CN114919202A - Method for weaving carbon fiber composite material crucible preformed body and integrally forming carbon fiber composite material crucible preformed body and base - Google Patents
Method for weaving carbon fiber composite material crucible preformed body and integrally forming carbon fiber composite material crucible preformed body and base Download PDFInfo
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- 229920000049 Carbon (fiber) Polymers 0.000 title claims abstract description 157
- 239000004917 carbon fiber Substances 0.000 title claims abstract description 157
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 title claims abstract description 133
- 238000009941 weaving Methods 0.000 title claims abstract description 60
- 238000000034 method Methods 0.000 title claims abstract description 50
- 239000002131 composite material Substances 0.000 title claims abstract description 26
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 10
- 229910002804 graphite Inorganic materials 0.000 claims abstract description 9
- 239000010439 graphite Substances 0.000 claims abstract description 9
- 239000000835 fiber Substances 0.000 claims description 10
- 239000011148 porous material Substances 0.000 claims description 5
- 239000010453 quartz Substances 0.000 claims description 5
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 5
- 239000004744 fabric Substances 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 3
- 238000009940 knitting Methods 0.000 claims 15
- 238000000465 moulding Methods 0.000 abstract description 8
- 239000002994 raw material Substances 0.000 abstract description 4
- 238000009954 braiding Methods 0.000 description 10
- 229910021421 monocrystalline silicon Inorganic materials 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 7
- 238000001467 acupuncture Methods 0.000 description 5
- 238000004080 punching Methods 0.000 description 5
- 229920000742 Cotton Polymers 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 4
- 238000004804 winding Methods 0.000 description 4
- 229910021420 polycrystalline silicon Inorganic materials 0.000 description 3
- 238000005336 cracking Methods 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 230000003628 erosive effect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/712—Containers; Packaging elements or accessories, Packages
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Abstract
Description
技术领域technical field
本发明涉及用于生产或制作单晶硅或多晶硅的一种碳纤维复合材料预成型体,具体涉及一种碳纤维复材预成型体编织及与底座一体成型方法。The invention relates to a carbon fiber composite material preform used for producing or producing single crystal silicon or polycrystalline silicon, in particular to a method for weaving and integrally forming a carbon fiber composite material preform with a base.
背景技术Background technique
在单晶硅的制作中,一般采用直拉法(CZ法),即从熔体中沿竖直方向拉制单晶硅。单晶硅的制作过程中,有一个部件是石墨坩锅,它用来承载内部单晶硅。在高温作用下,石墨坩锅会出现龟裂、侵蚀失效等问题,导致坩埚无法满足正常的使用要求。而且,随着单晶硅的生长,晶体的直径逐渐增大,在晶体直径增大的过程中,伴随着热量的传递。单晶硅热容很高,导致热量传递时耗能增加,对坩埚的结构性能要求较高。In the production of single crystal silicon, the Czochralski method (CZ method) is generally used, that is, the single crystal silicon is pulled from the melt along the vertical direction. In the production process of single crystal silicon, one component is the graphite crucible, which is used to carry the inner single crystal silicon. Under the action of high temperature, the graphite crucible will have problems such as cracking, erosion and failure, so that the crucible cannot meet the normal use requirements. Moreover, with the growth of single-crystal silicon, the diameter of the crystal gradually increases, and in the process of increasing the diameter of the crystal, heat is transferred. Single crystal silicon has a high heat capacity, which leads to an increase in energy consumption during heat transfer, and requires higher structural performance of the crucible.
目前存在的坩埚预成型体制作方法一般采用缠绕方式进行,将碳纤维缠绕成坩埚的形状,然后进行树脂的浸渍,最终做成碳/碳纤维复材的坩埚。但是缠绕而成的预成型体在结构上容易存在应力集中的现象,导致坩埚的整体性能受到影响。The existing crucible preform manufacturing method generally adopts the winding method, and the carbon fiber is wound into the shape of the crucible, and then the resin is impregnated, and finally a carbon/carbon fiber composite crucible is made. However, the wound preform is prone to stress concentration in structure, which affects the overall performance of the crucible.
发明内容SUMMARY OF THE INVENTION
本发明要解决的技术问题是:缠绕而成的预成型体在结构上容易存在应力集中的现象,导致坩埚的整体性能受到影响。The technical problem to be solved by the present invention is: the preform formed by winding is prone to stress concentration phenomenon in structure, which causes the overall performance of the crucible to be affected.
为了解决上述技术问题,本发明的技术方案是提供了一种碳纤复材坩埚预成型体编织及与底座一体成型方法,其特征在于,包括以下步骤:In order to solve the above technical problems, the technical solution of the present invention is to provide a method for weaving and integrally forming a carbon fiber composite crucible preform with a base, which is characterized in that it includes the following steps:
根据坩埚预成型体的结构和尺寸要求,计算碳纤维编织层数;Calculate the number of carbon fiber braided layers according to the structure and size requirements of the crucible preform;
将坩埚底座与坩埚芯模一体编织成型,采用n根碳纤维沿坩埚芯模中心轴线编织计算得到的层数,坩埚底座与坩埚芯模在编织过程中一体成型;The crucible base and the crucible core mold are integrally woven and formed, and the number of layers calculated by weaving n carbon fibers along the central axis of the crucible core mold is used, and the crucible base and the crucible core mold are integrally formed during the weaving process;
编织过程中,坩埚底座与坩埚芯模表面采用碳纤维编织和网胎交替覆盖,编织完成后进行针刺;During the weaving process, the surface of the crucible base and the crucible core mold are alternately covered with carbon fiber weaving and mesh tires, and acupuncture is performed after the weaving is completed;
成型之前,将坩埚芯模从碳纤维中抽取出来,同时将强磁铁与编织过程夹持末端拆卸下来。Before forming, the crucible mandrel is extracted from the carbon fiber, and the strong magnet and the braiding process clamping end are removed at the same time.
优选的,n根碳纤维采用三维编织机进行往复编织的方法,坩埚预成型体芯模在三维编织机的编织环中沿坩埚中心轴线水平方向往复运动。Preferably, the n carbon fibers are reciprocatingly braided by a three-dimensional braiding machine, and the core mold of the crucible preform reciprocates along the horizontal direction of the central axis of the crucible in the braiding ring of the three-dimensional braiding machine.
优选的,所述n根碳纤维在沿着坩埚中心轴线编织的过程由三维编织机的运动决定。Preferably, the process of weaving the n carbon fibers along the central axis of the crucible is determined by the movement of the three-dimensional weaving machine.
优选的,所述n根碳纤维在沿着坩埚中心轴线编织过程中,随着编织层数的增加,纤维长度和厚度逐层增加。Preferably, during the weaving process of the n carbon fibers along the central axis of the crucible, as the number of braiding layers increases, the length and thickness of the fibers increase layer by layer.
优选的,在坩埚芯模表面编织一层碳纤维编织层再覆盖一层碳纤维网胎,碳纤维网胎相对于碳纤维编织层交替铺设,直至碳纤维编织层达到计算的碳纤维编织层数;该碳纤维网胎由碳纤维短纤制备,呈棉絮状,碳纤维网胎与碳纤维编织层的碳纤维交替,以减少编织物孔隙。Preferably, a layer of carbon fiber braided layer is woven on the surface of the crucible core mold and then covered with a layer of carbon fiber mesh tire, and the carbon fiber mesh tire is alternately laid relative to the carbon fiber braided layer until the carbon fiber braided layer reaches the calculated number of carbon fiber braided layers; the carbon fiber mesh tire is composed of The carbon fiber short fibers are prepared in the form of cotton wool, and the carbon fiber mesh tires alternate with the carbon fibers of the carbon fiber braid to reduce the porosity of the braid.
优选的,编织完成后,进行针刺,使碳纤维网胎与碳纤维编织层成为一体并保持相对稳定的形状。所述针刺即采用特殊的针扎入碳纤维网胎和碳纤维编织层,使碳纤维网胎的碳纤维与碳纤维编织层更好地交错。Preferably, after the weaving is completed, needle punching is performed, so that the carbon fiber mesh body and the carbon fiber braided layer are integrated and maintain a relatively stable shape. The acupuncture uses special needles to penetrate the carbon fiber mesh tire and the carbon fiber braided layer, so that the carbon fibers of the carbon fiber mesh tire and the carbon fiber braided layer are better interlaced.
优选的,所述坩埚底座采用石墨或石英材质作为内部材料,坩埚底座外部采用碳纤维编织覆盖在石墨或者石英表面。所述的碳纤维覆盖包含所述碳纤维编织层和所述碳纤维网胎,所述碳纤维编织层和所述碳纤维网胎在坩埚底座交替覆盖。Preferably, the crucible base is made of graphite or quartz as the inner material, and the outside of the crucible base is woven with carbon fibers to cover the graphite or quartz surface. The carbon fiber covering includes the carbon fiber braided layer and the carbon fiber mesh tire, and the carbon fiber braided layer and the carbon fiber mesh tire are alternately covered on the crucible base.
优选的,所述坩埚底座呈“工”字型,包括碗状下部以及碗状上部,碗状下部、碗状上部共同组成坩埚底座,便于所述碳纤维编织层和所述碳纤维网胎交错配合固定在一起。Preferably, the crucible base is in the shape of an "I", including a bowl-shaped lower part and a bowl-shaped upper part, and the bowl-shaped lower part and the bowl-shaped upper part together form the crucible base, so that the carbon fiber braided layer and the carbon fiber mesh tire are interlaced and fixed. together.
优选的,对所述坩埚预成型体进行编织时,在所述坩埚芯模和坩埚底座外部分别加放强磁铁,用以固定坩埚芯模和坩埚底座。所述的强磁铁有两个,一个安装在编织过程夹持末端的凹槽内,与编织过程夹持末端一起,另一个放置在碗状上部,两个强磁铁磁性相互吸引,从而保持稳定的形态。Preferably, when weaving the crucible preform, strong magnets are respectively placed outside the crucible core mold and the crucible base to fix the crucible core mold and the crucible base. There are two said strong magnets, one is installed in the groove of the clamping end of the weaving process, together with the clamping end of the weaving process, and the other is placed in the upper part of the bowl, the two strong magnets attract each other magnetically, so as to maintain a stable form.
优选的,所述的坩埚芯模在编织完成后需要取出,由于坩埚芯模和坩埚底座表面有碳纤维编织层和碳纤维网胎交替覆盖,坩埚芯模取出后有利于保持预成型体的形状。Preferably, the crucible core mold needs to be taken out after the weaving is completed. Since the surface of the crucible core mold and the crucible base are alternately covered with carbon fiber braided layers and carbon fiber mesh tires, the crucible core mold is beneficial to maintain the shape of the preform after taking out.
为了提高坩埚的性能,本发明采用碳纤维复材预成型体与底座一体的形式,将石墨底座与坩埚体一体编织成型,保证坩埚的底部具有足够的强度和耐热性能。从结构上解决了单晶硅在坩埚内高温熔化导致坩埚侵蚀、龟裂等现象,满足单晶硅或多晶硅生产的需要,而且节约了坩埚的制作成本,一体成型减少预成型体成型时间,提高了坩埚的制作效率。In order to improve the performance of the crucible, the present invention adopts the form of the carbon fiber composite preform and the base, and the graphite base and the crucible body are integrally woven to ensure that the bottom of the crucible has sufficient strength and heat resistance. Structurally, it solves the phenomenon of crucible erosion and cracking caused by high temperature melting of single crystal silicon in the crucible, which meets the needs of single crystal silicon or polycrystalline silicon production, and saves the production cost of the crucible. The crucible production efficiency.
与现有坩埚相比,本发明的碳纤复材坩埚预成型体编织及与底座一体成型方法能够提高坩埚表面碳纤包覆性,增强坩埚的强度,提高坩埚的使用寿命,同时可以降低原材料成本。坩埚体部采用碳纤沿坩埚中心轴线编织的方法,中间交替用网胎覆盖,网胎由一种碳纤维短纤制备,呈棉絮状,网胎与编织层碳纤维交替,有利于减少编织物孔隙。编织完成后,进行针刺,使网胎与编织层成为一体并保持相对稳定的形状。避免了缠绕制作的预成型体带来了坩埚各个方向强度不同的缺陷,同时提高表面碳纤的聚合力,使得坩埚预成型体的结构强度得到改善。采用一体成型的方法,增强了坩埚底座与坩埚体部的连接性能,提高了产品使用寿命。Compared with the existing crucible, the carbon fiber composite material crucible preform weaving and integral molding method with the base of the present invention can improve the coating of carbon fiber on the surface of the crucible, enhance the strength of the crucible, improve the service life of the crucible, and at the same time can reduce the cost of raw materials. The crucible body adopts the method of weaving carbon fibers along the central axis of the crucible, and the middle is alternately covered with a mesh. After the weaving is completed, needle punching is performed to make the mesh body and the woven layer integrated and maintain a relatively stable shape. The defect of different strengths in all directions of the crucible caused by the preform produced by winding is avoided, and at the same time, the cohesive force of the surface carbon fibers is improved, so that the structural strength of the crucible preform is improved. The integrated molding method is adopted to enhance the connection performance between the crucible base and the crucible body and improve the service life of the product.
附图说明Description of drawings
图1为碳纤复材坩埚预成型体的剖视图;1 is a cross-sectional view of a carbon fiber composite crucible preform;
图2为碳纤复材坩埚预成型体底部结构剖视图;2 is a cross-sectional view of the bottom structure of a carbon fiber composite crucible preform;
图3为碳纤复材坩埚预成型体及与底座一体成型编织过程示意图。Fig. 3 is a schematic diagram of the carbon fiber composite crucible preform and the integrated weaving process with the base.
图中:In the picture:
1.坩埚芯模,2.坩埚底座,3.碗状下部,4.碗状上部,5.碳纤维,6.编织过程夹持末端,7.强磁铁,8.编织环,9.三维编织机。1. Crucible mandrel, 2. Crucible base, 3. Bowl-shaped lower part, 4. Bowl-shaped upper part, 5. Carbon fiber, 6. Clamping end for braiding process, 7. Strong magnet, 8. Braiding ring, 9. 3D braiding machine .
具体实施方式Detailed ways
下面结合具体实施例,进一步阐述本发明。应理解,这些实施例仅用于说明本发明而不用于限制本发明的范围。此外应理解,在阅读了本发明讲授的内容之后,本领域技术人员可以对本发明作各种改动或修改,这些等价形式同样落于本申请所附权利要求书所限定的范围。The present invention will be further described below in conjunction with specific embodiments. It should be understood that these examples are only used to illustrate the present invention and not to limit the scope of the present invention. In addition, it should be understood that after reading the content taught by the present invention, those skilled in the art can make various changes or modifications to the present invention, and these equivalent forms also fall within the scope defined by the appended claims of the present application.
本发明公开了一种坩埚预成型体编织及与底座一体成型方法,能有效地提高单晶硅或多晶硅在制造过程中坩锅的使用寿命,所获得的坩埚预成型体包括坩埚芯模1、坩埚底座2、碳纤维5。坩埚芯模1以坩埚预成型体的中心轴线为中心,横截面为U型,环形布置。The invention discloses a method for weaving and integrally forming a crucible preform with a base, which can effectively improve the service life of the crucible in the manufacturing process of monocrystalline silicon or polycrystalline silicon. The obtained crucible preform comprises a
坩埚底座2采用石墨或石英材质作为内部材料,坩埚底座2外层采用碳纤维编织覆盖在石墨或者石英表面。所述的碳纤维覆盖包含碳纤维编织层和碳纤维网胎,碳纤维编织层和碳纤维网胎在坩埚底座交替覆盖。碳纤维底座2呈“工”字型,包括碗状下部3和碗状上部4。碳纤维5属于多层纤维,包含碳纤维编织层和碳纤维网胎交替的纤维覆盖层。在坩埚芯模表面编织一层碳纤维编织层,覆盖一层碳纤维网胎。碳纤维网胎由一种碳纤维制备,呈棉絮状,碳纤维网胎与碳纤维编织层的碳纤维交替,有利于减少编织物孔隙。编织完成后,进行针刺,使碳纤维网胎与碳纤维编织层成为一体并保持相对稳定的形状。The
本发明提供的坩埚预成型体编织及与底座一体成型的方法将坩埚芯模1与坩埚底部2连接在一起进行编织,一体成型方法能够增强坩埚底部2与坩埚芯模1之间的连接性能。坩埚预成型体采用碳纤维进行编织,碳纤维编织层与碳纤维网胎交替覆盖在坩埚芯模1与坩埚底座2表面,碳纤维编织层数和厚度符合要求后,采用针刺的工艺对碳纤维5进行针刺,改善碳纤维编织层与层之间的连接性能。碳纤维编织层之间增加碳纤维网胎,减少纤维之间的孔隙,能够提高坩埚表面的包覆性,保证同心度一致,从而防止编织完成后坩埚芯模1抽出导致坩埚预成型体发生形变。在坩埚芯模表面编织一层碳纤维编织层,覆盖一层碳纤维网胎。所述碳纤维网胎由一种碳纤维短纤制备,呈棉絮状,碳纤维网胎与编织层碳纤维交替,有利于减少编织物孔隙。编织完成后,进行针刺,使碳纤维网胎与碳纤维编织层成为一体并保持相对稳定的形状。The crucible preform weaving and integral molding method with the base provided by the present invention connects the
所述针刺即采用特殊的针扎入碳纤维网胎和碳纤维编织层,使碳纤维网胎的碳纤维与碳纤维编织层更好地交错。The acupuncture uses special needles to penetrate the carbon fiber mesh tire and the carbon fiber braided layer, so that the carbon fibers of the carbon fiber mesh tire and the carbon fiber braided layer are better interlaced.
编织过程夹持末端6开设有凹槽,强磁铁7有两个,一个安装在编织过程夹持末端的凹槽内,与编织过程夹持末端6一起,另一个放置在碗状上部4,两个强磁铁磁性相互吸引,从而保持稳定的形态。The clamping
本实施例公开的一种坩埚预成型体编织及与底座一体成型的方法,具体包括以下步骤:A method for weaving a crucible preform and forming it integrally with a base disclosed in this embodiment specifically includes the following steps:
步骤1、前期准备:根据坩埚的应用场景及结构尺寸,确定坩埚预成型体的结构与尺寸,以碳纤维为原料,计算编织厚度和层数;
步骤2、编织工作:将坩埚芯模1、坩埚底座2与编织过程夹持末端6通过强磁铁7固定,然后将编织过程夹持末端6安装在三维编织机9上。利用坩埚芯模1沿坩埚中心轴线通过编织环8往复编织运动,坩埚芯模1和坩埚底座2表面覆盖的碳纤维5包括碳纤维编织层和交替铺设的碳纤维网胎两种,编织一层碳纤维编织层,铺设一层碳纤维网胎。在编织过程中,坩埚芯模1沿方向一运动完成一个行程的编织后,在编织层上铺设一层碳纤维网胎,改变三维编织机9的牵引方向,坩埚芯模1沿与初始方向一相反的方向二运动,继续下一个行程的编织,编织完成后,再次铺设一层碳纤维网胎,循环往复,直至编织厚度达到步骤1的计算厚度。在编织过程中,在坩埚芯模表面编织一层碳纤维编织层,覆盖一层碳纤维网胎。所述碳纤维网胎由一种碳纤维短纤制备,呈棉絮状,碳纤维网胎与碳纤维编织层的碳纤维交替,有利于减少编织物孔隙。编织完成后,进行针刺,使碳纤维网胎与碳纤维编织层成为一体并保持相对稳定的形状。所述针刺即采用特殊的针扎入碳纤维网胎和碳纤维编织层,使碳纤维网胎的碳纤维与碳纤维编织层更好地交错。
步骤3、坩埚成型:对编织好的坩埚预成型体进行树脂成型。成型之前,将坩埚芯模1从碳纤维5中抽取出来,同时将强磁铁7与编织过程夹持末端拆卸下来。坩埚底座2被碳纤维包覆,留在碳纤维5内,一起成型。
在加工后期,编织预成型体本体的外侧会切除一部分,普通缠绕而成的坩埚预成型体可能会出现纤维脱离坩埚本部的现象,而本发明采用的碳纤复材坩埚预成型体编织及与底座一体成型方法能够有效避免这种现象的发生。In the later stage of processing, a part of the outer side of the braided preform body will be cut off, and the crucible preform formed by ordinary winding may have the phenomenon that the fibers are detached from the crucible body. The one-piece molding method can effectively avoid the occurrence of this phenomenon.
因此,本发明采用的复材坩埚预成型体编织及与底座一体成型方法,可以很大程度上提高坩埚的强度,节约坩埚预成型体原材料和加工成本,同时提高坩埚的使用寿命。Therefore, the method of weaving and integrally forming the composite crucible preform adopted in the present invention can greatly improve the strength of the crucible, save the raw material and processing cost of the crucible preform, and at the same time increase the service life of the crucible.
最后需要说明的是,以上实施并非限制而只是说明本发明的技术方案,本领域的专家和技术人员应当理解,在本发明的基础上进行方案修改或者技术替换,而不脱离本发明技术方案的精神和要求,其均应包含在本发明的权利要求范围之中。Finally, it should be noted that the above implementation is not a limitation but only illustrates the technical solution of the present invention. Experts and technicians in the field should understand that the solution modification or technical replacement can be carried out on the basis of the present invention without departing from the technical solution of the present invention. The spirit and requirements shall be included in the scope of the claims of the present invention.
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2024055392A1 (en) * | 2022-09-15 | 2024-03-21 | 南京航空航天大学 | Weaving and needling integrated preform formation method and preform formation device |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH10330185A (en) * | 1997-05-28 | 1998-12-15 | Toyo Tanso Kk | Crucible for pulling single crystal and its production |
JP2000290093A (en) * | 1999-04-09 | 2000-10-17 | Tokai Carbon Co Ltd | Carbon crucible for single crystal pulling |
WO2009024045A1 (en) * | 2007-08-21 | 2009-02-26 | Hunan Kingbo Carbon-Carbon Composites Co. Ltd | A c/c composite crucible and a producing method thereof |
CN202830218U (en) * | 2011-05-18 | 2013-03-27 | 科发伦材料株式会社 | Carbon fiber reinforced carbon composite crucible and composite cylinder component |
CN108638599A (en) * | 2018-04-18 | 2018-10-12 | 保定顺天新材料股份有限公司 | Monocrystaline silicon stove Carbon fibe crucible knitted body and preparation method thereof |
CN112028657A (en) * | 2020-08-03 | 2020-12-04 | 杭州卓导新材料有限公司 | Preparation method of carbon/carbon composite material crucible |
-
2022
- 2022-03-15 CN CN202210251154.2A patent/CN114919202A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH10330185A (en) * | 1997-05-28 | 1998-12-15 | Toyo Tanso Kk | Crucible for pulling single crystal and its production |
JP2000290093A (en) * | 1999-04-09 | 2000-10-17 | Tokai Carbon Co Ltd | Carbon crucible for single crystal pulling |
WO2009024045A1 (en) * | 2007-08-21 | 2009-02-26 | Hunan Kingbo Carbon-Carbon Composites Co. Ltd | A c/c composite crucible and a producing method thereof |
CN202830218U (en) * | 2011-05-18 | 2013-03-27 | 科发伦材料株式会社 | Carbon fiber reinforced carbon composite crucible and composite cylinder component |
CN108638599A (en) * | 2018-04-18 | 2018-10-12 | 保定顺天新材料股份有限公司 | Monocrystaline silicon stove Carbon fibe crucible knitted body and preparation method thereof |
CN112028657A (en) * | 2020-08-03 | 2020-12-04 | 杭州卓导新材料有限公司 | Preparation method of carbon/carbon composite material crucible |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2024055392A1 (en) * | 2022-09-15 | 2024-03-21 | 南京航空航天大学 | Weaving and needling integrated preform formation method and preform formation device |
JP7610900B2 (en) | 2022-09-15 | 2025-01-09 | 南京航空航天大学 | Preform molding method and preform molding device that integrates knitting and needling |
US12338561B2 (en) | 2022-09-15 | 2025-06-24 | Nanjing University Of Aeronautics And Astronautics | Integrated braiding and needle punching preform forming method and preform forming device |
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