparation device accords with the high flux of genetic material engineering, each heat treatment completed in one process flow has the difference, and the application range is wide.
According to the invention, the high-temperature alloy block is shielded through the heat insulation sleeve in a vacuum environment, no heat radiation and no heat convection are generated, and only the heat conduction of the high-temperature alloy block is effectively realized through the heat insulation block and the cold plate, so that the heat treatment process of the high-temperature alloy block is more accurate.
According to the invention, a series of process actions are completed in the vacuum environment in the vacuum chamber by the vacuum manipulator, so that the automation degree is high, and the manual error rate is reduced.
Additional features and advantages of the invention will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention. The objectives and other advantages of the invention may be realized and attained by the structure particularly pointed out in the written description and drawings.
The technical scheme of the invention is further described in detail through the drawings and the embodiments.
Drawings
The accompanying drawings are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate the invention and together with the embodiments of the invention, serve to explain the invention. In the drawings:
FIG. 1 is an isometric view of a high throughput preparation apparatus for superalloy blocks in accordance with the present invention;
FIG. 2 is a schematic diagram of a high-throughput forming die for forming a high-temperature alloy block to finish hot static pressure forming of the high-temperature alloy block;
FIG. 3 is a schematic illustration of the heat treatment process of the high temperature alloy block in the gradient cooling zone of the present invention.
In the figure: the high-temperature alloy block forming device comprises a 1-vacuum chamber, a 101-vacuum door, a 2-vacuum manipulator, a 3-high-temperature alloy block high-throughput forming die, 301-compression bars, 302-hot static pressure dies, 303-jacking bars, 304-grooves, 4-high-temperature alloy blocks, 5-cold plates, 6-heat insulation blocks and 7-heat insulation sleeves.
Detailed Description
In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present invention.
Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present invention, the meaning of "a plurality" is two or more, unless explicitly defined otherwise.
In the present invention, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art according to the specific circumstances.
The preferred embodiments of the present invention will be described below with reference to the accompanying drawings, it being understood that the preferred embodiments described herein are for illustration and explanation of the present invention only, and are not intended to limit the present invention.
An embodiment of the invention provides a high-throughput preparation method of high-temperature alloy blocks, wherein a plurality of high-temperature alloy blocks are obtained in one process cycle, and the heat treatment process of each high-temperature alloy block is different. Referring to FIG. 1, the high-throughput preparation method of the high-temperature alloy block comprises the following steps:
step S1: adding metal mixed powder into a high-temperature alloy block high-flux forming die 3 in a vacuum chamber 1, and vacuumizing the vacuum chamber 1;
step S2: the high-flux forming die 3 of the high-temperature alloy block is subjected to die assembly, static pressure and heating, so that metal mixed powder is formed into a high-temperature alloy block 4;
step S3: the high-flux forming die 3 of the high-temperature alloy block is opened, and the high-temperature alloy block 4 is lifted;
step S4: the vacuum manipulator 2 places the high-temperature alloy blocks 4 one by one into the gradient cooling area;
step S5: the vacuum manipulator 2 is sleeved with a heat insulation sleeve 7 on each high-temperature alloy block 4;
step S6: and (3) carrying out different heat treatment processes on each high-temperature alloy block 4 through a gradient cooling area, and finally obtaining a plurality of high-temperature alloy blocks 4 with different grain sizes.
Referring to fig. 3, in the embodiment of the present invention, the gradient cooling zone includes a cold plate 5 and a plurality of thermal insulation stacks arranged on the cold plate 5 in a gradient arrangement, each thermal insulation stack is formed by stacking different numbers of thermal insulation blocks 6 along the height direction, a high temperature alloy block 4 is placed on the top of each thermal insulation stack, and a thermal insulation sleeve 7 is sleeved on each high temperature alloy block 4. Specifically, the number of the heat preservation blocks 6 in the heat preservation stack is selected according to the characteristics of the high-temperature alloy blocks 4, so that the adjustment is convenient, and the application range is wide.
Preferably, the heat preservation block 6 is made of aluminum silicate fiber products, has the temperature resistance of 1000 ℃ and the heat conductivity coefficient of 0.035W/(m.K); the heat insulation sleeve 7 is made of microporous calcium silicate plates, and has the temperature resistance of 1300 ℃ and the heat conductivity coefficient of 0.174W/(m.K); the cold plate 5 is made of Q235B high-quality carbon steel, has heat resistance of 1000 ℃, has a heat conductivity coefficient of 34.89 KW/(m.c), and is preferably used for bearing the heat insulation block 6 in vacuum on the upper surface and refrigerating the lower surface by a heat exchanger.
In the embodiment of the invention, the number of the heat insulation blocks 6 in each heat insulation pile is different, the heat resistance of the heat insulation blocks 6 is larger than that of the high-temperature alloy blocks 4, the heat insulation blocks 6 can cover the lower surface of the high-temperature alloy blocks 4, the high-temperature alloy blocks 4 only contain a heat conduction cooling mode, and the vacuum environment of the vacuum chamber 1 cuts off the heat convection cooling mode of the high-temperature alloy blocks 4. The heat insulation sleeve 7 can cover the upper surface and the side of the superalloy block 4, effectively blocks heat radiation and heat dissipation of the superalloy block 4, has larger thermal resistance than the heat insulation block 6, and the cold plate 5 can quickly transfer heat to the outside of the vacuum chamber 1 and maintain constant temperature.
Referring to fig. 2, in the embodiment of the present invention, in step S1, metal mixed powder is added into each groove of the hot isostatic pressing mold 302 of the superalloy block high-throughput molding mold 3; in step S2, the superalloy block high-throughput molding die 3 is lowered by the pressing rod 301 and provides static pressure for the metal mixed powder in each groove of the hot isostatic pressing die 302, and at the same time, the metal mixed powder is heated by the pressing rod 301, the hot isostatic pressing die 302 and the jacking rod 303 located at the bottom of the hot isostatic pressing die 302. In step S3, the superalloy block high-throughput molding die 3 lifts the superalloy block 4 by the lift rod 303.
According to the high-flux preparation method of the high-temperature alloy blocks, M rows and N columns of high-temperature alloy blocks are obtained in one process cycle, the heat treatment process of each high-temperature alloy block is different, the high-flux preparation method accords with the high flux of genetic material engineering, and each heat treatment completed in one process flow has a difference.
The high-flux preparation method of the high-temperature alloy block provided by the invention effectively realizes gradient heat treatment of metal mixed powder, can efficiently obtain high-temperature alloy blocks with different grain sizes, and realizes high-flux preparation of the high-temperature alloy block, and has high efficiency and low cost.
Referring to fig. 1, another embodiment of the present invention provides a high-flux preparation device for high-temperature alloy blocks, which includes a vacuum chamber 1, a high-flux forming mold 3 for high-temperature alloy blocks disposed in the vacuum chamber 1, a vacuum manipulator 2, and a gradient cooling zone, wherein the high-flux forming mold 3 for high-temperature alloy blocks obtains a plurality of high-temperature alloy blocks 4 by static pressure, heating and forming of metal mixed powder; the vacuum manipulator 2 is used for conveying the high-temperature alloy blocks 4 into a gradient cooling zone, and the gradient cooling zone is used for completing different heat treatment processes of each high-temperature alloy block 4, so that each high-temperature alloy block 4 has different grain sizes finally.
Referring to fig. 2, in the embodiment of the invention, a high-temperature alloy block high-throughput forming mold 3 comprises a compression bar 301, a hot static pressure mold 302 and a lifting rod 303, wherein the upper surface of the hot static pressure mold 302 is provided with M rows by N columns of grooves 304, the number of M and N is equal to or greater than 3, metal mixed powder with different components can be added into each groove 304, and the lifting rod 303 capable of lifting is arranged at the bottom of each groove 304. The pressing rods 301 are disposed right above the hot static pressure mold 302 and correspond to the grooves 304 one by one, the pressing rods 301 can be lifted, and static pressure can be provided for the metal mixed powder in the grooves 304 when the pressing rods 301 descend.
In this embodiment, the metal mixed powder in the groove 304 is heated by the pressing rod 301, the hot static pressure die 302 and the jacking rod 303, and the high-throughput molding die 3 for high-temperature alloy blocks effectively completes high-throughput molding of M rows by N columns of high-temperature alloy blocks 4.
Referring to fig. 3, in the embodiment of the invention, the gradient cooling area includes a cold plate 5 and M rows by N columns of heat insulation stacks arranged on the cold plate 5 in a gradient arrangement, the number of M, N is 3 or more, a high-temperature alloy block 4 is placed on top of each heat insulation stack, and a heat insulation sleeve 7 is sleeved on each high-temperature alloy block 4. The gradient cooling area effectively completes the high-flux heat treatment process of M rows by N columns of high-temperature alloy blocks 4.
In the embodiment of the invention, each heat insulation pile is formed by stacking different numbers of heat insulation blocks 6 along the height direction, so that the heights of the heat insulation piles are different, and different heat treatment processes can be realized.
Preferably, the heat preservation block 6 is made of aluminum silicate fiber products, has the temperature resistance of 1000 ℃ and the heat conductivity coefficient of 0.035W/(m.K); the heat insulation sleeve 7 is made of microporous calcium silicate plates, and has the temperature resistance of 1300 ℃ and the heat conductivity coefficient of 0.174W/(m.K); the cold plate 5 is made of Q235B high-quality carbon steel, has heat resistance of 1000 ℃, has a heat conductivity coefficient of 34.89 KW/(m.c), and is preferably used for bearing the heat insulation block 6 in vacuum on the upper surface and refrigerating the lower surface by a heat exchanger.
The high-flux preparation device for the high-temperature alloy block provided by the other embodiment of the invention comprises the following working procedures:
step S1: after the vacuum door 101 of the vacuum chamber 1 is opened, the top of the lift rod 303 is placed at the bottom of the recess 304 of the hot isostatic pressing mold 302. Placing metal mixed powder with different components into M rows and N columns of grooves 304;
step S2: after the vacuum door 101 of the vacuum chamber 1 is closed and sealed, the vacuum chamber 1 is evacuated. The plurality of pressure rods 301 descend and the bottoms of the pressure rods are pressed downwards from the upper parts of the grooves 304 to provide static pressure for the metal mixed powder in the grooves 304, and meanwhile, the pressure rods 301, the hot static pressure die 302 and the jacking rod 303 heat the metal mixed powder, so that the metal mixed powder is prepared to form a high-temperature alloy block 4;
step S3: lifting and resetting the pressure lever 301, and lifting the lifting lever 303 to lift the superalloy block 4;
step S4: the vacuum manipulator 2 places M rows by N columns of high-temperature alloy blocks 4 on corresponding M rows by N columns of heat preservation stacks one by one;
step S5: the vacuum manipulator 2 places heat insulation sleeves 7 one by one on each high-temperature alloy block 4;
step S6: under each superalloy block 4, the amount of heat transferred from each superalloy block 4 to the cold plate 5 is different due to the different number of insulation blocks 6 in the insulation stack, i.e. the heat treatment process of each superalloy block 4 is different;
step S7: finally obtaining M rows by N columns of high-temperature alloy blocks 4 with different heat treatment processes, wherein the grain sizes of each high-temperature alloy block 4 are different.
In the embodiment of the invention, the vacuum manipulator 2 is preferably a four-degree-of-freedom vacuum manipulator, and one of the vacuum manipulators clamps the side surface of the superalloy block 4 or the heat insulation sleeve 7; secondly, horizontally advancing and retreating; thirdly, horizontally moving leftwards and rightwards; fourth, the height direction rises and falls.
In the embodiment of the present invention, the metal mixed powder is in different grooves 304 of the hot hydrostatic die 302, and the total mass and volume are equal, but the metal elements are different. For example, each superalloy block 4 contains 12 elements of titanium, aluminum, magnesium, nickel, and the like. But each element has a different ratio. For example, one groove 304 contains 2.37% of nickel and the other groove 304 contains 4.61% of nickel, so that M rows by N columns of superalloy blocks 4 are prepared, and the material properties of each superalloy block 4 are different.
In the embodiment of the invention, the number of the heat preservation blocks 6 in each heat preservation stack is different by M rows and N columns, the heat resistance of the heat preservation blocks 6 is larger than that of the high-temperature alloy block 4, and the heat preservation blocks 6 can cover the lower surface of the high-temperature alloy block 4. The high-temperature alloy block 4 only contains a heat conduction cooling mode, and the vacuum environment of the vacuum chamber 1 cuts off a heat convection heat dissipation mode of the high-temperature alloy block 4. The heat insulation sleeve 7 can cover the upper surface and the side surface of the high-temperature alloy block 4, effectively blocks the heat radiation and the heat dissipation of the high-temperature alloy block 4, and the heat resistance of the heat insulation sleeve 7 is larger than that of the heat insulation block 6. The cold plate 5 can quickly transfer heat to the outside of the vacuum chamber 1 and maintain constant temperature, and concretely, the conventional engineering implementation consists of a liquid storage tank, a cooling liquid pump, a cooling pipe, a vacuum through-wall sealing plug, a temperature sensor, a radiator and the like, and the principle is an industrial air conditioner.
According to the invention, the high-temperature alloy block 4 is shielded through the heat insulation sleeve 7 in a vacuum environment, no heat radiation and no heat convection are generated, and the heat insulation block 6 and the cold plate 5 effectively enable the high-temperature alloy block 4 to have heat conduction, so that the heat treatment process of the high-temperature alloy block 4 is more accurate. A series of process actions are completed in the vacuum environment in the vacuum chamber 1 through the vacuum manipulator 2, so that the automation degree is high, and the manual error rate is reduced.
According to the high-flux preparation device for the high-temperature alloy blocks, M rows and N columns of high-temperature alloy blocks are obtained in one process cycle, the heat treatment process of each high-temperature alloy block is different, the high-flux preparation device accords with the high flux of genetic material engineering, and each heat treatment completed in one process flow has the difference, so that the high-flux preparation of the high-temperature alloy blocks is realized.
It will be apparent to those skilled in the art that various modifications and variations can be made to the present invention without departing from the spirit or scope of the invention. Thus, it is intended that the present invention also include such modifications and alterations insofar as they come within the scope of the appended claims or the equivalents thereof.
Claims (4)
1. The high-flux preparation method of the high-temperature alloy block is characterized by comprising the following steps of:
step S1: adding metal mixed powder into a high-temperature alloy block high-flux forming die (3) in a vacuum chamber (1), and vacuumizing the vacuum chamber (1);
step S2: the high-temperature alloy block high-flux forming die (3) is subjected to die assembly, static pressure and heating, so that metal mixed powder is formed into a high-temperature alloy block (4);
step S3: the high-temperature alloy block high-flux forming die (3) is opened, and the high-temperature alloy block (4) is lifted;
step S4: the vacuum mechanical arm (2) places the high-temperature alloy blocks (4) into the gradient cooling area one by one;
step S5: the vacuum manipulator (2) is sleeved with a heat insulation sleeve (7) on each high-temperature alloy block (4);
step S6: carrying out different heat treatment processes on each high-temperature alloy block (4) through a gradient cooling zone to finally obtain a plurality of high-temperature alloy blocks (4) with different grain sizes;
the gradient cooling zone comprises a cold plate (5) and a plurality of heat preservation stacks which are arranged on the cold plate (5) in a gradient arrangement, each heat preservation stack is formed by stacking different numbers of heat preservation blocks (6) along the height direction, and the top of each heat preservation stack is provided with one high-temperature alloy block (4);
in the step S1, adding metal mixed powder into each groove of a hot static pressure die (302) of the high-temperature alloy block high-flux forming die (3);
in step S2, the high-throughput molding die (3) of the superalloy block descends through the compression bar (301) and provides static pressure for the metal mixed powder in each groove of the hot static pressure die (302), and simultaneously heats the metal mixed powder through the compression bar (301), the hot static pressure die (302) and the jacking rod (303) positioned at the bottom of the hot static pressure die (302);
in step S3, the high-temperature alloy block high-throughput molding die (3) lifts the high-temperature alloy block (4) through the lifting rod (303).
2. The high-throughput preparation method of superalloy blocks according to claim 1, wherein the thermal insulation block (6) is an aluminium silicate fiber product; the heat insulation sleeve (7) is made of a microporous calcium silicate plate; the cold plate (5) is made of carbon steel.
3. The high-flux preparation device for the high-temperature alloy blocks is characterized by comprising a vacuum chamber (1), a high-flux forming die (3) for the high-temperature alloy blocks, a vacuum mechanical arm (2) and a gradient cooling zone, wherein the high-flux forming die (3) for the high-temperature alloy blocks is used for obtaining a plurality of high-temperature alloy blocks (4) by carrying out static pressure, heating and forming on metal mixed powder; the vacuum manipulator (2) is used for conveying the high-temperature alloy blocks (4) into a gradient cooling area, and the gradient cooling area is used for completing different heat treatment processes of the high-temperature alloy blocks (4), so that the high-temperature alloy blocks (4) have different grain sizes finally;
the high-throughput molding die (3) for the high-temperature alloy block comprises a compression bar (301), a hot static pressure die (302) and a jacking rod (303), wherein a plurality of grooves (304) for adding metal mixed powder with different components are formed in the upper surface of the hot static pressure die (302), and the jacking rod (303) capable of lifting is arranged at the bottom of each groove (304); the pressing rods (301) are arranged right above the hot static pressure die (302) and correspond to the grooves (304) one by one, the pressing rods (301) can be lifted, and static pressure can be provided for metal mixed powder in the grooves (304) when the pressing rods (301) are lifted; the metal mixed powder in the groove (304) is heated through the pressing rod (301), the hot static pressure die (302) and the jacking rod (303);
the gradient cooling zone comprises a cold plate (5) and a plurality of heat preservation stacks which are arranged on the cold plate (5) in a gradient arrangement, the top of each heat preservation stack is provided with one high-temperature alloy block (4), and a heat insulation sleeve (7) is sleeved on each high-temperature alloy block (4);
each heat insulation pile is formed by stacking different numbers of heat insulation blocks (6) along the height direction.
4. A high throughput preparation apparatus of superalloy blocks according to claim 3, characterised in that the thermal block (6) is an aluminium silicate fibre product; the heat insulation sleeve (7) is made of a microporous calcium silicate plate; the cold plate (5) is made of carbon steel.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202311578107.XA CN117282968B (en) | 2023-11-24 | 2023-11-24 | High-flux preparation method and device for high-temperature alloy block |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202311578107.XA CN117282968B (en) | 2023-11-24 | 2023-11-24 | High-flux preparation method and device for high-temperature alloy block |
Publications (2)
Publication Number | Publication Date |
---|---|
CN117282968A CN117282968A (en) | 2023-12-26 |
CN117282968B true CN117282968B (en) | 2024-02-09 |
Family
ID=89253890
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202311578107.XA Active CN117282968B (en) | 2023-11-24 | 2023-11-24 | High-flux preparation method and device for high-temperature alloy block |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN117282968B (en) |
Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107101868A (en) * | 2017-06-14 | 2017-08-29 | 北京科技大学 | A kind of high flux forging thermal cycle simulation and method |
CN107695346A (en) * | 2017-11-23 | 2018-02-16 | 北京科技大学 | Powder metallurgic method high flux prepares the device and method with characterizing aluminum alloy materials |
CN108707731A (en) * | 2018-07-23 | 2018-10-26 | 昆明理工大学 | A kind of microwave high throughput prepares the device and method of alloy |
CN110592417A (en) * | 2019-09-27 | 2019-12-20 | 昆明贵金属研究所 | High-flux preparation method of sliding electric contact material with gradient distribution of components |
CN111579323A (en) * | 2020-05-09 | 2020-08-25 | 中国航发北京航空材料研究院 | High-throughput preparation and test method of powder superalloy inclusion sample |
CN112195356A (en) * | 2020-09-23 | 2021-01-08 | 北京科技大学 | High-flux preparation method of metal matrix composite material reinforced phase prefabricated blank for infiltration |
JP2021110031A (en) * | 2019-12-31 | 2021-08-02 | ウォンジン アルミニウム | Apparatus for producing high strength composite material |
CN113218744A (en) * | 2021-05-10 | 2021-08-06 | 烟台大学 | High-flux preparation method and device for backward extrusion gradient thermal deformation and gradient thermal treatment |
CN113234905A (en) * | 2021-05-10 | 2021-08-10 | 烟台大学 | High-flux preparation method and device for gradient thermal deformation and gradient thermal treatment |
CN114986970A (en) * | 2022-05-07 | 2022-09-02 | 昆明理工大学 | High-flux powder pressing control system and high-flux powder pressing method |
CN115958182A (en) * | 2023-01-13 | 2023-04-14 | 烟台大学 | High-temperature alloy forming device and method based on biological gene high-throughput engineering |
CN116393677A (en) * | 2023-04-07 | 2023-07-07 | 哈尔滨工业大学 | Method for preparing diamond/aluminum composite material by high-flux near-net forming |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109759594B (en) * | 2019-01-08 | 2020-09-11 | 钢铁研究总院 | Hot isostatic pressing high-flux micro-manufacturing method for composite material and sheath mold thereof |
-
2023
- 2023-11-24 CN CN202311578107.XA patent/CN117282968B/en active Active
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107101868A (en) * | 2017-06-14 | 2017-08-29 | 北京科技大学 | A kind of high flux forging thermal cycle simulation and method |
CN107695346A (en) * | 2017-11-23 | 2018-02-16 | 北京科技大学 | Powder metallurgic method high flux prepares the device and method with characterizing aluminum alloy materials |
CN108707731A (en) * | 2018-07-23 | 2018-10-26 | 昆明理工大学 | A kind of microwave high throughput prepares the device and method of alloy |
CN110592417A (en) * | 2019-09-27 | 2019-12-20 | 昆明贵金属研究所 | High-flux preparation method of sliding electric contact material with gradient distribution of components |
JP2021110031A (en) * | 2019-12-31 | 2021-08-02 | ウォンジン アルミニウム | Apparatus for producing high strength composite material |
CN111579323A (en) * | 2020-05-09 | 2020-08-25 | 中国航发北京航空材料研究院 | High-throughput preparation and test method of powder superalloy inclusion sample |
CN112195356A (en) * | 2020-09-23 | 2021-01-08 | 北京科技大学 | High-flux preparation method of metal matrix composite material reinforced phase prefabricated blank for infiltration |
CN113218744A (en) * | 2021-05-10 | 2021-08-06 | 烟台大学 | High-flux preparation method and device for backward extrusion gradient thermal deformation and gradient thermal treatment |
CN113234905A (en) * | 2021-05-10 | 2021-08-10 | 烟台大学 | High-flux preparation method and device for gradient thermal deformation and gradient thermal treatment |
CN114986970A (en) * | 2022-05-07 | 2022-09-02 | 昆明理工大学 | High-flux powder pressing control system and high-flux powder pressing method |
CN115958182A (en) * | 2023-01-13 | 2023-04-14 | 烟台大学 | High-temperature alloy forming device and method based on biological gene high-throughput engineering |
CN116393677A (en) * | 2023-04-07 | 2023-07-07 | 哈尔滨工业大学 | Method for preparing diamond/aluminum composite material by high-flux near-net forming |
Also Published As
Publication number | Publication date |
---|---|
CN117282968A (en) | 2023-12-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US7011510B2 (en) | Hot isostatic pressing apparatus and hot isostatic pressing method | |
US20100166903A1 (en) | Elevated temperature forming die apparatus | |
CN110094974B (en) | High-flux hot-pressing sintering device for modular combined material and using method thereof | |
CN101947617B (en) | Double-chamber high-temperature forging and forming device of TiAl intermetallic compound forge piece and method thereof | |
CN207702962U (en) | A kind of magnet vacuum sintering furnace | |
JP2016531074A (en) | How to make a glass product | |
CN117282968B (en) | High-flux preparation method and device for high-temperature alloy block | |
CN109111091A (en) | Graphite mold, 3D glass hot bending device and 3D glass hot bending method | |
CN110849145A (en) | Muffle furnace crucible frame for automatic production line and working method thereof | |
CN113400632A (en) | Hot stamping device and hot stamping method | |
CN219752141U (en) | Quartz crucible preparation system | |
CN113493904B (en) | High-temperature high-vacuum annealing furnace | |
CN202123667U (en) | Production device for polytetrafluoroethylene sealing rings | |
CN114951879A (en) | Low-temperature efficient vacuumizing sealing equipment and sealing process for vacuum cup | |
TWI813845B (en) | Lifting atmosphere sintering device | |
CN108300950A (en) | The preparation method and hot-working section formulating method of ZrCuNiAl block metal glass | |
CN210475046U (en) | Positive-pressure creep leveling furnace | |
CN203007337U (en) | Titanium and titanium alloy sheet stacking type bell type annealing furnace | |
CN209242914U (en) | For the molding graphite jig of 3D glass and 3D glass bending device | |
CN221259500U (en) | External heating type carbon tube furnace | |
CN104668500A (en) | Device and method for preparing aluminum/magnesium alloy semi-solid slurry | |
JPH0122144B2 (en) | ||
CN113134607A (en) | Lifting type atmosphere sintering device | |
CN206109452U (en) | Combination formula annealing stove with multilayer multiseriate stove courage level is arranged | |
CN201864556U (en) | High-vacuum ceramic LCC (leadless chip carrier) packaging device |
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 |