CN108638599A - Monocrystaline silicon stove Carbon fibe crucible knitted body and preparation method thereof - Google Patents
Monocrystaline silicon stove Carbon fibe crucible knitted body and preparation method thereof Download PDFInfo
- Publication number
- CN108638599A CN108638599A CN201810345962.9A CN201810345962A CN108638599A CN 108638599 A CN108638599 A CN 108638599A CN 201810345962 A CN201810345962 A CN 201810345962A CN 108638599 A CN108638599 A CN 108638599A
- Authority
- CN
- China
- Prior art keywords
- carbon fibe
- knitted body
- crucible
- cloth
- net tire
- 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.)
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims abstract description 60
- 229910052799 carbon Inorganic materials 0.000 title claims abstract description 60
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 title claims abstract description 17
- 229910052710 silicon Inorganic materials 0.000 title claims abstract description 17
- 239000010703 silicon Substances 0.000 title claims abstract description 17
- 238000002360 preparation method Methods 0.000 title claims abstract description 14
- 239000004744 fabric Substances 0.000 claims abstract description 68
- 239000003610 charcoal Substances 0.000 claims abstract description 35
- 238000004804 winding Methods 0.000 claims abstract description 20
- 150000001875 compounds Chemical class 0.000 claims description 6
- 238000007493 shaping process Methods 0.000 claims description 6
- 239000002131 composite material Substances 0.000 claims description 4
- 239000002994 raw material Substances 0.000 claims description 4
- 238000009730 filament winding Methods 0.000 claims description 3
- 239000000463 material Substances 0.000 abstract description 5
- 239000010410 layer Substances 0.000 description 19
- 239000002344 surface layer Substances 0.000 description 2
- 238000009941 weaving Methods 0.000 description 2
- 238000002679 ablation Methods 0.000 description 1
- 238000009954 braiding Methods 0.000 description 1
- CREMABGTGYGIQB-UHFFFAOYSA-N carbon carbon Chemical compound C.C CREMABGTGYGIQB-UHFFFAOYSA-N 0.000 description 1
- 239000011203 carbon fibre reinforced carbon Substances 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000005137 deposition process Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/022—Non-woven fabric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B1/00—Layered products having a non-planar shape
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/02—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by a sequence of laminating steps, e.g. by adding new layers at consecutive laminating stations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/18—Handling of layers or the laminate
- B32B38/1808—Handling of layers or the laminate characterised by the laying up of the layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/06—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B35/00—Apparatus not otherwise provided for, specially adapted for the growth, production or after-treatment of single crystals or of a homogeneous polycrystalline material with defined structure
- C30B35/002—Crucibles or containers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/10—Fibres of continuous length
- B32B2305/20—Fibres of continuous length in the form of a non-woven mat
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/544—Torsion strength; Torsion stiffness
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Textile Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Physical Vapour Deposition (AREA)
Abstract
The invention discloses a kind of monocrystaline silicon stove Carbon fibe crucible knitted bodies, including the knitted body ontology being centered around on core model, the knitted body ontology includes internal layer, middle level and outer layer from inside to outside, the internal layer includes plain weave charcoal cloth and Carbon fibe net tire with the outer layer, the middle level includes laminated cloth and Carbon fibe net tire, and the plain weave charcoal cloth, the laminated cloth and the equal continuous winding of Carbon fibe net tire are on the core model.The present invention uses above-mentioned monocrystaline silicon stove Carbon fibe crucible knitted body and preparation method thereof, can greatly improve the intensity of crucible, improve the service life of crucible, while can reduce cost of material and processing cost.
Description
Technical field
The present invention relates to crucible knitted body technical fields, more particularly to a kind of monocrystaline silicon stove Carbon fibe crucible knitted body
And preparation method thereof.
Background technology
Carbon carbon composite has the function of resistance to ablation, highly thermally conductive, low-expansion coefficient etc., extensively as a kind of new material
Applied to fields such as photovoltaic, aerospaces.Currently, the weaving manner of crucible knitted body replaces laying using charcoal cloth, net tire, then
It is pierced by circumferentially continuous winding, radial needle.This weaving cannot form the disconnected winding of continuous nothing, in the head of every layer of charcoal cloth
Occur connecing stubble at tail, cause the crucible after deposition process during thermal field of single crystal furnace use, by external force extruding while repeatedly
It uses, causes crucible that longitudinal fracture occurs in use for some time, shorten the service life of product.
Invention content
The object of the present invention is to provide a kind of monocrystaline silicon stove Carbon fibe crucible knitted bodies and preparation method thereof, can be significantly
The intensity for improving crucible, improves the service life of crucible, while can reduce cost of material and processing cost.
To achieve the above object, the present invention provides a kind of monocrystaline silicon stove Carbon fibe crucible knitted bodies, including are centered around
Knitted body ontology on core model, the knitted body ontology includes sequentially connected from inside to outside internal layer, middle level and outer layer, described
Internal layer includes compound plain weave charcoal cloth and Carbon fibe net tire with the outer layer, and the middle level includes laminated cloth and Carbon fibe net
Tire, the plain weave charcoal cloth, the laminated cloth and the equal continuous winding of Carbon fibe net tire are on the core model.
Preferably, the laminated cloth is that circumferential direction is wrapped on the core model.
Preferably, the plain weave charcoal cloth and the Carbon fibe net tire are pierced by needle and are connected, the Carbon fibe net tire and described
Composite joint is pierced by needle between laminated cloth.
A kind of monocrystaline silicon stove preparation method of Carbon fibe crucible knitted body, includes the following steps:
(1) early-stage preparations:The structure and size of machine-shaping crucible as needed, determine the knot for needing machine-shaping knitted body
Structure and size are separately woven into plain weave charcoal cloth and Carbon fibe net tire using Carbon fibe as raw material;It requires to count according to the size of knitted body
It calculates total winding number of plies and carries out continous way winding to calculate required plain weave charcoal cloth, laminated cloth and Carbon fibe net tire total length;
(2) continuous winding:The knitted body ontology includes from inside to outside internal layer, middle level and outer layer, and internal layer and outer layer include
Plain weave charcoal cloth and Carbon fibe net tire, middle level include close paved Carbon fibe net tire and laminated cloth successively;
Plain weave charcoal cloth is wrapped on the core model of crucible shape, Carbon fibe net tire, plain weave charcoal cloth and Carbon fibe are then laid with
Net tire is pierced compound by radial needle;
When knitted body ontology is routed to certain wall thickness, increase the long filament circumferential direction winding of laminated cloth, i.e., in knitted body ontology
Wall thickness centre position increases laminated cloth filament winding.
Preferably, it when the plain weave charcoal cloth, the laminated cloth and the Carbon fibe net tire are pierced into the hand-manipulating of needle, needs to ensure concentric
Degree is consistent, to prevent the appearance of metaboly.
Therefore, the present invention uses above-mentioned monocrystaline silicon stove Carbon fibe crucible knitted body and preparation method thereof, can carry significantly
The intensity of high crucible improves the service life of crucible, while can reduce cost of material and processing cost.In crucible knitted body ontology
Between increase the long filament circumferential direction winding of laminated cloth, on the one hand can increase the anti-pultrusion intensity of circumferential direction of product, while can be to avoid table
There is running phenomenon in layer, improves the service life of product.
Below by embodiment, technical scheme of the present invention will be described in further detail.
Specific implementation mode
Embodiments of the present invention are described further below.
A kind of monocrystaline silicon stove Carbon fibe crucible knitted body, including the knitted body ontology that is centered around on core model, knitted body sheet
Body includes internal layer, middle level and outer layer from inside to outside, and internal layer includes compound plain weave charcoal cloth and Carbon fibe net tire with outer layer, is put down
Line charcoal cloth and Carbon fibe net tire are pierced by needle to be connected.Middle level includes laminated cloth and Carbon fibe net tire, plain weave charcoal cloth, Carbon fibe net tire
Composite joint is pierced by needle between laminated cloth.Plain weave charcoal cloth, laminated cloth and the equal continuous winding of Carbon fibe net tire are on core model.It is flat
When line charcoal cloth, laminated cloth and Carbon fibe net tire are pierced into the hand-manipulating of needle, need to ensure that concentricity is consistent, to prevent the appearance of metaboly.
For laminated cloth between plain weave charcoal cloth and Carbon fibe net tire, laminated cloth is that circumferential direction is wrapped on core model.Crucible knitted body
The long filament circumferential direction winding for increasing laminated cloth among ontology, on the one hand can increase the anti-pultrusion intensity of circumferential direction of product, while can be with
It avoids surface layer from running phenomenon occur, improves the service life of product.
A kind of monocrystaline silicon stove preparation method of Carbon fibe crucible knitted body, includes the following steps:
(1) early-stage preparations:The structure and size of machine-shaping crucible as needed, determine the knot for needing machine-shaping knitted body
Structure and size are separately woven into plain weave charcoal cloth and Carbon fibe net tire using Carbon fibe as raw material;It requires to count according to the size of knitted body
It calculates total winding number of plies and carries out continous way winding to calculate required plain weave charcoal cloth, laminated cloth and Carbon fibe net tire total length;
(2) continuous winding:Knitted body ontology includes from inside to outside internal layer, middle level and outer layer, and internal layer and outer layer include plain weave
Charcoal cloth and Carbon fibe net tire, middle level include close paved Carbon fibe net tire and laminated cloth successively;
Plain weave charcoal cloth is wrapped on the core model of crucible shape, Carbon fibe net tire, plain weave charcoal cloth and Carbon fibe are then laid with
Net tire is pierced compound by radial needle;
When knitted body ontology is routed to certain wall thickness, increase the long filament circumferential direction winding of laminated cloth, i.e., in knitted body ontology
Wall thickness centre position increases laminated cloth filament winding.
The inner and outer surface layers of phase after processing, knitted body ontology can be cut off, if surfaces externally and internally continues growing plain weave charcoal cloth
Circumferential direction winding, after machining, there is long filament in crucible knitted body surfaces externally and internally, can cause running phenomenon.The present invention is in knitted body sheet
Add one layer of laminated cloth needle thorn braiding when body middle level, the waste of raw material not only can be reduced, while can avoid running occur
Phenomenon.Woven according to such method, crucible monocrystal thermal-field using when by original 50-60 stoves can be increased to 80 stoves a left side
The right side improves the service life of crucible.
Therefore, the present invention uses above-mentioned monocrystaline silicon stove Carbon fibe crucible knitted body and preparation method thereof, can carry significantly
The intensity of high crucible improves the service life of crucible, while can reduce cost of material and processing cost.
Finally it should be noted that:The above embodiments are merely illustrative of the technical solutions of the present invention rather than is limited,
Although the present invention is described in detail with reference to preferred embodiments, it will be understood by those of ordinary skill in the art that:Its according to
Technical scheme of the present invention can be so modified or replaced equivalently, and these modifications or equivalent replacement cannot also make to repair
Technical solution after changing is detached from the spirit and scope of technical solution of the present invention.
Claims (5)
1. a kind of monocrystaline silicon stove Carbon fibe crucible knitted body, it is characterised in that:Including the knitted body ontology being centered around on core model,
The knitted body ontology includes sequentially connected from inside to outside internal layer, middle level and outer layer, and the internal layer is wrapped with the outer layer
Include compound plain weave charcoal cloth and Carbon fibe net tire, the middle level includes laminated cloth and Carbon fibe net tire, the plain weave charcoal cloth, described
Laminated cloth and the equal continuous winding of Carbon fibe net tire are on the core model.
2. a kind of monocrystaline silicon stove according to claim 1 Carbon fibe crucible knitted body, it is characterised in that:The laminated cloth
It is wrapped on the core model for circumferential direction.
3. a kind of monocrystaline silicon stove according to claim 1 Carbon fibe crucible knitted body, it is characterised in that:The plain weave charcoal
Cloth and the Carbon fibe net tire are pierced by needle to be connected, and is led between the plain weave charcoal cloth, the Carbon fibe net tire and the laminated cloth
Cross needle thorn composite joint.
4. a kind of preparation method of monocrystaline silicon stove Carbon fibe crucible knitted body as described in claim 1, which is characterized in that packet
Include following steps:
(1) early-stage preparations:The structure and size of machine-shaping crucible as needed, determine need the structure of machine-shaping knitted body with
Size is separately woven into plain weave charcoal cloth and Carbon fibe net tire using Carbon fibe as raw material;It requires to calculate according to the size of knitted body total
The number of plies is wound, to calculate required plain weave charcoal cloth, laminated cloth and Carbon fibe net tire total length, carries out continous way winding;
(2) continuous winding:The knitted body ontology includes from inside to outside internal layer, middle level and outer layer, and internal layer and outer layer include plain weave
Charcoal cloth and Carbon fibe net tire, middle level include close paved Carbon fibe net tire and laminated cloth successively;
Plain weave charcoal cloth is wrapped on the core model of crucible shape, one layer of Carbon fibe net tire, plain weave charcoal cloth and Carbon fibe are then covered
Net tire is pierced compound by radial needle;
When knitted body ontology is routed to certain wall thickness, increase the long filament circumferential direction winding of laminated cloth, i.e., in knitted body ontology wall thickness
Centre position increases laminated cloth filament winding.
5. a kind of preparation method of monocrystaline silicon stove Carbon fibe crucible knitted body according to claim 4, it is characterised in that:
When the plain weave charcoal cloth, the laminated cloth and the Carbon fibe net tire are pierced into the hand-manipulating of needle, need to ensure that concentricity is consistent, to prevent from becoming
The appearance of shape phenomenon.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201810345962.9A CN108638599A (en) | 2018-04-18 | 2018-04-18 | Monocrystaline silicon stove Carbon fibe crucible knitted body and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201810345962.9A CN108638599A (en) | 2018-04-18 | 2018-04-18 | Monocrystaline silicon stove Carbon fibe crucible knitted body and preparation method thereof |
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CN108638599A true CN108638599A (en) | 2018-10-12 |
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CN201810345962.9A Withdrawn CN108638599A (en) | 2018-04-18 | 2018-04-18 | Monocrystaline silicon stove Carbon fibe crucible knitted body and preparation method thereof |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111002435A (en) * | 2019-12-19 | 2020-04-14 | 保定顺天新材料股份有限公司 | Weaving process of carbon-carbon crucible preform for monocrystalline silicon furnace |
CN114455965A (en) * | 2021-12-30 | 2022-05-10 | 西安超码科技有限公司 | Containing alpha-Al2O3Coated C/SiC composite crucible |
CN114560715A (en) * | 2022-04-28 | 2022-05-31 | 浙江德鸿碳纤维复合材料有限公司 | Crucible supporting rod and preparation method thereof |
CN114919202A (en) * | 2022-03-15 | 2022-08-19 | 云路复合材料(上海)有限公司 | Method for weaving carbon fiber composite material crucible preformed body and integrally forming carbon fiber composite material crucible preformed body and base |
WO2023124269A1 (en) * | 2021-12-30 | 2023-07-06 | 隆基绿能科技股份有限公司 | High-temperature-resistant carbon-carbon composite body and production method therefor, and carbon fiber prefab |
-
2018
- 2018-04-18 CN CN201810345962.9A patent/CN108638599A/en not_active Withdrawn
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111002435A (en) * | 2019-12-19 | 2020-04-14 | 保定顺天新材料股份有限公司 | Weaving process of carbon-carbon crucible preform for monocrystalline silicon furnace |
CN114455965A (en) * | 2021-12-30 | 2022-05-10 | 西安超码科技有限公司 | Containing alpha-Al2O3Coated C/SiC composite crucible |
WO2023124269A1 (en) * | 2021-12-30 | 2023-07-06 | 隆基绿能科技股份有限公司 | High-temperature-resistant carbon-carbon composite body and production method therefor, and carbon fiber prefab |
CN114455965B (en) * | 2021-12-30 | 2023-09-05 | 西安超码科技有限公司 | A composition containing alpha-Al 2 O 3 Coated C/SiC composite crucible |
CN114919202A (en) * | 2022-03-15 | 2022-08-19 | 云路复合材料(上海)有限公司 | Method for weaving carbon fiber composite material crucible preformed body and integrally forming carbon fiber composite material crucible preformed body and base |
CN114560715A (en) * | 2022-04-28 | 2022-05-31 | 浙江德鸿碳纤维复合材料有限公司 | Crucible supporting rod and preparation method thereof |
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