CN114589819A - Hot bending die and preparation method thereof, curved ceramic part and electronic equipment - Google Patents
Hot bending die and preparation method thereof, curved ceramic part and electronic equipment Download PDFInfo
- Publication number
- CN114589819A CN114589819A CN202011421304.7A CN202011421304A CN114589819A CN 114589819 A CN114589819 A CN 114589819A CN 202011421304 A CN202011421304 A CN 202011421304A CN 114589819 A CN114589819 A CN 114589819A
- Authority
- CN
- China
- Prior art keywords
- barrier layer
- mold
- hot bending
- mold body
- hot
- 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.)
- Pending
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B28—WORKING CEMENT, CLAY, OR STONE
- B28D—WORKING STONE OR STONE-LIKE MATERIALS
- B28D1/00—Working stone or stone-like materials, e.g. brick, concrete or glass, not provided for elsewhere; Machines, devices, tools therefor
- B28D1/30—Working stone or stone-like materials, e.g. brick, concrete or glass, not provided for elsewhere; Machines, devices, tools therefor to form contours, i.e. curved surfaces, irrespective of the method of working used
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/10—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/58—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides
- C04B35/584—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides based on silicon nitride
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/62222—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products obtaining ceramic coatings
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/52—Multiple coating or impregnating multiple coating or impregnating with the same composition or with compositions only differing in the concentration of the constituents, is classified as single coating or impregnation
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/89—Coating or impregnation for obtaining at least two superposed coatings having different compositions
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3224—Rare earth oxide or oxide forming salts thereof, e.g. scandium oxide
- C04B2235/3225—Yttrium oxide or oxide-forming salts thereof
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3224—Rare earth oxide or oxide forming salts thereof, e.g. scandium oxide
- C04B2235/3229—Cerium oxides or oxide-forming salts thereof
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3231—Refractory metal oxides, their mixed metal oxides, or oxide-forming salts thereof
- C04B2235/3232—Titanium oxides or titanates, e.g. rutile or anatase
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/96—Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/96—Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
- C04B2235/963—Surface properties, e.g. surface roughness
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P40/00—Technologies relating to the processing of minerals
- Y02P40/50—Glass production, e.g. reusing waste heat during processing or shaping
- Y02P40/57—Improving the yield, e-g- reduction of reject rates
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Mining & Mineral Resources (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
Description
技术领域technical field
本申请属于电子产品技术领域,具体涉及热弯模具及其制备方法、曲面陶瓷件和电子设备。The application belongs to the technical field of electronic products, and in particular relates to a hot bending die and a preparation method thereof, a curved ceramic piece and electronic equipment.
背景技术Background technique
陶瓷材料具有硬度高、韧性好、耐磨等优点,近年来常常应用于电子设备中。随着电子设备外观设计的不断改变,越来越多的地方需要用到弯曲状的制件。因此,曲面陶瓷件的制备,对其在电子设备中的应用有重要意义。Ceramic materials have the advantages of high hardness, good toughness and wear resistance, and are often used in electronic equipment in recent years. With the continuous change of the appearance design of electronic equipment, more and more places need to use curved parts. Therefore, the preparation of curved ceramic parts is of great significance for its application in electronic devices.
发明内容SUMMARY OF THE INVENTION
鉴于此,本申请提供了一种热弯模具、热弯模具的制备方法,通过在模具本体上设置二氧化硅层和阻挡层,从而使得热弯模具具有优异的机械性能、结构稳定性和化学稳定性,从而使其能够用于陶瓷件的热弯,制备曲面陶瓷件,并且模具不与陶瓷件反应,保证曲面陶瓷件的生成良率,有利于曲面陶瓷件在电子设备中的应用。In view of this, the present application provides a hot bending mold and a method for preparing a hot bending mold. By arranging a silicon dioxide layer and a barrier layer on the mold body, the hot bending mold has excellent mechanical properties, structural stability and chemical properties. Stability, so that it can be used for hot bending of ceramic parts to prepare curved ceramic parts, and the mold does not react with the ceramic parts, ensuring the generation yield of the curved ceramic parts, which is beneficial to the application of the curved ceramic parts in electronic equipment.
第一方面,本申请提供了一种热弯模具,用于陶瓷件的热弯,所述热弯模具具有容置腔,所述容置腔用于容置所述陶瓷件,所述热弯模具包括模具本体,以及依次设置在所述模具本体靠近所述容置腔一侧的二氧化硅层以及至少一层阻挡层,所述模具本体的材质包括含硅化合物,所述阻挡层的材质包括氧化物陶瓷材料且不含二氧化硅。In a first aspect, the present application provides a hot bending die for hot bending a ceramic piece, the hot bending die has a accommodating cavity, the accommodating cavity is used for accommodating the ceramic piece, the hot bending die The mold includes a mold body, a silicon dioxide layer and at least one barrier layer sequentially arranged on the side of the mold body close to the accommodating cavity. The material of the mold body includes a silicon-containing compound, and the material of the barrier layer is Contains oxide ceramic material and does not contain silica.
第二方面,本申请提供了一种热弯模具的制备方法,包括:In a second aspect, the application provides a method for preparing a hot bending die, comprising:
提供模具本体前体,所述模具本体前体的材质包括含硅化合物,所述模具本体前体具有容置腔;providing a mold body precursor, the material of the mold body precursor includes a silicon-containing compound, and the mold body precursor has a accommodating cavity;
将所述模具本体前体进行煅烧,在所述模具本体前体靠近所述容置腔的一侧表面生成二氧化硅层;calcining the mold body precursor to generate a silicon dioxide layer on the surface of the mold body precursor near the accommodating cavity;
在所述二氧化硅层的表面成型至少一层阻挡层,所述阻挡层的材质包括氧化物陶瓷材料且不含二氧化硅,得到热弯模具。At least one barrier layer is formed on the surface of the silicon dioxide layer, and the material of the barrier layer includes oxide ceramic material and does not contain silicon dioxide to obtain a hot bending mold.
第三方面,本申请提供了一种曲面陶瓷件,通过使用第一方面所述的热弯模具获得。In a third aspect, the present application provides a curved ceramic piece obtained by using the hot bending die described in the first aspect.
第四方面,本申请提供了一种电子设备,包括第三方面所述的曲面陶瓷件。In a fourth aspect, the present application provides an electronic device, including the curved ceramic piece described in the third aspect.
本申请提供了一种热弯模具,该热弯模具中二氧化硅与模具本体和阻挡层之间的结合力好,提升整体结构的稳定性和使用寿命,并且阻挡层性能稳定,可以阻隔热弯模具使用过程中陶瓷件与模具本体、二氧化硅层接触和反应,避免陶瓷件粘模,容易脱模,保证陶瓷件的生产良率。该热弯模具制备方法简单,操作方便。通过该热弯模具制得的曲面陶瓷件的表面平整、无气泡产生,产品品质优异,能够应用于电子设备中,改善电子设备的外观和性能。The application provides a hot bending mold, in which the silicon dioxide, the mold body and the barrier layer have good bonding force, improve the stability and service life of the overall structure, and have stable performance of the barrier layer, which can block heat During the use of the bending mold, the ceramic parts contact and react with the mold body and the silicon dioxide layer, so as to avoid the ceramic parts from sticking to the mold, easy to demould, and ensure the production yield of the ceramic parts. The preparation method of the hot bending mold is simple and the operation is convenient. The surface of the curved ceramic piece prepared by the hot bending die is smooth, no bubbles are generated, the product quality is excellent, and the product can be applied to electronic equipment to improve the appearance and performance of the electronic equipment.
附图说明Description of drawings
为了更清楚地说明本申请实施方式中的技术方案,下面将对本申请实施方式中所需要使用的附图进行说明。In order to describe the technical solutions in the embodiments of the present application more clearly, the accompanying drawings required to be used in the embodiments of the present application will be described below.
图1为本申请一实施方式提供的热弯模具的示意图。FIG. 1 is a schematic diagram of a hot bending die provided by an embodiment of the present application.
图2为本申请一实施方式提供的热弯模具的结构示意图。FIG. 2 is a schematic structural diagram of a hot bending die provided by an embodiment of the present application.
图3为本申请一实施方式提供的热弯模具的结构示意图。FIG. 3 is a schematic structural diagram of a hot bending die provided by an embodiment of the present application.
图4为本申请另一实施方式提供的热弯模具的结构示意图。FIG. 4 is a schematic structural diagram of a hot bending die provided by another embodiment of the present application.
图5为本申请一实施方式提供的热弯模具的制备方法流程图。FIG. 5 is a flowchart of a method for preparing a hot bending die provided by an embodiment of the present application.
图6为本申请一实施方式提供的曲面陶瓷件。FIG. 6 is a curved ceramic piece provided by an embodiment of the present application.
图7为图6中A-A线的剖面放大图。FIG. 7 is an enlarged cross-sectional view taken along the line A-A in FIG. 6 .
图8为本申请一实施方式的电子设备的结构示意图。FIG. 8 is a schematic structural diagram of an electronic device according to an embodiment of the present application.
标号说明:Label description:
模具本体-11,凹模-111,凸模-112,二氧化硅层-12,阻挡层-13,容置腔-10热弯模具-100,曲面陶瓷件-200。Mold body-11, female mold-111, punch-112, silicon dioxide layer-12, barrier layer-13, accommodating cavity-10 Hot bending mold-100, curved ceramic piece-200.
具体实施方式Detailed ways
以下是本申请的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本申请原理的前提下,还可以做出若干改进和润饰,这些改进和润饰也视为本申请的保护范围。The following are the preferred embodiments of the present application. It should be pointed out that for those skilled in the art, without departing from the principles of the present application, several improvements and modifications can be made, and these improvements and modifications are also regarded as the present invention. The scope of protection applied for.
下文的公开提供了许多不同的实施方式或例子用来实现本申请的不同结构。为了简化本申请的公开,下文中对特定例子的部件和设置进行描述。当然,它们仅仅为示例,并且目的不在于限制本申请。此外,本申请可以在不同例子中重复参考数字和/或参考字母,这种重复是为了简化和清楚的目的,其本身不指示所讨论各种实施方式和/或设置之间的关系。此外,本申请提供了的各种特定的工艺和材料的例子,但是本领域普通技术人员可以意识到其他工艺的应用和/或其他材料的使用。The following disclosure provides many different embodiments or examples for implementing different structures of the present application. To simplify the disclosure of the present application, the components and arrangements of specific examples are described below. Of course, they are only examples and are not intended to limit the application. Furthermore, this application may repeat reference numerals and/or reference letters in different instances for the purpose of simplicity and clarity, and does not in itself indicate a relationship between the various embodiments and/or arrangements discussed. In addition, this application provides examples of various specific processes and materials, but one of ordinary skill in the art will recognize the application of other processes and/or the use of other materials.
请参考图1,为本申请一实施方式提供的热弯模具的示意图,其中,热弯模具100具有容置腔10,容置腔10用于容置陶瓷件。请参阅图2,为本申请一实施方式提供的热弯模具的结构示意图,其中,热弯模具100包括模具本体11,以及依次设置在模具本体11靠近容置腔10一侧的二氧化硅层12以及至少一层阻挡层13,模具本体11的材质包括含硅化合物,阻挡层13的材质包括氧化物陶瓷材料且不含二氧化硅。其中,模具本体11的材质包括含硅化合物,使得热弯模具100具有优异的强度、耐冷热冲击、耐高温腐蚀以及低的高温蠕变率;二氧化硅层12与模具本体11和阻挡层13之间的结合力好,提升整体结构的稳定性和使用寿命;阻挡层13可以阻隔陶瓷件与模具本体11、二氧化硅层12直接接触,并避免陶瓷件与模具本体11、二氧化硅层12之间发生反应,从而避免陶瓷件粘模现象以及陶瓷件表面不良的产生,使得热弯后的陶瓷件容易脱模,且陶瓷件表面良好,保证陶瓷件的生产良率,同时阻挡层13的设置使得热弯模具100在使用时可以直接置于空气气氛中,阻挡层13性能稳定,在空气中不易发生反应,依然能够起到阻隔作用,使热弯过程无需在惰性气氛中进行,减小后续生产成本;热弯模具100中模具本体11、二氧化硅层12和阻挡层13三者结合作用,从而提高了热弯模具100的整体性能,同时热弯模具100中相邻各层之间具有优异的结合力,进一步提升整体结构的稳定性和使用寿命。Please refer to FIG. 1 , which is a schematic diagram of a hot bending mold according to an embodiment of the present application, wherein the
相关技术中,在对陶瓷件进行热弯时,模具本体11直接与陶瓷件接触进行热弯操作,由于热弯在高温下进行,在此过程中,模具本体11在高温条件下表面发生反应,产生二氧化硅;虽然生成的二氧化硅阻隔模具本体11的进一步反应,但二氧化硅会与陶瓷件之间发生反应,产生硅酸盐等物质,造成陶瓷件表面具有鼓泡,并且与模具本体11之间有粘接,产生粘模,造成脱模困难。在本申请中,通过设置阻挡层13,阻挡了陶瓷件与模具本体11之间接触反应,使得陶瓷件的表面质量良好,容易脱模,提高整体结构的稳定性,同时设置二氧化硅层12,提高模具本体11与阻挡层13之间的结合力,增强结构稳定性。In the related art, when hot bending the ceramic piece, the
在本申请中,模具本体11的材质包括含硅化合物,从而使得热弯模具100具有优异的高温强度、抗热震性、耐高温腐蚀以及低的蠕变率,保证了热弯模具100的性能和使用寿命。In the present application, the material of the
请参阅图3,为本申请一实施方式提供的热弯模具的结构示意图,其中,模具本体11包括相匹配的凸模112和凹模111。可以理解的,图3中所示的为热弯模具100开合状态的示意图,相匹配的凸模112和凹模111可以盖合在一起,并且在凸模112和凹模111之间具有容置空间,从而使得热弯模具100具有的容置陶瓷件的容置腔10。其中,凸模112还可以称之为后模、动模、公模、下模或阳模,凹模111也可以称之为前模、定模、母模、上模或阴模。可以理解的,图3中模具本体11的结构仅作为一示例,其他形状、匹配状态的模具本体11也适用于本申请。可以理解的,热弯模具100具有容置腔10,也就是说,凸模112和凹模111盖合之后,凸模112和凹模111盖合之后之间具有间距,使得热弯模具100具有容置腔10,即模具本体11中具有容置腔空间。在本申请实施方式中,当模具本体11包括凸模112和凹模111时,由于二氧化硅层12以及至少一层阻挡层13依次设置在模具本体11靠近容置腔10的一侧,因此,在凸模112靠近容置腔10一侧的表面上依次设置了二氧化硅层12以及至少一层阻挡层13,在凹模111靠近容置腔10一侧的表面上依次设置了二氧化硅层12以及至少一层阻挡层13,也就是说,沿热弯模具100外部至容置腔10的方向上,热弯模具100包括了模具本体11、二氧化硅层12以及至少一层阻挡层13。在本申请中,通过在凸模112和凹模111表面设置阻挡层13,使得阻挡层13与陶瓷件之间接触,避免凸模112和凹模111和陶瓷件接触发生反应,保证了陶瓷件的性能,同时通过二氧化硅层12进行过渡,使得凸模112和凹模111、与阻挡层13之间更稳定结合,提升整体结构的稳定性。在一实施例中,凸模112和凹模111可以通过插接卡合固定,也可以通过螺丝固定,具体可以根据需要进行选择。Please refer to FIG. 3 , which is a schematic structural diagram of a hot bending mold according to an embodiment of the present application, wherein the
在本申请实施方式中,含硅化合物包括碳化硅和氮化硅中的至少一种。采用碳化硅和/或氮化硅制得的模具本体11具有优异的高温强度、低的高温蠕变率的性能,进一步提高模具本体11的使用寿命。在一实施例中,当模具本体11包括凸模112和凹模111时,凸模112和凹模111的材质分别包括碳化硅和氮化硅中的至少一种。具体的,凸模112和凹模111的材质可以相同,也可以不同。In the embodiments of the present application, the silicon-containing compound includes at least one of silicon carbide and silicon nitride. The
在本申请实施方式中,模具本体11可以通过无压烧结、热压烧结、热等静压烧结或反应烧结等方式获得。在一实施例中,将碳化硅与粘结剂混合后,通过干压成型、挤出成型或注塑成型的方式得到坯体,将坯体进行烧结后得到模具本体11。具体的,烧结温度可以为1200℃-1500℃,时间可以为1h-5h。在本申请中,模具本体11的厚度、形状、容置腔10的大小可以根据实际需要进行选择。In the embodiment of the present application, the
抗弯强度是抵抗弯曲不断裂的能力。一般采用三点抗弯测试或四点测试方法评测。本申请中通过采用GB/T 6569-2006《精细陶瓷弯曲强度试验方法》对模具本体11进行四点抗弯强度的检测。在本申请中,模具本体11的抗弯强度大于550MPa。进一步的,模具本体11的抗弯强度大于600MPa。更进一步的,模具本体11的抗弯强度大于750MPa。在一实施例中,当模具本体11由碳化硅组成时,模具本体11的抗弯强度大于550MPa、大于600MPa或大于620MPa等。在另一实施例中,当模具本体11由氮化硅组成时,模具本体11的抗弯强度大于750MPa、大于800MPa或大于830MPa等。本申请的模具本体11具有优异的抗弯强度,进而保证了其使用寿命。Flexural strength is the ability to resist bending without breaking. Generally, three-point bending test or four-point test method are used for evaluation. In this application, the four-point bending strength test of the
本申请通过采用GB/T 25995-2010《精细陶瓷密度和显气孔率试验方法》对模具本体11的气孔率进行检测。在本申请实施方式中,模具本体11的气孔率小于1%。即模具本体11的致密度大于99%。进一步的,模具本体11的气孔率小于0.5%。模具本体11的低气孔率保证了模具本体11内部的结合强度,有利于整体结构稳定性的提升。In this application, the porosity of the
在本申请中,二氧化硅层12作为过渡层,与模具本体11和阻挡层13之间的结合力好,提升了整体的稳定性。在本申请实施方式中,在阻挡层13制备过程中,氧化物陶瓷材料与二氧化硅层中的非桥键氧发生反应,形成永久键合,使得二氧化硅层12与阻挡层13之间具有优异的结合力。在本申请实施方式中,二氧化硅层12完全覆盖模具本体11的表面,从而有利于后续阻挡层13的制备,以及完全阻隔陶瓷件与模具本体11接触。In the present application, the
在本申请实施方式中,二氧化硅层12的厚度为10nm-100nm。通过设置上述厚度的二氧化硅层12,可以使得二氧化硅层12与模具本体11、阻挡层13之间具有较强的结合力,提高整体的结构稳定性和高温稳定性;二氧化硅层12厚度过薄,与阻挡层13的结合力一般,不利于阻挡层13长期稳定的存在;二氧化硅层12强度较低,当二氧化硅层12过厚时,二氧化硅占比过多,在热弯过程中模具表面层结构的强度偏低,影响二氧化硅层12与阻挡层13和模具本体11之间的结合力,影响整体结构稳定性,甚至会造成阻挡层13脱落的发生。因此,上述厚度的二氧化硅层12与模具本体11、阻挡层13之间的结合力优异,同时又不会降低整体强度,提高了整体结构的稳定性。进一步的,二氧化硅层12的厚度为15nm-90nm。更进一步的,二氧化硅层12的厚度为20nm-50nm。具体的,二氧化硅层12的厚度可以但不限于为10nm、25nm、30nm、40nm、50nm、60nm、65nm、70nm、75nm或85nm。In the embodiment of the present application, the thickness of the
在本申请实施方式中,可以将模具本体11进行煅烧,从而使得模具本体11中的含硅化合物与氧气反应,生成二氧化硅,即可得到二氧化硅层12。二氧化硅层12的制备方法简单,操作方便,同时由于是在模具本体11表面直接反应制得二氧化硅层12,因此,二氧化硅层12与模具本体11之间的结合力十分优异,避免了二氧化硅层12与模具本体11在高温下分离的发生。在一实施例中,煅烧的温度可以为1200℃-1500℃,时间为1h-5h。进一步的,煅烧的温度可以为1250℃-1400℃,时间为2h-4.5h。In the embodiment of the present application, the
在本申请中,阻挡层13用于阻隔模具本体11与陶瓷件之间接触,防止在热弯过程中模具本体11与陶瓷件之间发生反应,保证了陶瓷件热弯后易于脱模,陶瓷件的表面平整性佳;同时阻挡层13与二氧化硅层12之间的结合力好,使得阻挡层13可以很好地设置在模具本体11上,避免脱落的发生。在本申请实施方式中,阻挡层13完全覆盖二氧化硅层12,以完全隔绝陶瓷件与二氧化硅层12的接触,保证陶瓷件的品质。In this application, the
在本申请中,热弯模具100中可以包括一层或多层阻挡层13。通过设置一层阻挡层13可以达到上述效果,通过设置多层阻挡层13,可以进一步提升热弯模具100整体结构的稳定性。在本申请一实施方式中,阻挡层13的层数小于10层。也就是说,热弯模具100中可以设置1层-9层的阻挡层13。通过设置上述的层数的阻挡层13,既保证了整体结构的稳定性,同时在热弯过程中,积累在阻挡层13内部的内应力不会过大,防止脱落的发生。进一步的,阻挡层13的层数为2层-8层。具体的,热弯模具100中可以但不限于包括1层阻挡层13、2层阻挡层13、3层阻挡层13、4层阻挡层13、5层阻挡层13、6层阻挡层13、7层阻挡层13、8层阻挡层13或9层阻挡层13。请参阅图4,为本申请另一实施方式提供的热弯模具的结构示意图,其与图2大致相同,不同之处在于,热弯模具100中包括了2层阻挡层13。可以理解的,热弯模具100中还可以包括其他数量的多层阻挡层13,在此不一一举例说明。当热弯模具100具有多层阻挡层13时,多层阻挡层13的材质、厚度可以相同,也可以不同,可以根据需要进行选择。In the present application, one or more barrier layers 13 may be included in the hot bending die 100 . The above effect can be achieved by providing one layer of
在本申请实施方式中,阻挡层13的厚度为100nm-500nm。可以理解的,此处阻挡层13的厚度为一层阻挡层13的厚度。通过设置上述厚度的阻挡层13,既能够阻隔陶瓷件与模具本体11接触和反应,同时与二氧化硅层12具有优异的结合力,并且也保证了在具有多层阻挡层13时,多层阻挡层13之间可以更好地结合在一起,防止脱落的发生。进一步的,阻挡层13的厚度为100nm-450nm。更进一步的,阻挡层13的厚度为100nm-200nm。具体的,阻挡层13的厚度可以但不限于为120nm、160nm、170nm、190nm、230nm、250nm、280nm、300nm、340nm、370nm、400nm、440nm、450nm或480nm。In the embodiment of the present application, the thickness of the
在本申请实施方式中,当热弯模具100具有多层阻挡层13时,阻挡层13的总厚度小于990nm。既保证与二氧化硅之间的结合力,又可以起到阻挡作用。进一步的,阻挡层13的总厚度小于800nm。更进一步的,阻挡层13的总厚度小于500nm。在一实施方式中,当热弯模具100具有多层阻挡层13时,多层阻挡层13的厚度沿二氧化硅层12至容置腔10的方向上增加。从而使得靠近二氧化硅层12的阻挡层13主要起到结合作用,保证与二氧化硅层12结合力,靠近容置腔10的阻挡层13主要啊起到阻隔作用,阻挡陶瓷件与模具本体11和二氧化硅层12接触。在一实施例中,当热弯模具100具有多层阻挡层13时,包括依次设置在二氧化硅12上的第一阻挡层、第二阻挡层、…、第N阻挡层,其中N为正整数。可选的,N为小于10的正整数。在一具体实施例中,第一阻挡层的厚度为50nm-150nm、80nm-120nm或100nm-150nm,从而先保证多层阻挡层与二氧化硅层之间的结合力,保证整体结构的稳定性。在另一具体实施例中,第N阻挡层的厚度为160nm-500nm、170nm-400nm、180nm-300nm或180nm-200nm,从而保证阻挡层13的阻挡作用,防止在热弯过程中陶瓷件与二氧化硅层12和模具本体11接触。In the embodiment of the present application, when the hot bending die 100 has multiple barrier layers 13 , the total thickness of the barrier layers 13 is less than 990 nm. It not only ensures the bonding force with silica, but also acts as a barrier. Further, the total thickness of the
在本申请中,阻挡层13的材质包括氧化物陶瓷材料,使得阻挡层13性能稳定,不易与氧气发生氧化,层结构的稳定性高,有利于热弯模具100直接在空气气氛中使用,无需使用惰性气氛,减少了后续应用的工艺难度;同时阻挡层13的材质不含二氧化硅,即可避免在热弯过程中陶瓷件与二氧化硅之间发生反应,避免脱模困难的问题。氧化物陶瓷材料具有优良的强度、硬度、绝缘性、热传导、耐高温、耐氧化、耐腐蚀、耐磨及高温强度等特性,在严苛的环境条件下具有良好的高温稳定性与力学性能。在本申请实施方式中,阻挡层13的材质包括二元氧化物、玻璃陶瓷材料、钛酸盐陶瓷材料及羟基磷灰石陶瓷材料中的至少一种。可以理解的,本申请选用的阻挡层13的材质在热弯过程中不与陶瓷件反生反应,同时与二氧化硅之间具有较好的结合力;具体的,二元氧化物陶瓷材料包括氧化铝、氧化钛、氧化锌及稀土氧化物中的至少一种。进一步的,氧化物陶瓷材料包括氧化铝、二氧化钛、氧化钇和氧化铈中的至少一种。在本申请一实施例中,阻挡层13的材质为氧化铝。氧化铝与二氧化硅层可以产生较强的化学键,从而提高阻挡层与二氧化硅层之间的结合力。在本申请另一实施例中,阻挡层13的材质包括氧化铝,以及二氧化钛、氧化钇和氧化铈中的至少一种。通过添加二氧化钛、氧化钇和氧化铈中的至少一种,从而可以提升阻挡层13的性能。在一实施例中,按质量百分比计,阻挡层13包括氧化铝80%-100%、二氧化钛0%-20%、氧化钇0%-5%以及氧化铈0%-1%。其中,氧化钛可以提高阻挡层13的致密度和硬度,使得阻挡层13在循环使用时不易磨损;氧化钇和氧化铈可以提升阻挡层13的致密度、多层阻挡层13之间的结合力,在循环使用时不易剥落,同时还提升了整体的抗热震性。进一步的,阻挡层13中氧化铝的质量含量为85%-98%、85%-96%、88%-95%或90%-95%等。具体的,阻挡层13中氧化铝的质量含量可以但不限于为80%、82%、84%、86%、89%、91%、92%、93%、94%、97%或99%。进一步的,阻挡层13中二氧化钛的质量含量为1%-15%、2%-13%、3%-10%或3%-8%等。具体的,阻挡层13中二氧化钛的质量含量可以但不限于为4%、5%、6%、11%、12%、16%、18%或19%。进一步的,阻挡层13中氧化钇的质量含量为1%-5%、1%-4%、1%-3%或2%-5%等。具体的,阻挡层13中氧化钇的质量含量可以但不限于为1%、1.5%、2%、2.5%、3%、3.5%、4.5%或5%。进一步的,阻挡层13中氧化铈的质量含量为0%-0.8%、0%-0.01%、0.001%-0.5%或0.001%-0.1%等。具体的,阻挡层13中氧化铈的质量含量可以但不限于为0.001%、0.005%、0.008%、0.01%、0.05%、0.07%、0.1%、0.3%、0.5%或0.7%。在另一实施例中,按质量百分比计,阻挡层13包括氧化铝90%-95%、二氧化钛3%-8%、氧化钇1%-3%以及氧化铈0%-0.01%。在又一实施例中,按质量百分比计,阻挡层13包括氧化铝90%-95%、二氧化钛3%-8%、氧化钇1%-3%以及氧化铈0.001%-0.01%。由于氧化铈为淡黄色,因此上述范围的氧化铈可以避免使陶瓷件表面颜色发生变化,同时也尽量避免热弯时少量铈原子渗入陶瓷件晶格中,从而避免了对陶瓷件相变强化的影响,保证了陶瓷件的强度。In the present application, the material of the
在本申请实施方式中,二氧化硅层12以及至少一层的阻挡层13的总厚度在1000nm以下。也就是说,设置在模具本体11上的涂层的总厚度在1000nm以下,从而保证了热弯模具100在循环使用过程中涂层内部不会积累过量的内应力,防止涂层的脱落,保证热弯模具100整体结构的稳定性。在一实施例中,二氧化硅层12以及至少一层的阻挡层13的总厚度为100nm-1000nm。从而使得涂层的厚度不会过薄,不易磨穿,使用寿命长,同时也保证了结构的稳定性。进一步的,二氧化硅层12以及至少一层的阻挡层13的总厚度为200nm-1000nm、200nm-900nm、300nm-800nm等。In the embodiment of the present application, the total thickness of the
在本申请实施方式中,热弯模具100靠近容置腔10一侧的表面的粗糙度小于100nm。从而保证了热弯过程中陶瓷件与热弯模具100之间不会发生粘结,同时保证了陶瓷件表面的平整和光滑。进一步的,热弯模具100靠近容置腔10一侧的表面的粗糙度小于50nm、60nm、70nm、80nm或90nm。In the embodiment of the present application, the roughness of the surface of the hot bending die 100 on the side close to the
在本申请实施方式中,热弯模具100的抗弯强度大于600MPa。进一步的,热弯模具100的抗弯强度大于670MPa。更进一步的,热弯模具100的抗弯强度大于800MPa。在一实施例中,当模具本体11由碳化硅组成时,热弯模具100的抗弯强度大于600MPa。在另一实施例中,当模具本体11由氮化硅组成时,热弯模具100的抗弯强度大于800MPa。本申请的热弯模具100具有优异的抗弯强度,保证其使用寿命。In the embodiment of the present application, the bending strength of the hot bending die 100 is greater than 600 MPa. Further, the bending strength of the hot bending die 100 is greater than 670 MPa. Furthermore, the bending strength of the hot bending die 100 is greater than 800 MPa. In one embodiment, when the
在本申请实施方式中,热弯模具100的气孔率低于0.1%。进一步的,模具本体11的气孔率小于0.5%。热弯模具100的低气孔率保证了热弯模具100内部的结合强度,有利于整体结构稳定性的提升。In the embodiment of the present application, the porosity of the hot bending die 100 is less than 0.1%. Further, the porosity of the
在本申请中,通过在模具本体11上设置二氧化硅层12和阻挡层13,从而使得热弯模具100的性能优异,结构稳定,使用寿命长;在热弯中不会和陶瓷件发生粘结,保证陶瓷件容易脱模,同时可以直接在空气气氛中使用,减小陶瓷件生产成本。In the present application, the
请参阅图5,为本申请一实施方式提供的热弯模具的制备方法流程图,该制备方法制备上述任一实施例的热弯模具100,包括:Please refer to FIG. 5 , which is a flowchart of a method for preparing a hot-bending mold according to an embodiment of the present application. The preparation method for preparing the hot-bending
操作101:提供模具本体前体,模具本体前体的材质包括含硅化合物,模具本体前体具有容置腔。Operation 101 : providing a mold body precursor, the material of the mold body precursor includes a silicon-containing compound, and the mold body precursor has a accommodating cavity.
操作102:将模具本体前体进行煅烧,在模具本体前体靠近容置腔的一侧表面生成二氧化硅层。Operation 102 : calcining the mold body precursor to form a silicon dioxide layer on the surface of the mold body precursor near the accommodating cavity.
操作103:在二氧化硅层的表面成型至少一层阻挡层,阻挡层的材质包括氧化物陶瓷材料且不含二氧化硅,得到热弯模具。Operation 103: At least one barrier layer is formed on the surface of the silicon dioxide layer, and the material of the barrier layer includes oxide ceramic material and does not contain silicon dioxide to obtain a hot bending mold.
在操作101中,模具本体前体可以通过无压烧结、热压烧结、热等静压烧结或反应烧结等方式获得,也可以为市售的模具本体前体。在本申请实施方式中,模具本体前体的气孔率小于1%,游离硅含量小于1%,游离碳含量小于1%。从而保证热弯模具100的性能。在本申请实施方式中,烧结温度可以为1200℃-1500℃,时间可以为1h-5h。进一步的,烧结温度为1250℃-1400℃,时间可以为1h-3h。具体的,烧结可以但不限于在空气气氛中进行。通过烧结稳定模具本体前体内部的微观结构,降低游离硅和游离碳含量,提高模具本体前体的抗热震性,不易开裂,提高使用寿命。在一实施例中,还包括对烧结后的模具本体前体进行抛光。具体的,抛光后模具本体前体的表面粗糙度小于1μm。在另一实施例中,模具本体前体可以进行多次烧结,以提高内部结构的稳定性。具体的,可以但不限于进行2次烧结、3次烧结或4次烧结等,可以在每次烧结后进行抛光处理。In
在操作102中,将模具本体前体进行煅烧,在模具本体前体靠近容置腔10的一侧表面生成二氧化硅层12。模具本体前体中具有含硅化合物,通过煅烧,使含硅化合物与氧气反应,在模具本体前体表面生产了二氧化硅。可以理解的,由于模具本体前体在此过程中表面发生反应,与最终制得的热弯模具100中模具本体11的组成成分有一定的区别,因此,将发生反应之前的模具本体11称之为模具本体前体,但模具本体前体的相关性能、结构等均可为上述模具本体11的描述范围。具体的,当模具本体前体包括凹模前体和凸模前体时,可以将凹模前体和凸模前体靠近容置腔10的一侧表面进行煅烧处理,从而在凹模前体和凸模前体靠近容置腔10的一侧表面上分别成型二氧化硅层12。也就是说,经煅烧处理后,模具本体前体成为模具本体11,凹模前体成为凹模111,凸模前体成为凸模112。在一实施方式中,煅烧的温度为1200℃-1500℃,时间为1h-5h。进一步的,煅烧的温度为1250℃-1450℃,时间为1.5h-4h。In
在操作103中,可以通过气相沉积和喷涂中的至少一种方法成型阻挡层13。在一实施方式中,可以在二氧化硅层12表面成型多层阻挡层13,多层阻挡层13的成型方法可以相同,也可以不同。在另一实施方式中,气相沉积包括物理气相沉积和化学气相沉积中的至少一种,具体的,可以但不限于为真空蒸镀、磁控溅射、常压化学气相沉积等,提高与二氧化硅层12之间的结合力。在又一实施方式中,喷涂为热喷涂,具体的,可以但不限于为等离子热喷涂,降低工艺复杂度,降低制备成本。在一实施例中,采用氧化铝作为靶材,在真空中在二氧化硅层表面蒸镀阻挡层13,其中,靶材功率为6kW-10kW,以氮气为反应气体,氮气的流量为120sccm-150sccm,镀膜时间为5min-10min。在另一实施例中,等离子热喷涂的电弧电压为80V-100V,电弧电流为600A-800A,喷涂距离为500mm-90mm,喷涂移动速度为3m/min-5m/min,氩气流量为25dm3/min-40dm3/min,氢气流量120dm3/min-160dm3/min。在一具体实施例中,等离子热喷涂的电弧电压为90V、电弧电流为700A、喷涂距离为80mm、喷枪移动速度为5m/min、氩气流量为30dm3/min、氢气流量为150dm3/min。In
在本申请实施方式中,在成型阻挡层13后,还进行煅烧处理。通过煅烧,可以提高阻挡层13与二氧化硅层12之间的结合力,降低阻挡层13和二氧化硅层12的孔隙率,提升整体结构的稳定性和使用寿命。在一实施方式中,煅烧的温度为1200℃-1500℃,时间为1h-5h。进一步的,煅烧的温度为1250℃-1450℃,时间为1.5h-4h。更进一步的,煅烧的温度为1250℃-1400℃,时间为2h-4h。在另一实施方式中,当成型多层阻挡层13时,可以在成型多层阻挡层13后再进行煅烧处理。在又一实施方式中,当成型多层阻挡层13时,在成型每一层阻挡层13后均进行煅烧处理,从而可以使成型的每一层阻挡层13的孔隙率以及与其他层结构之间的结合力增强,更有利于整体结构稳定性的提升。In the embodiment of the present application, after the
在本申请实施方式中,还包括对热弯模具100进行抛光处理。可以理解的,抛光处理是对热弯模具100靠近容置腔10的一侧表面进行,从而有利于保证热弯后陶瓷件表面的平整和光滑。在一实施例中,热弯模具100靠近容置腔10一侧的表面的粗糙度小于100nm。In the embodiment of the present application, polishing processing is also performed on the hot bending die 100 . It can be understood that the polishing process is performed on the surface of the side surface of the hot bending die 100 close to the
本申请提供的制备方法简单、操作方便,能够得到性能稳定的热弯模具100,有利于进行陶瓷件的热弯处理。The preparation method provided by the present application is simple and convenient to operate, and a hot bending die 100 with stable performance can be obtained, which is favorable for hot bending treatment of ceramic parts.
本申请还提供了一种曲面陶瓷件200,通过上述的热弯模具100获得。通过采用上述的热弯模具100,可以制得曲面陶瓷件200,该曲面陶瓷件200容易与热弯模具100分离,表面平整光滑,品质佳。可以理解的,通过将陶瓷件置于热弯模具100中经过热弯过程,得到曲面陶瓷件200;该陶瓷件可以但不限于为平板状,曲面陶瓷件200可以但不限于为2.5D陶瓷件、3D陶瓷件等,具体的曲面陶瓷件200形状根据热弯模具100容置腔10内部形状决定,当然也可以根据所需的曲面陶瓷件200的形状设计所需的热弯模具100。请参阅图6,为本申请一实施方式提供的曲面陶瓷件。请参阅图7,为图6中A-A线的剖面放大图。可以看出,通过上述热弯模具100,可以制得曲面陶瓷件200,曲面陶瓷件200的表面平整、无气泡产生,产品品质优异,有利于其应用。The present application also provides a curved
本申请还提供了一种电子设备,包括上述的曲面陶瓷件200。通过在电子设备中设置曲面陶瓷件200,提升了电子设备的外观可变性,增强视觉效果,提升产品竞争力。可以理解的,电子设备可以但不限于为手机、平板电脑、笔记本电脑、手表、MP3、MP4、GPS导航仪、数码相机等。下面以手机为例进行说明。请参阅图8,为本申请一实施方式的电子设备的结构示意图,电子设备包括了上述的曲面陶瓷件200。此时,曲面陶瓷件200作为电子设备的壳体使用。具体的,曲面陶瓷件200可以但不限于作为电子设备的后盖、中框、按键等,提升电子设备的品质。The present application also provides an electronic device including the above-mentioned curved
实施例1Example 1
一种热弯模具的制备方法A kind of preparation method of hot bending die
提供碳化硅模具本体,碳化硅模具本体具有容置腔;将碳化硅模具本体靠近容置腔的一侧表面在1300℃下烧结2h后进行抛光处理,并再重复两次烧结和抛光处理,再在1400℃下煅烧3h,在碳化硅模具本体靠近容置腔的一侧表面生成二氧化硅层。A silicon carbide mold body is provided, and the silicon carbide mold body has an accommodating cavity; the surface of the side of the silicon carbide mold body close to the accommodating cavity is sintered at 1300 ° C for 2 hours and then polished, and the sintering and polishing treatment are repeated twice, and then After calcination at 1400°C for 3 hours, a silicon dioxide layer is formed on the surface of the silicon carbide mold body on the side close to the accommodating cavity.
提供阻挡浆料,其中阻挡浆料中包括了92%的氧化铝、5%的氧化钛和3%的氧化钇。通过等离子喷涂的方式,在二氧化硅层成型150nm的阻挡层,其中等离子喷涂的电弧电压为90V、电弧电流为700A、喷涂距离为80mm、喷枪移动速度为5m/min、氩气流量为30dm3/min、氢气流量为150dm3/min。然后在1250℃下煅烧1h后,对阻挡层表面进行抛光处理,使其表面粗糙度小于100nm,即得到热弯模具。A barrier slurry is provided, wherein the barrier slurry includes 92% alumina, 5% titania, and 3% yttria. By means of plasma spraying, a barrier layer of 150 nm is formed on the silicon dioxide layer, wherein the arc voltage of the plasma spraying is 90V, the arc current is 700A, the spraying distance is 80mm, the moving speed of the spray gun is 5m/min, and the flow rate of argon gas is 30dm3 . /min, and the hydrogen flow rate was 150 dm 3 /min. Then, after calcining at 1250° C. for 1 h, the surface of the barrier layer is polished to make the surface roughness less than 100 nm, that is, a hot bending die is obtained.
实施例2Example 2
与实施例1大体相同,不同之处在于,成型阻挡层后不进行煅烧处理。It is substantially the same as Example 1, except that the calcination treatment is not performed after forming the barrier layer.
实施例3Example 3
与实施例1大体相同,不同之处在于,采用氮化硅模具本体,成型三层阻挡层,且每成型一层阻挡层后均进行煅烧处理。It is basically the same as Example 1, except that a silicon nitride mold body is used to form three barrier layers, and calcination is performed after each barrier layer is formed.
对比例1Comparative Example 1
与实施例1大体相同,不同之处在于,不设置二氧化硅层。It is substantially the same as Example 1, except that no silicon dioxide layer is provided.
对比例2Comparative Example 2
与实施例2大体相同,不同之处在于,不设置二氧化硅层。It is substantially the same as Example 2, except that no silicon dioxide layer is provided.
效果实施例Effect Example
采用Anton Paar品牌的MCT300型微米划痕仪,以及N-138型金刚石球形压头(压头直径200μm,最大载荷30N),对实施例和对比例制得的热弯模具进行检查。结果发现,实施例1中阻挡层的剥离力为26N,实施例2中阻挡层的剥离力为17N,实施例3中阻挡层的剥离力为28N,对比例1中阻挡层的剥离力为11N,对比例2中阻挡层的剥离力为7N。可以看出,本申请提供的热弯模具中阻挡层的结合力更好,整体结构的稳定性更强,有利于长时间使用。Using Anton Paar brand MCT300 micrometer scratch tester, and N-138 diamond spherical indenter (indenter diameter 200μm, maximum load 30N), the hot bending dies prepared in the Examples and Comparative Examples were inspected. It was found that the peeling force of the barrier layer in Example 1 was 26N, the peeling force of the barrier layer in Example 2 was 17N, the peeling force of the barrier layer in Example 3 was 28N, and the peeling force of the barrier layer in Comparative Example 1 was 11N , the peeling force of the barrier layer in Comparative Example 2 was 7N. It can be seen that the bonding force of the barrier layer in the hot bending mold provided by the present application is better, and the stability of the overall structure is stronger, which is favorable for long-term use.
以上对本申请实施方式所提供的内容进行了详细介绍,本文对本申请的原理及实施方式进行了阐述与说明,以上说明只是用于帮助理解本申请的方法及其核心思想;同时,对于本领域的一般技术人员,依据本申请的思想,在具体实施方式及应用范围上均会有改变之处,综上所述,本说明书内容不应理解为对本申请的限制。The content provided by the embodiments of the present application has been introduced in detail above, and the principles and embodiments of the present application have been described and explained herein. Persons of ordinary skill, according to the idea of the present application, will have changes in the specific implementation manner and application scope. In conclusion, the contents of this specification should not be construed as a limitation on the present application.
Claims (14)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011421304.7A CN114589819A (en) | 2020-12-07 | 2020-12-07 | Hot bending die and preparation method thereof, curved ceramic part and electronic equipment |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011421304.7A CN114589819A (en) | 2020-12-07 | 2020-12-07 | Hot bending die and preparation method thereof, curved ceramic part and electronic equipment |
Publications (1)
Publication Number | Publication Date |
---|---|
CN114589819A true CN114589819A (en) | 2022-06-07 |
Family
ID=81812917
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202011421304.7A Pending CN114589819A (en) | 2020-12-07 | 2020-12-07 | Hot bending die and preparation method thereof, curved ceramic part and electronic equipment |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN114589819A (en) |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1830852A (en) * | 2005-03-10 | 2006-09-13 | 鸿富锦精密工业(深圳)有限公司 | Mould and its preparation method |
CN1899992A (en) * | 2005-07-19 | 2007-01-24 | 鸿富锦精密工业(深圳)有限公司 | Mould kernel and its preparing method |
CN102389922A (en) * | 2011-06-16 | 2012-03-28 | 昆山市瑞捷精密模具有限公司 | Nickel-based superheat-resisting alloy stamping mould with self-lubricating coating |
CN105705670A (en) * | 2013-02-11 | 2016-06-22 | 康宁股份有限公司 | Coatings for glass-shaping molds and glass shaping molds comprising the same |
CN108474108A (en) * | 2016-01-20 | 2018-08-31 | 康宁股份有限公司 | It is used for the cated mold of tool of glass-based material forming at high temperature |
CN110304944A (en) * | 2019-07-15 | 2019-10-08 | 浙江星星科技股份有限公司 | A kind of surface treatment method of 3D hot bending graphite jig |
CN110723964A (en) * | 2019-09-30 | 2020-01-24 | 江西中材新材料有限公司 | Barrier layer, sintering mold and preparation method thereof |
CN110733098A (en) * | 2019-10-08 | 2020-01-31 | Oppo广东移动通信有限公司 | 3D ceramic shell, preparation method thereof and electronic equipment |
-
2020
- 2020-12-07 CN CN202011421304.7A patent/CN114589819A/en active Pending
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1830852A (en) * | 2005-03-10 | 2006-09-13 | 鸿富锦精密工业(深圳)有限公司 | Mould and its preparation method |
CN1899992A (en) * | 2005-07-19 | 2007-01-24 | 鸿富锦精密工业(深圳)有限公司 | Mould kernel and its preparing method |
CN102389922A (en) * | 2011-06-16 | 2012-03-28 | 昆山市瑞捷精密模具有限公司 | Nickel-based superheat-resisting alloy stamping mould with self-lubricating coating |
CN105705670A (en) * | 2013-02-11 | 2016-06-22 | 康宁股份有限公司 | Coatings for glass-shaping molds and glass shaping molds comprising the same |
CN108474108A (en) * | 2016-01-20 | 2018-08-31 | 康宁股份有限公司 | It is used for the cated mold of tool of glass-based material forming at high temperature |
CN110304944A (en) * | 2019-07-15 | 2019-10-08 | 浙江星星科技股份有限公司 | A kind of surface treatment method of 3D hot bending graphite jig |
CN110723964A (en) * | 2019-09-30 | 2020-01-24 | 江西中材新材料有限公司 | Barrier layer, sintering mold and preparation method thereof |
CN110733098A (en) * | 2019-10-08 | 2020-01-31 | Oppo广东移动通信有限公司 | 3D ceramic shell, preparation method thereof and electronic equipment |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN108794033A (en) | A kind of self toughening fibrous monolithic ceramic structural ceramics and preparation method thereof | |
CN105693255A (en) | Method for producing transparent ceramic component by injection molding | |
TW201022180A (en) | Aluminum-nitride-based composite material, method for manufacturing the same, and member for a semiconductor manufacturing apparatus | |
JP2007224386A (en) | Sintered target for manufacturing transparent conductive film, transparent conductive film manufactured by using the same, and transparent conductive base material | |
TW201228993A (en) | Sinter, sputtering target and molding die, and production process of sinter using the same | |
KR101534448B1 (en) | Flame Spray Coating Substrate Containing Rare-Earth Oxide and Method for Preparing the Same | |
JP4006535B2 (en) | Semiconductor or liquid crystal manufacturing apparatus member and manufacturing method thereof | |
TW200305479A (en) | Lapping carrier for use in fabricating sliders | |
CN106790791A (en) | A kind of cell phone rear cover with metal-like and preparation method thereof | |
CN112159946A (en) | Anti-sticking coating, carbon-based boat and preparation method of anti-sticking coating | |
CN101734925B (en) | Silicon nitride porous ceramic with controllable porosity and preparation method thereof | |
KR101452736B1 (en) | Method for producing a zirconia ceramic case having a logo for a portable electronic device | |
TW201505816A (en) | Heat insulation metal mold and method of manufacturing the same | |
CN114589819A (en) | Hot bending die and preparation method thereof, curved ceramic part and electronic equipment | |
CN107619282B (en) | A kind of preparation method of high toughness titanium silicon carbide-silicon carbide composite ceramic special-shaped parts | |
CN102350050B (en) | The preparation method of zircon gemstone go piece | |
JP5206716B2 (en) | In-Ga-Zn-based composite oxide sintered body and method for producing the same | |
CN107287546A (en) | Heat insulation cup prepared by a kind of utilization thermal spraying 3D printing technique and preparation method thereof | |
CN114959575A (en) | Insulating wear-resistant protective coating for thin film sensor, preparation method and application thereof | |
JP3756567B2 (en) | Mold for optical element molding | |
TWI335906B (en) | Die for press-molding glass and stripping method thereof | |
TWI262176B (en) | Mold for molding optical glass products and method for making the mold | |
JP5532064B2 (en) | Rare earth oxide-containing thermal spray substrate manufacturing method and laminate manufacturing method | |
KR20010008780A (en) | Titanium diboride sintered body with silicon nitride as a sintering aid and method for manufacture thereof | |
CN114959652B (en) | Composite film applied to metal surface, preparation method of composite film and metal product |
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 | ||
AD01 | Patent right deemed abandoned |
Effective date of abandoning: 20250325 |
|
AD01 | Patent right deemed abandoned |