CN108178648B - Three-dimensional carbon fiber reinforced alumina-zirconia composite material and preparation method thereof - Google Patents
Three-dimensional carbon fiber reinforced alumina-zirconia composite material and preparation method thereof Download PDFInfo
- Publication number
- CN108178648B CN108178648B CN201810008948.XA CN201810008948A CN108178648B CN 108178648 B CN108178648 B CN 108178648B CN 201810008948 A CN201810008948 A CN 201810008948A CN 108178648 B CN108178648 B CN 108178648B
- Authority
- CN
- China
- Prior art keywords
- carbon fiber
- alumina
- dimensional carbon
- zirconia composite
- zirconia
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- MCMNRKCIXSYSNV-UHFFFAOYSA-N ZrO2 Inorganic materials O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 title claims abstract description 245
- 239000002131 composite material Substances 0.000 title claims abstract description 218
- 229920000049 Carbon (fiber) Polymers 0.000 title claims abstract description 176
- 239000004917 carbon fiber Substances 0.000 title claims abstract description 176
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 title claims abstract description 170
- 238000002360 preparation method Methods 0.000 title claims abstract description 37
- 238000000034 method Methods 0.000 claims abstract description 53
- 238000010438 heat treatment Methods 0.000 claims abstract description 46
- 230000008569 process Effects 0.000 claims abstract description 27
- 238000001035 drying Methods 0.000 claims abstract description 20
- 238000007598 dipping method Methods 0.000 claims abstract description 6
- 239000000919 ceramic Substances 0.000 claims description 68
- 238000005470 impregnation Methods 0.000 claims description 39
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 37
- 239000012298 atmosphere Substances 0.000 claims description 15
- 239000003381 stabilizer Substances 0.000 claims description 15
- 239000002245 particle Substances 0.000 claims description 11
- 239000004744 fabric Substances 0.000 claims description 8
- 239000011148 porous material Substances 0.000 claims description 7
- 239000007787 solid Substances 0.000 claims description 7
- 229910017604 nitric acid Inorganic materials 0.000 claims description 6
- 238000010030 laminating Methods 0.000 claims description 4
- 239000002904 solvent Substances 0.000 claims description 4
- 238000002156 mixing Methods 0.000 claims description 3
- 238000009958 sewing Methods 0.000 claims 1
- 238000007254 oxidation reaction Methods 0.000 abstract description 14
- 230000003647 oxidation Effects 0.000 abstract description 13
- 230000004584 weight gain Effects 0.000 abstract description 6
- 235000019786 weight gain Nutrition 0.000 abstract description 6
- 230000000087 stabilizing effect Effects 0.000 abstract description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract 1
- 229910052799 carbon Inorganic materials 0.000 abstract 1
- 239000011159 matrix material Substances 0.000 description 33
- 239000002994 raw material Substances 0.000 description 30
- 239000000835 fiber Substances 0.000 description 23
- 239000012071 phase Substances 0.000 description 17
- 239000000843 powder Substances 0.000 description 15
- 239000000543 intermediate Substances 0.000 description 12
- 230000014759 maintenance of location Effects 0.000 description 10
- 238000005245 sintering Methods 0.000 description 10
- 238000012360 testing method Methods 0.000 description 10
- 239000002253 acid Substances 0.000 description 9
- 239000000243 solution Substances 0.000 description 8
- 238000005452 bending Methods 0.000 description 7
- 239000000203 mixture Substances 0.000 description 7
- 238000000280 densification Methods 0.000 description 6
- 239000007788 liquid Substances 0.000 description 6
- 239000007791 liquid phase Substances 0.000 description 6
- 230000002787 reinforcement Effects 0.000 description 6
- 238000011160 research Methods 0.000 description 6
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 5
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 5
- 238000006243 chemical reaction Methods 0.000 description 5
- 239000011261 inert gas Substances 0.000 description 5
- 238000007781 pre-processing Methods 0.000 description 5
- 239000007790 solid phase Substances 0.000 description 5
- 230000003068 static effect Effects 0.000 description 5
- 229910052726 zirconium Inorganic materials 0.000 description 5
- 239000011165 3D composite Substances 0.000 description 4
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 4
- 230000006378 damage Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000011049 filling Methods 0.000 description 4
- 230000003014 reinforcing effect Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000008021 deposition Effects 0.000 description 3
- 238000001514 detection method Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 229910017053 inorganic salt Inorganic materials 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000012266 salt solution Substances 0.000 description 3
- 239000002002 slurry Substances 0.000 description 3
- 238000002441 X-ray diffraction Methods 0.000 description 2
- 239000000654 additive Substances 0.000 description 2
- 230000003064 anti-oxidating effect Effects 0.000 description 2
- 239000012300 argon atmosphere Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000007731 hot pressing Methods 0.000 description 2
- 230000007062 hydrolysis Effects 0.000 description 2
- 238000006460 hydrolysis reaction Methods 0.000 description 2
- 230000008595 infiltration Effects 0.000 description 2
- 238000001764 infiltration Methods 0.000 description 2
- 238000003475 lamination Methods 0.000 description 2
- 239000004745 nonwoven fabric Substances 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 238000006722 reduction reaction Methods 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910001928 zirconium oxide Inorganic materials 0.000 description 2
- 230000002378 acidificating effect Effects 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 235000008429 bread Nutrition 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000002738 chelating agent Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000007865 diluting Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002105 nanoparticle Substances 0.000 description 1
- YPJKMVATUPSWOH-UHFFFAOYSA-N nitrooxidanyl Chemical compound [O][N+]([O-])=O YPJKMVATUPSWOH-UHFFFAOYSA-N 0.000 description 1
- 238000002203 pretreatment Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 239000011226 reinforced ceramic Substances 0.000 description 1
- 239000011208 reinforced composite material Substances 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
- 150000003754 zirconium Chemical class 0.000 description 1
Images
Classifications
-
- 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
- C04B35/01—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
- C04B35/48—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 zirconium or hafnium oxides, zirconates, zircon or hafnates
-
- 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
-
- 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
- C04B2235/3217—Aluminum oxide or oxide forming salts thereof, e.g. bauxite, alpha-alumina
-
- 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
- C04B2235/3244—Zirconium oxides, zirconates, hafnium oxides, hafnates, 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
- C04B2235/70—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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Composite Materials (AREA)
- Compositions Of Oxide Ceramics (AREA)
Abstract
本发明公开了一种三维碳纤维增强氧化铝‑氧化锆复合材料及其制备方法,制备方法包括以下步骤:(1)对氧化铝‑氧化锆复合溶胶进行稳定;(2)将三维碳纤维预制件真空浸渍于氧化铝‑氧化锆复合溶胶中;(3)干燥浸渍后的三维碳纤维预制件;(4)热处理;(5)重复步骤(2)~(4)的浸渍‑干燥‑热处理过程,直至三维碳纤维增强氧化铝‑氧化锆复合材料中间体相比于上一次浸渍‑干燥‑热处理过程增重低于1%,得到三维碳纤维增强氧化铝‑氧化锆复合材料。本发明制备的三维碳纤维增强氧化铝‑氧化锆复合材料具有耐高温、抗氧化和力学性能优良等优点。
The invention discloses a three-dimensional carbon fiber reinforced alumina-zirconia composite material and a preparation method thereof. The preparation method comprises the following steps: (1) stabilizing the alumina-zirconia composite sol; (2) vacuuming the three-dimensional carbon fiber preform dipping in alumina-zirconia composite sol; (3) drying the impregnated three-dimensional carbon fiber preform; (4) heat treatment; (5) repeating the impregnation-drying-heat treatment process of steps (2) to (4) until three-dimensional Compared with the previous impregnation-drying-heat treatment process, the carbon fiber reinforced alumina-zirconia composite material has a weight gain of less than 1%, and a three-dimensional carbon fiber-reinforced alumina-zirconia composite material is obtained. The three-dimensional carbon fiber reinforced alumina-zirconia composite material prepared by the invention has the advantages of high temperature resistance, oxidation resistance and excellent mechanical properties.
Description
技术领域technical field
本发明属于耐高温的纤维增强陶瓷基复合材料及其制备技术领域,尤其涉及一种三维碳纤维预制件增强氧化铝-氧化锆复相陶瓷复合材料及其制备方法。The invention belongs to the high temperature resistant fiber reinforced ceramic matrix composite material and the technical field of preparation thereof, in particular to a three-dimensional carbon fiber preform reinforced alumina-zirconia composite ceramic composite material and a preparation method thereof.
背景技术Background technique
氧化铝-氧化锆复相陶瓷兼具氧化铝和氧化锆的耐高温、抗氧化、耐蠕变、耐腐蚀等优点,是一种优良的耐高温陶瓷材料,作为热障和防护涂层、航空发动机涡轮叶片等得到较多研究。作为单体陶瓷,氧化铝-氧化锆复相陶瓷的断裂韧性较低,大多数情况下为4~5MPa·m1/2。如此低的断裂韧性导致单体氧化铝-氧化锆复相陶瓷很难作为结构材料获得实际应用,特别是在具有较大机械载荷冲击、热冲击的场合,必须要进行增韧处理。Alumina-zirconia composite ceramics have the advantages of high temperature resistance, oxidation resistance, creep resistance and corrosion resistance of alumina and zirconia. Engine turbine blades have been studied a lot. As a single ceramic, the fracture toughness of alumina-zirconia composite ceramics is relatively low, in most cases 4-5 MPa·m 1/2 . Such a low fracture toughness makes it difficult for single alumina-zirconia composite ceramics to be practically used as structural materials, especially in the occasions with large mechanical load shock and thermal shock, which must be toughened.
在陶瓷基体中引入纤维,已经被证明是能够显著提高断裂韧性的最为有效的增韧方法。在增强纤维中,碳纤维因成本低、耐高温、拉伸强度高、易编织成型复杂形状等优点而成为使用最为广泛的增强体。因此,若能将碳纤维与氧化铝-氧化锆复相陶瓷复合在一起,结合两者的优势,理论上有望获得兼具耐高温、抗氧化、高强度、高韧性的纤维增强氧化铝-氧化锆复相陶瓷复合材料。Introducing fibers into a ceramic matrix has been shown to be the most effective toughening method to significantly increase fracture toughness. Among the reinforcing fibers, carbon fibers have become the most widely used reinforcements due to their advantages of low cost, high temperature resistance, high tensile strength, and easy weaving to form complex shapes. Therefore, if carbon fiber and alumina-zirconia composite ceramics can be composited together, combining the advantages of both, it is theoretically expected to obtain fiber-reinforced alumina-zirconia with high temperature resistance, oxidation resistance, high strength and high toughness. Multiphase ceramic composites.
按照纤维在复合材料中的排布方式,即纤维预制件的结构形式,可以分为一维、二维、三维预制件增强复合材料。一维复合材料是指将纤维束通过陶瓷基体粉末配制成的泥浆(浆料中有粘接剂将陶瓷粉末粘附在纤维上)缠绕成无纬布,再将无纬布按不同方向、不同角度铺层,或者直接按不同方向、不同角度缠绕成所需形状,然后经高温无压或者热压烧结得到的复合材料。二维复合材料是指通过涂刷、浸涂陶瓷基体粉末配制成的泥浆等方式在纤维布表面粘附上陶瓷基体,将纤维布叠层后,经高温无压或者热压烧结得到的复合材料。三维复合材料是指先将纤维制作成三维立体的预制件,然后通过气相法、液相法等手段将陶瓷基体引入预制件中所得到的复合材料。相比较而言,三维复合材料的整体性较优(一维和二维复合材料的面内、层间性能较弱),纤维含量与排布方向性的可设计性强,更加适用于复杂形状构件的制备。According to the arrangement of fibers in the composite material, that is, the structural form of the fiber preform, it can be divided into one-dimensional, two-dimensional, and three-dimensional preform-reinforced composite materials. One-dimensional composite material refers to a slurry prepared by passing fiber bundles through a ceramic matrix powder (there is a binder in the slurry to adhere the ceramic powder to the fibers) into a non-woven fabric, and then the non-woven fabric is wound in different directions and different directions. Angle layup, or directly wound into the desired shape in different directions and angles, and then sintered at high temperature without pressure or hot pressing. The two-dimensional composite material refers to the composite material obtained by adhering the ceramic matrix on the surface of the fiber cloth by brushing or dipping the slurry prepared by the ceramic matrix powder, and then laminating the fiber cloth and sintering at high temperature without pressure or hot pressing. . The three-dimensional composite material refers to the composite material obtained by first making the fibers into a three-dimensional preform, and then introducing the ceramic matrix into the preform by means of gas phase method and liquid phase method. In comparison, the integrity of 3D composites is better (one-dimensional and two-dimensional composites have weak in-plane and interlayer properties), and the fiber content and arrangement direction are highly designable, making them more suitable for complex-shaped components. preparation.
然而,由于预制件结构的不同,三维复合材料的致密化难以照搬一维、二维复合材料的制备工艺。针对三维预制件的结构特点,目前通常采用两种致密化方法:一是将预制件加热到所需温度后,通入气态原料,原料扩散至预制件中在高温作用下反应沉积得到陶瓷基体,随着沉积时间延长,预制件中孔隙逐渐被陶瓷基体填充,致密度不断增加,称之为气相法;二是将预制件浸渍液态原料后,干燥去除溶剂,然后在高温下热处理得到陶瓷基体,重复“浸渍-干燥-热处理”若干个周期,预制件中孔隙逐渐被陶瓷基体填充,致密度不断增加,称之为液相法。相比之下,液相法对设备的要求低,对复合时设备中的温度场、化学场不敏感,在复杂形状和批量构件制备时的优势更加明显。而且对于纤维增强氧化铝-氧化锆复相陶瓷复合材料而言,目前适合用于沉积氧化铝和氧化锆的气态原料太少,沉积特性也不够理想,液态原料则比较容易获得,性能可靠。However, due to the different structures of preforms, the densification of 3D composites is difficult to copy the preparation process of 1D and 2D composites. According to the structural characteristics of the three-dimensional preform, two densification methods are usually used at present: one is to heat the preform to the required temperature, then feed the gaseous raw material, and the raw material diffuses into the preform and reacts and deposits the ceramic matrix under the action of high temperature. As the deposition time prolongs, the pores in the preform are gradually filled with the ceramic matrix, and the density increases continuously, which is called the gas phase method; the second is to immerse the preform in the liquid raw material, dry to remove the solvent, and then heat treatment at high temperature to obtain the ceramic matrix. Repeating several cycles of "dipping-drying-heat treatment", the pores in the preform are gradually filled with the ceramic matrix, and the density increases continuously, which is called the liquid phase method. In contrast, the liquid phase method has low requirements on equipment, is not sensitive to the temperature field and chemical field in the equipment during compounding, and has more obvious advantages in the preparation of complex shapes and batch components. Moreover, for fiber-reinforced alumina-zirconia composite ceramic composites, there are currently too few gaseous raw materials suitable for the deposition of alumina and zirconia, and the deposition characteristics are not ideal. Liquid raw materials are relatively easy to obtain and have reliable performance.
对于液相法而言,如何快速制备出高致密度、高力学性能的三维纤维预制件增强氧化铝-氧化锆复相陶瓷复合材料,是需要解决的一个关键问题,所涉及的关键技术点包括液态原料性质、浸渍工艺、热处理工艺。目前还未发现通过液相法制备三维碳纤维预制件增强氧化铝-氧化锆复相陶瓷复合材料的研究报道。For the liquid phase method, how to quickly prepare a three-dimensional fiber preform reinforced alumina-zirconia composite ceramic composite material with high density and high mechanical properties is a key problem that needs to be solved. The key technical points involved include: Liquid raw material properties, impregnation process, heat treatment process. There is no research report on the preparation of three-dimensional carbon fiber preform reinforced alumina-zirconia composite ceramic composites by liquid phase method.
发明内容SUMMARY OF THE INVENTION
本发明要解决的技术问题是克服现有技术的不足,提供一种耐高温、抗氧化和力学性能优良的三维碳纤维增强氧化铝-氧化锆复合材料及其制备方法。The technical problem to be solved by the present invention is to overcome the deficiencies of the prior art and provide a three-dimensional carbon fiber reinforced alumina-zirconia composite material with excellent high temperature resistance, oxidation resistance and mechanical properties and a preparation method thereof.
为解决上述技术问题,本发明采用以下技术方案:In order to solve the above-mentioned technical problems, the present invention adopts the following technical solutions:
一种三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,包括以下步骤:A preparation method of a three-dimensional carbon fiber reinforced alumina-zirconia composite material, comprising the following steps:
(1)制备氧化铝-氧化锆复合溶胶:将氧化铝溶胶和氧化锆溶胶混合,加入稳定剂,得到氧化铝-氧化锆复合溶胶;(1) Preparation of alumina-zirconia composite sol: mixing alumina sol and zirconia sol, adding stabilizer to obtain alumina-zirconia composite sol;
(2)浸渍:将三维碳纤维预制件置于容器中,抽真空后吸入步骤(1)所得的氧化铝-氧化锆复合溶胶,进行真空浸渍,使所述氧化铝-氧化锆复合溶胶填充在三维碳纤维预制件中;(2) Impregnation: The three-dimensional carbon fiber preform is placed in a container, and after vacuuming, the alumina-zirconia composite sol obtained in step (1) is inhaled, and vacuum impregnation is performed, so that the alumina-zirconia composite sol is filled in the three-dimensional composite sol. In carbon fiber prefabs;
(3)干燥:将三维碳纤维预制件取出干燥,以去除氧化铝-氧化锆复合溶胶中的溶剂和稳定剂;(3) Drying: The three-dimensional carbon fiber preform is taken out and dried to remove the solvent and stabilizer in the alumina-zirconia composite sol;
(4)热处理:在惰性气氛保护下进行热处理,得到三维碳纤维增强氧化铝-氧化锆复合材料中间体;(4) Heat treatment: heat treatment under the protection of an inert atmosphere to obtain a three-dimensional carbon fiber reinforced alumina-zirconia composite intermediate;
(5)重复步骤(2)~(4)的浸渍-干燥-热处理过程,直至三维碳纤维增强氧化铝-氧化锆复合材料中间体相比于上一次浸渍-干燥-热处理过程增重低于1%,得到三维碳纤维增强氧化铝-氧化锆复合材料。(5) Repeat the impregnation-drying-heat treatment process of steps (2) to (4) until the weight gain of the three-dimensional carbon fiber reinforced alumina-zirconia composite material intermediate is less than 1% compared with the previous impregnation-drying-heat treatment process , to obtain three-dimensional carbon fiber reinforced alumina-zirconia composites.
上述的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,优选的,所述步骤(1)中,所述稳定剂包括HNO3、HCl或H2SO4中的一种或多种。In the above-mentioned preparation method of a three-dimensional carbon fiber reinforced alumina-zirconia composite material, preferably, in the step (1), the stabilizer includes one or more of HNO 3 , HCl or H 2 SO 4 .
上述的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,优选的,所述稳定剂的加入量为氧化铝溶胶质量的20%~30%。In the above-mentioned preparation method of the three-dimensional carbon fiber reinforced alumina-zirconia composite material, preferably, the added amount of the stabilizer is 20% to 30% of the mass of the alumina sol.
上述的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,优选的,所述步骤(1)中,所述氧化铝-氧化锆复合溶胶中,固含量为20wt%~40wt%,氧化铝与氧化锆的摩尔比为95/5~5/95,复合溶胶的胶粒尺寸≤30nm。For the preparation method of the above three-dimensional carbon fiber reinforced alumina-zirconia composite material, preferably, in the step (1), in the alumina-zirconia composite sol, the solid content is 20wt% to 40wt%, and the alumina and The molar ratio of zirconia is 95/5 to 5/95, and the particle size of the composite sol is less than or equal to 30 nm.
上述的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,优选的,所述步骤(3)中,干燥温度为350℃~750℃,干燥时间为1h~6h。In the above-mentioned preparation method of the three-dimensional carbon fiber reinforced alumina-zirconia composite material, preferably, in the step (3), the drying temperature is 350℃~750℃, and the drying time is 1h~6h.
上述的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,优选的,所述步骤(2)中,所述真空浸渍的工艺条件为:真空度≤500Pa,浸渍时间为4h~8h。In the above-mentioned preparation method of the three-dimensional carbon fiber reinforced alumina-zirconia composite material, preferably, in the step (2), the vacuum impregnation process conditions are: vacuum degree≤500Pa, and the impregnation time is 4h-8h.
上述的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,优选的,所述步骤(2)中,真空浸渍后还包括在设定压力下进行气压辅助浸渍,使所述氧化铝-氧化锆复合溶胶进一步填充在三维碳纤维预制件中,所述气压辅助浸渍的工艺条件为:所述设定压力为2MPa~10MPa,浸渍时间为2h~6h。In the above-mentioned preparation method of the three-dimensional carbon fiber reinforced alumina-zirconia composite material, preferably, in the step (2), after the vacuum impregnation, it also includes air pressure-assisted impregnation under a set pressure to make the alumina-zirconia The composite sol is further filled in the three-dimensional carbon fiber preform, and the process conditions of the air pressure-assisted impregnation are: the set pressure is 2MPa-10MPa, and the impregnation time is 2h-6h.
上述的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,优选的,所述步骤(4)中,所述热处理的工艺过程为:在惰性气氛保护下,以10℃/min~20℃/min的速率升温至1100℃~1500℃,保温0.5h~2h。For the preparation method of the above-mentioned three-dimensional carbon fiber reinforced alumina-zirconia composite material, preferably, in the step (4), the process of the heat treatment is as follows: under the protection of an inert atmosphere, the temperature is 10°C/min~20°C/min. The temperature was raised to 1100°C to 1500°C at a rate of min, and the temperature was kept for 0.5h to 2h.
上述的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,优选的,在所述步骤(2)之前还包括三维碳纤维预制件预处理步骤,具体为:将所述三维碳纤维预制件置于真空或惰性气氛下,以10℃/min~20℃/min的速率升温至1400℃~1800℃并保温1h~4h。The preparation method of the above-mentioned three-dimensional carbon fiber reinforced alumina-zirconia composite material, preferably, before the step (2), it further includes a three-dimensional carbon fiber preform preprocessing step, specifically: placing the three-dimensional carbon fiber preform in a vacuum Or in an inert atmosphere, the temperature is raised to 1400°C to 1800°C at a rate of 10°C/min to 20°C/min and kept for 1h to 4h.
上述的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,优选的,所述三维碳纤维预制件为碳纤维布叠层缝合得到的三维碳纤维预制件、碳纤维布与网胎交替叠层针刺得到的三维碳纤维预制件、三维五向编织结构的三维碳纤维预制件、二维半编织结构的三维碳纤维预制件、三维四向编织结构的三维碳纤维预制件中的一种或多种;所述三维碳纤维预制件中碳纤维的体积分数为25%~55%。For the preparation method of the above-mentioned three-dimensional carbon fiber reinforced alumina-zirconia composite material, preferably, the three-dimensional carbon fiber preform is a three-dimensional carbon fiber preform obtained by lamination and stitching of carbon fiber cloth, and a carbon fiber cloth and a mesh tire alternately laminated and needled. One or more of three-dimensional carbon fiber preforms, three-dimensional carbon fiber preforms with a three-dimensional five-way braided structure, three-dimensional carbon fiber preforms with a two-dimensional semi-braided structure, and three-dimensional carbon fiber preforms with a three-dimensional four-way braided structure; the three-dimensional carbon fiber preforms The volume fraction of carbon fiber in the piece is 25% to 55%.
作为一个总的发明构思,本发明还提供一种上述的制备方法制得的三维碳纤维增强氧化铝-氧化锆复合材料,包括三维碳纤维预制件和氧化铝-氧化锆复相陶瓷,所述氧化铝-氧化锆复相陶瓷中,氧化锆的摩尔含量为5%~95%,所述氧化铝-氧化锆复相陶瓷均匀填充于三维碳纤维预制件的孔隙中,所述三维碳纤维增强氧化铝-氧化锆复合材料的孔隙率为10%~17%。As a general inventive concept, the present invention also provides a three-dimensional carbon fiber reinforced alumina-zirconia composite material prepared by the above preparation method, including a three-dimensional carbon fiber preform and an alumina-zirconia composite ceramic, the alumina -In the zirconia multiphase ceramics, the molar content of zirconia is 5% to 95%, the alumina-zirconia multiphase ceramics are uniformly filled in the pores of the three-dimensional carbon fiber preform, and the three-dimensional carbon fiber reinforced alumina-oxidized The porosity of zirconium composites is 10% to 17%.
与现有技术相比,本发明的优点在于:Compared with the prior art, the advantages of the present invention are:
1、本发明以氧化铝-氧化锆复合溶胶为液态原料,采用液相法制备三维碳纤维增强氧化铝-氧化锆复合材料,高固含量、纳米尺度的溶胶可以使氧化铝-氧化锆粒子快速、均匀地填充到预制件中的空隙中,相比于从溶液出发的技术路线,致密化效率高;相比于以陶瓷粉末配制成的泥浆为原料的技术路线,氧化铝-氧化锆粒子的分布均匀性好,且生成氧化铝-氧化锆复相陶瓷的温度低,对纤维的损伤小。1. The present invention uses the alumina-zirconia composite sol as the liquid raw material, and adopts the liquid phase method to prepare the three-dimensional carbon fiber reinforced alumina-zirconia composite material. The high solid content and nano-scale sol can make the alumina-zirconia particles fast, It is uniformly filled into the voids in the preform, and the densification efficiency is high compared to the technical route starting from the solution; The uniformity is good, and the temperature of forming alumina-zirconia composite ceramics is low, and the damage to the fiber is small.
本发明在制备三维碳纤维增强氧化铝-氧化锆复合材料的过程中,在液态原料氧化铝-氧化锆复合溶胶中引入酸液作为稳定剂,解决了氧化铝溶胶和氧化锆溶胶因水解速度明显不同而导致的相容性差的问题,获得了稳定的氧化铝-氧化锆复合溶胶,为复合材料的制备提供了可靠的原料保障。申请人在制备氧化铝-氧化锆复合溶胶的过程中发现,氧化铝溶胶和氧化锆溶胶混合后发生沉淀,沉淀破坏了溶胶中纳米尺寸胶体粒子的单分散状态,得到的是大尺寸团聚状态的颗粒,无法浸渍到纤维预制件的孔隙中去,不能用作“浸渍-干燥-热处理”技术路线的原料。前期曾尝试通过稀释、添加螯合剂等方式(原理为增加空间位阻,降低胶体粒子的碰撞机率)来稳定氧化铝-氧化锆复合溶胶,但一是稳定化效果并不太理想,二是会在一定程度上降低复合溶胶的固含量,从而降低复合材料的制备效率。为了更好地稳定氧化铝-氧化锆复合溶胶, 申请人对氧化铝溶胶和氧化锆溶胶混合后产生沉淀的原因进行了深入的理论研究和实践探索,研究结果表明:氧化铝溶胶为碱性,氧化锆溶胶为酸性,因而两者混合时,pH值失配,溶胶失稳,发生沉淀。本发明逆向思维,根据氧化铝溶胶和氧化锆溶胶合成过程中的水解机理,通过添加酸液使得已经水解的胶体粒子部分胶溶,从而减少了碰撞失稳机率,同时将两者的pH值调整到同一水平,明显提高了复合溶胶的稳定性,也不会降低复合溶胶的固含量与复合效率。另外,添加酸液还能在一定程度上降低复合溶胶的粘度,从而有利于向纤维预制件中的浸渍。In the process of preparing the three-dimensional carbon fiber reinforced alumina-zirconia composite material, acid solution is introduced into the liquid raw material alumina-zirconia composite sol as a stabilizer, which solves the problem that the hydrolysis speed of alumina sol and zirconia sol is obviously different. However, due to the problem of poor compatibility, a stable alumina-zirconia composite sol is obtained, which provides a reliable raw material guarantee for the preparation of composite materials. In the process of preparing the alumina-zirconia composite sol, the applicant found that the alumina sol and the zirconia sol were mixed and precipitated. The particles cannot be impregnated into the pores of the fiber preform and cannot be used as raw materials for the "impregnation-drying-heat treatment" technical route. Earlier attempts were made to stabilize the alumina-zirconia composite sol by diluting and adding chelating agents (the principle is to increase steric hindrance and reduce the collision probability of colloidal particles), but first, the stabilization effect is not ideal, and second, it will To a certain extent, the solid content of the composite sol is reduced, thereby reducing the preparation efficiency of the composite material. In order to better stabilize the alumina-zirconia composite sol, the applicant has conducted in-depth theoretical research and practical exploration on the causes of precipitation after mixing alumina sol and zirconia sol. The research results show that the alumina sol is alkaline, Zirconia sol is acidic, so when the two are mixed, the pH value is mismatched, the sol is destabilized, and precipitation occurs. The present invention reverses its thinking, according to the hydrolysis mechanism in the synthesis process of alumina sol and zirconia sol, by adding acid solution to partially peptize the hydrolyzed colloidal particles, thereby reducing the probability of collision instability, and adjusting the pH value of the two at the same time At the same level, the stability of the composite sol is significantly improved, and the solid content and composite efficiency of the composite sol are not reduced. In addition, the addition of the acid solution can also reduce the viscosity of the composite sol to a certain extent, thereby facilitating the impregnation into the fiber preform.
酸液优选为强酸,强酸对氧化铝-氧化锆复合溶胶的稳定效果优于弱酸,其中,硝酸对氧化铝-氧化锆复合溶胶的稳定效果最佳。The acid solution is preferably a strong acid, and the stabilizing effect of the strong acid on the alumina-zirconia composite sol is better than that of the weak acid. Among them, nitric acid has the best stabilizing effect on the alumina-zirconia composite sol.
2、由于氧化铝-氧化锆复合溶胶中含有稳定剂,它会以酸根的形式残留在凝胶中,若不能在较低温度下将其排除干净,会影响高温下氧化铝和氧化锆的反应与烧结,同时也会损伤碳纤维。本发明选择在干燥阶段通过提高干燥温度(350℃~750℃)将其去除,在这个温度范围内,酸根将被分解,如硝酸根能够分解成NOx和O2而排除干净,这样在高温下就不会因有气体挥发而影响氧化铝和氧化锆的反应与烧结收缩,同时又不至于对碳纤维造成明显的损伤。2. Since the alumina-zirconia composite sol contains stabilizers, it will remain in the gel in the form of acid radicals. If it cannot be removed at a lower temperature, it will affect the reaction of alumina and zirconia at high temperatures. With sintering, it will also damage the carbon fiber. The present invention chooses to remove it by increasing the drying temperature (350 ℃ ~ 750 ℃) in the drying stage. In this temperature range, the acid radical will be decomposed, for example, the nitrate radical can be decomposed into NO x and O 2 and be eliminated completely, so that at high temperature It will not affect the reaction and sintering shrinkage of alumina and zirconia due to gas volatilization, and will not cause obvious damage to the carbon fiber.
3、优选的,本发明所用溶胶中,氧化铝-氧化锆均为无定形态,又为纳米尺度,其表面能很高,因而具有高的烧结活性,为复合材料的高温热处理提供了优质的原料保障。3. Preferably, in the sol used in the present invention, alumina and zirconia are both amorphous and nanoscale, and their surface energy is very high, so they have high sintering activity, which provides high-quality composite materials for high-temperature heat treatment. Raw material guarantee.
4、优选的,本发明在浸渍阶段,采用先真空浸渍然后气压辅助浸渍方式,先抽真空排除掉预制中空隙中的空气,为溶胶的渗入提供空间,由于溶胶中是纳米尺寸的单颗粒均匀分散的氧化铝-氧化锆复合胶体粒子,具有很好的稳定性,因而能够迅速、均匀地进入预制件的空隙中;然后通过外部气压作用,促进溶胶进一步向预制件内部渗入,进入一些孔道复杂的空隙中,甚至能够破坏一些闭孔使其变成开孔,从而提高浸渍效率和填充程度。4. Preferably, in the impregnation stage of the present invention, the method of first vacuum impregnation and then air pressure assisted impregnation is adopted, and the air in the prefabricated void is firstly removed by vacuuming, so as to provide space for the infiltration of the sol, because the nano-sized single particles in the sol are uniform The dispersed alumina-zirconia composite colloidal particles have good stability, so they can quickly and uniformly enter the voids of the preform; and then through the action of external air pressure, the sol is further infiltrated into the preform, entering some complex pores. In the voids, some closed cells can even be destroyed to turn them into open cells, thereby improving the impregnation efficiency and filling degree.
5、优选地,本发明在选择无定形态、粒径小且稳定的氧化铝-氧化锆复合溶胶作为复合材料基体原料的基础上,通过对氧化铝-氧化锆烧结收缩行为的研究,把热处理温度设定为1100℃~1500℃,在这个温度范围内,既能确保氧化铝-氧化锆转化成氧化铝-氧化锆复相陶瓷,又能获得较高的基体致密度(提高基体承受载荷和传递载荷的能力),最终获得综合性能优良的三维碳纤维预制件增强氧化铝-氧化锆复相陶瓷复合材料。5. Preferably, in the present invention, on the basis of selecting amorphous, small and stable alumina-zirconia composite sol as the matrix raw material of the composite material, through the research on the sintering shrinkage behavior of alumina-zirconia, heat treatment The temperature is set at 1100℃~1500℃, within this temperature range, it can not only ensure the conversion of alumina-zirconia into alumina-zirconia composite ceramics, but also obtain a higher matrix density (increase the substrate bearing load and The ability to transfer load), and finally obtain a three-dimensional carbon fiber preform reinforced alumina-zirconia composite ceramic composite with excellent comprehensive properties.
总之,本发明从液态原料特性、浸渍工艺、干燥工艺、热处理温度四方面着手,显著提高了三维碳纤维预制件增强氧化铝-氧化锆复相陶瓷复合材料的致密程度,既增强了基体本身的承载能力,又增强了基体传递载荷的能力,因而所制备的三维碳纤维增强氧化铝-氧化锆复合材料呈现出优良的力学性能、耐高温性能和抗氧化性能。In a word, the present invention starts from the characteristics of liquid raw materials, impregnation process, drying process, and heat treatment temperature, and significantly improves the density of the three-dimensional carbon fiber preform reinforced alumina-zirconia composite ceramic composite material, which not only enhances the bearing capacity of the matrix itself Therefore, the prepared three-dimensional carbon fiber reinforced alumina-zirconia composite material exhibits excellent mechanical properties, high temperature resistance and oxidation resistance.
6、本发明制备的三维碳纤维增强氧化铝-氧化锆复合材料,首次将碳纤维、氧化铝-氧化锆复相陶瓷、三维预制件三者的优势结合在一起,具有耐高温、抗氧化以及优良的力学性能等优点。具体地,利用三维碳纤维预制件的力学特性提供优良的力学性能,尤其是提供高的断裂韧性,克服了单体氧化铝-氧化锆复相陶瓷的脆性;利用氧化铝-氧化锆复相陶瓷优良的抗氧化特性,对碳纤维进行包裹和保护,提供复合材料优良的抗氧化性能;利用碳纤维的耐高温特性与氧化铝-氧化锆复相陶瓷的高熔点,提供复合材料优良的耐高温能力。并且,该复合材料孔隙率较低(10%~17%),也即氧化铝-氧化锆复相陶瓷的含量和致密度高,因而该复合材料的力学性能、耐高温性能和抗氧化性能得以进一步提高。6. The three-dimensional carbon fiber reinforced alumina-zirconia composite material prepared by the present invention combines the advantages of carbon fiber, alumina-zirconia composite ceramics and three-dimensional prefabricated parts for the first time, and has high temperature resistance, oxidation resistance and excellent performance. mechanical properties, etc. Specifically, the mechanical properties of the three-dimensional carbon fiber preform are used to provide excellent mechanical properties, especially high fracture toughness, which overcomes the brittleness of the single alumina-zirconia composite ceramics; the use of alumina-zirconia composite ceramics provides excellent mechanical properties. The anti-oxidation properties of carbon fiber are wrapped and protected to provide excellent anti-oxidation properties of composite materials; the high-temperature resistance properties of carbon fibers and the high melting point of alumina-zirconia composite ceramics are used to provide excellent high-temperature resistance capabilities of composite materials. In addition, the porosity of the composite material is low (10% to 17%), that is, the content and density of the alumina-zirconia composite ceramics are high, so the mechanical properties, high temperature resistance and oxidation resistance of the composite material are improved. Further improve.
附图说明Description of drawings
图1为本发明实施例1所制备的三维碳纤维增强氧化铝-氧化锆复合材料的宏观照片。FIG. 1 is a macro photo of the three-dimensional carbon fiber reinforced alumina-zirconia composite material prepared in Example 1 of the present invention.
图2为本发明实施例1所制备的三维碳纤维增强氧化铝-氧化锆复合材料的微观结构图。FIG. 2 is a microstructure diagram of the three-dimensional carbon fiber reinforced alumina-zirconia composite material prepared in Example 1 of the present invention.
图3为本发明的基体原料氧化铝-氧化锆复合溶胶(Al2O3与ZrO2的摩尔比为1∶0.3)经干燥所得凝胶粉末的XRD图谱。Figure 3 is the XRD pattern of the gel powder obtained by drying the matrix raw material alumina-zirconia composite sol (the molar ratio of Al 2 O 3 and ZrO 2 is 1:0.3).
图4为本发明的基体原料氧化铝-氧化锆复合溶胶(Al2O3与ZrO2的摩尔比为1∶0.3)经干燥后的凝胶粉末,经压制成块后,在不同温度下热处理后的线收缩情况。Figure 4 is the dried gel powder of the matrix raw material alumina-zirconia composite sol (the molar ratio of Al 2 O 3 and ZrO 2 is 1:0.3) of the present invention. After being pressed into blocks, heat treatment at different temperatures After the line shrinks.
图5为本发明的基体原料氧化铝-氧化锆复合溶胶(Al2O3与ZrO2的摩尔比为1∶0.3)经干燥后的凝胶粉末,在不同温度热处理后的XRD图谱。Figure 5 shows the XRD patterns of the dried gel powder of the matrix raw material alumina-zirconia composite sol (molar ratio of Al 2 O 3 and ZrO 2 is 1:0.3) after heat treatment at different temperatures.
具体实施方式Detailed ways
以下结合说明书附图和具体优选的实施例对本发明作进一步描述,但并不因此而限制本发明的保护范围。The present invention will be further described below with reference to the accompanying drawings and specific preferred embodiments, but the protection scope of the present invention is not limited thereby.
实施例1:Example 1:
一种本发明的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,包括以下具体工艺步骤:A preparation method of a three-dimensional carbon fiber reinforced alumina-zirconia composite material of the present invention comprises the following specific process steps:
(1)溶胶选取:选取固相含量为30wt%的氧化铝-氧化锆复合溶胶作为氧化铝-氧化锆复相陶瓷基体的原料,其中氧化铝与氧化锆摩尔比为1∶0.3,在上述氧化铝-氧化锆复合溶胶中加入HNO3作为稳定剂,HNO3的加入量为氧化铝溶胶重量的25%。(1) Sol selection: Select an alumina-zirconia composite sol with a solid phase content of 30 wt% as the raw material for the alumina-zirconia composite ceramic matrix, wherein the molar ratio of alumina and zirconia is 1:0.3. HNO 3 was added to the aluminum-zirconia composite sol as a stabilizer, and the amount of HNO 3 was 25% of the weight of the alumina sol.
(2)预制件预处理:选取碳纤维布叠层缝合得到的三维碳纤维预制件为增强相,三维碳纤维预制件中纤维的体积分数为48%。将选取的三维碳纤维预制件置于真空下,以20℃/min的速率升温至1400℃并保温2h,然后随炉降温,完成预制件的预处理。(2) Pre-processing of preforms: The three-dimensional carbon fiber preform obtained by lamination and stitching of carbon fiber cloth is selected as the reinforcement phase, and the volume fraction of fibers in the three-dimensional carbon fiber preform is 48%. The selected three-dimensional carbon fiber preforms were placed under vacuum, heated to 1400°C at a rate of 20°C/min and kept for 2 h, and then cooled with the furnace to complete the pretreatment of the preforms.
(3)真空浸渍:将经预处理的三维碳纤维预制件置于真空罐中,抽真空至真空度达到300Pa时,吸入步骤(1)的氧化铝-氧化锆复合溶胶,使氧化铝-氧化锆复合溶胶淹没三维碳纤维预制件,浸泡6h。(3) Vacuum impregnation: place the pretreated three-dimensional carbon fiber preform in a vacuum tank, and when the vacuum degree reaches 300Pa, inhale the alumina-zirconia composite sol of step (1) to make the alumina-zirconia composite sol. The composite sol submerged the three-dimensional carbon fiber preform for 6 hours.
(4)气压辅助浸渍:将预制件(仍浸泡在溶胶中)移至压力釜中,充气至4MPa,进行气压辅助浸渍,保持4h。(4) Air pressure-assisted impregnation: Move the preform (still immersed in the sol) into the autoclave, inflate to 4MPa, and carry out air-pressure-assisted impregnation for 4h.
(5)干燥:将三维碳纤维预制件从溶胶中取出,在惰性气氛中500℃下干燥2h。(5) Drying: The three-dimensional carbon fiber preform was taken out from the sol and dried at 500 °C for 2 h in an inert atmosphere.
(6)热处理:将干燥后的三维碳纤维预制件在高纯惰性气体保护下,以15℃/min的速率升温至1300℃,并保温1h,然后随炉降温,得到三维碳纤维增强氧化铝-氧化锆复合材料中间体。(6) Heat treatment: under the protection of high-purity inert gas, the dried three-dimensional carbon fiber preform is heated to 1300 °C at a rate of 15 °C/min, and kept for 1 h, and then cooled with the furnace to obtain three-dimensional carbon fiber reinforced alumina-oxidized Zirconium composite intermediates.
(7)重复过程:重复步骤(3)~(6),共24次,经检测,最后一次处理后,三维碳纤维增强氧化铝-氧化锆复合材料中间体相比于上一次处理后的增重率为0.77%,复合过程完毕,得到三维碳纤维增强氧化铝-氧化锆复合材料。(7) Repeat process: Repeat steps (3) to (6) for a total of 24 times. After the last treatment, the three-dimensional carbon fiber reinforced alumina-zirconia composite intermediate has a weight gain compared to the last treatment. The ratio was 0.77%, the composite process was completed, and the three-dimensional carbon fiber reinforced alumina-zirconia composite material was obtained.
图1为本实施例制备的三维碳纤维增强氧化铝-氧化锆复合材料的宏观照片,经检测,本实施例得到的三维碳纤维增强氧化铝-氧化锆复合材料的孔隙率为13.1%,弯曲强度为275.7MPa,断裂韧性为13.9MPa·m1/2。经1500℃高温惰性气氛中热处理1h后,强度保留率98.2%;经1500℃静态空气氧化0.5h后,强度保留率94.4%。Fig. 1 is a macro photo of the three-dimensional carbon fiber reinforced alumina-zirconia composite material prepared in this embodiment. After testing, the porosity of the three-dimensional carbon fiber reinforced alumina-zirconia composite material obtained in this embodiment is 13.1%, and the bending strength is 275.7MPa, and the fracture toughness was 13.9MPa·m 1/2 . After heat treatment in a high temperature inert atmosphere at 1500℃ for 1h, the strength retention rate was 98.2%; after static air oxidation at 1500℃ for 0.5h, the strength retention rate was 94.4%.
图2为本实施例制备得到的三维碳纤维增强氧化铝-氧化锆复合材料的微观结构图,可以看到,其组成包括三维碳纤维预制件和氧化铝-氧化锆复相陶瓷,其中,氧化铝-氧化锆复相陶瓷为基体,三维碳纤维预制件为增强相,氧化铝-氧化锆复相陶瓷粒子烧结后成块状,均匀填充于纤维束内部即单根纤维之间的空隙。氧化铝-氧化锆复相陶瓷基体中,Al2O3和ZrO2的摩尔比为1∶0.3。Fig. 2 is a microstructure diagram of the three-dimensional carbon fiber reinforced alumina-zirconia composite material prepared in this example. It can be seen that its composition includes a three-dimensional carbon fiber preform and an alumina-zirconia composite ceramic, wherein the alumina- The zirconia composite ceramic is the matrix, the three-dimensional carbon fiber preform is the reinforcing phase, and the alumina-zirconia composite ceramic particles are sintered into blocks, which are uniformly filled in the fiber bundles, that is, the gaps between the individual fibers. In the alumina-zirconia composite ceramic matrix, the molar ratio of Al 2 O 3 and ZrO 2 is 1:0.3.
实施例2:Example 2:
一种本发明的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,包括以下具体工艺步骤:A preparation method of a three-dimensional carbon fiber reinforced alumina-zirconia composite material of the present invention comprises the following specific process steps:
(1)溶胶选取:选取固相含量为35wt%的氧化铝-氧化锆复合溶胶作为氧化铝-氧化锆复相陶瓷基体的原料,其中氧化铝与氧化锆摩尔比为95∶5,在上述氧化铝-氧化锆复合溶胶中加入HNO3作为稳定剂,HNO3加入量为氧化铝溶胶重量的20%。(1) Sol selection: Select an alumina-zirconia composite sol with a solid phase content of 35wt% as the raw material for the alumina-zirconia composite ceramic matrix, wherein the alumina to zirconia molar ratio is 95:5. HNO3 was added to the aluminum-zirconia composite sol as a stabilizer, and the amount of HNO3 was 20% of the weight of the alumina sol.
(2)预制件预处理:选取三维四向编织结构的三维碳纤维预制件为增强相,三维碳纤维预制件中纤维的体积分数为53%。将选取的三维碳纤维预制件置于高纯氩气气氛中,以20℃/min的速率升温至1800℃并保温1h,然后随炉降温,完成预制件的预处理。(2) Pre-processing of preforms: The three-dimensional carbon fiber preform with a three-dimensional four-way braided structure is selected as the reinforcement phase, and the volume fraction of fibers in the three-dimensional carbon fiber preform is 53%. The selected three-dimensional carbon fiber preforms were placed in a high-purity argon atmosphere, heated to 1800°C at a rate of 20°C/min and kept for 1 h, and then cooled with the furnace to complete the pretreatment of the preforms.
(3)真空浸渍:将经预处理的三维碳纤维预制件置于真空罐中,抽真空至真空度达到100Pa时,吸入步骤(1)的氧化铝-氧化锆复合溶胶,使氧化铝-氧化锆复合溶胶淹没三维碳纤维预制件,浸泡4h。(3) Vacuum impregnation: place the pretreated three-dimensional carbon fiber preform in a vacuum tank, and when the vacuum degree reaches 100Pa, inhale the alumina-zirconia composite sol of step (1) to make the alumina-zirconia composite sol. The composite sol submerged the three-dimensional carbon fiber preform for 4 hours.
(4)气压辅助浸渍:将预制件(仍浸泡在溶胶中)移至压力釜中,充气至8MPa,进行气压辅助浸渍,保持6h。(4) Air pressure assisted impregnation: Move the preform (still soaked in sol) to the autoclave, inflate to 8MPa, carry out air pressure assisted impregnation, and keep it for 6h.
(5)干燥:将三维碳纤维预制件从溶胶中取出,在惰性气氛中400℃下干燥4h。(5) Drying: The three-dimensional carbon fiber preform was taken out from the sol and dried at 400 °C for 4 h in an inert atmosphere.
(6)热处理:将干燥后的三维碳纤维预制件在高纯惰性气体保护下,以15℃/min的速率升温至1500℃,并保温0.5h,然后随炉降温,得到三维碳纤维增强氧化铝-氧化锆复合材料中间体。(6) Heat treatment: under the protection of high-purity inert gas, the dried three-dimensional carbon fiber preform is heated to 1500 °C at a rate of 15 °C/min, and kept for 0.5 h, and then cooled with the furnace to obtain three-dimensional carbon fiber reinforced alumina- Zirconia composite intermediates.
(7)重复过程:重复步骤(3)~(6),共25次,经检测,最后一次处理后,三维碳纤维增强氧化铝-氧化锆复合材料中间体相比于上一次处理后的增重率为0.93%,复合过程完毕,得到三维碳纤维增强氧化铝-氧化锆复合材料。(7) Repeat process: Repeat steps (3) to (6) for a total of 25 times. After the last treatment, the three-dimensional carbon fiber reinforced alumina-zirconia composite intermediate has a weight gain compared to the last treatment. The ratio was 0.93%, the composite process was completed, and the three-dimensional carbon fiber reinforced alumina-zirconia composite material was obtained.
经检测,本实施例制备得到的三维碳纤维增强氧化铝-氧化锆复合材料的孔隙率为12.6%,弯曲强度为302.8MPa,断裂韧性为12.4MPa·m1/2。经1500℃高温惰性气氛中热处理1h后,强度保留率99.0%;经1500℃静态空气氧化0.5h后,强度保留率98.3%。其组成包括三维碳纤维预制件和氧化铝-氧化锆复相陶瓷,其中,氧化铝-氧化锆复相陶瓷为基体,氧化锆在复相陶瓷中的摩尔含量为5%,三维碳纤维预制件为增强相,氧化铝-氧化锆复相陶瓷均匀填充于三维碳纤维预制件的空隙中。After testing, the three-dimensional carbon fiber reinforced alumina-zirconia composite material prepared in this example has a porosity of 12.6%, a bending strength of 302.8 MPa, and a fracture toughness of 12.4 MPa·m 1/2 . After heat treatment in a high temperature inert atmosphere at 1500℃ for 1h, the strength retention rate was 99.0%; after static air oxidation at 1500℃ for 0.5h, the strength retention rate was 98.3%. Its composition includes a three-dimensional carbon fiber preform and an alumina-zirconia composite ceramic, wherein the alumina-zirconia composite ceramic is the matrix, the molar content of zirconia in the composite ceramic is 5%, and the three-dimensional carbon fiber preform is the reinforcement. The alumina-zirconia composite ceramics are uniformly filled in the voids of the three-dimensional carbon fiber preform.
实施例3:Example 3:
一种本发明的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,包括以下具体工艺步骤:A preparation method of a three-dimensional carbon fiber reinforced alumina-zirconia composite material of the present invention comprises the following specific process steps:
(1)溶胶选取:选取固相含量为20wt%的氧化铝-氧化锆复合溶胶作为氧化铝-氧化锆复相陶瓷基体的原料,其中氧化铝与氧化锆摩尔比为5∶95,在上述氧化铝-氧化锆复合溶胶中加入HNO3作为稳定剂,HNO3加入量为氧化铝溶胶重量的20%。(1) Sol selection: choose an alumina-zirconia composite sol with a solid phase content of 20wt% as the raw material for the alumina-zirconia composite ceramic matrix, wherein the alumina to zirconia molar ratio is 5:95. HNO3 was added to the aluminum-zirconia composite sol as a stabilizer, and the amount of HNO3 was 20% of the weight of the alumina sol.
(2)预制件预处理:选取二维半编织结构的三维碳纤维预制件为增强相,三维碳纤维预制件中纤维的体积分数为46%。将选取的三维碳纤维预制件置于真空下,以15℃/min的速率升温至1400℃并保温3h,然后随炉降温,完成预制件的预处理。(2) Pre-processing of preforms: The three-dimensional carbon fiber preform with a two-dimensional semi-woven structure is selected as the reinforcement phase, and the volume fraction of fibers in the three-dimensional carbon fiber preform is 46%. The selected three-dimensional carbon fiber preforms were placed under vacuum, heated to 1400°C at a rate of 15°C/min and kept for 3 hours, and then cooled with the furnace to complete the pretreatment of the preforms.
(3)真空浸渍:将经预处理的三维碳纤维预制件置于真空罐中,抽真空至真空度达到200Pa时,吸入步骤(1)的氧化铝-氧化锆复合溶胶,使氧化铝-氧化锆复合溶胶淹没三维碳纤维预制件,浸泡8h。(3) Vacuum impregnation: place the pretreated three-dimensional carbon fiber preform in a vacuum tank, and when the vacuum degree reaches 200Pa, inhale the alumina-zirconia composite sol of step (1) to make the alumina-zirconia composite sol. The composite sol submerged the three-dimensional carbon fiber preform for 8 hours.
(4)气压辅助浸渍:将预制件(仍浸泡在溶胶中)移至压力釜中,充气至10MPa,进行气压辅助浸渍,保持2h。(4) Air pressure-assisted impregnation: Move the preform (still immersed in the sol) to the autoclave, inflate to 10MPa, and carry out air-pressure-assisted impregnation for 2h.
(5)干燥:将三维碳纤维预制件从溶胶中取出,在惰性气氛中700℃下干燥1h。(5) Drying: The three-dimensional carbon fiber preform was taken out from the sol, and dried at 700 °C for 1 h in an inert atmosphere.
(6)热处理:将干燥后的三维碳纤维预制件在高纯惰性气体保护下,以10℃/min的速率升温至1200℃,并保温1.5h,然后随炉降温,得到三维碳纤维增强氧化铝-氧化锆复合材料中间体。(6) Heat treatment: under the protection of high-purity inert gas, the dried three-dimensional carbon fiber preform is heated to 1200 °C at a rate of 10 °C/min, and kept for 1.5 hours, and then cooled with the furnace to obtain three-dimensional carbon fiber reinforced alumina- Zirconia composite intermediates.
(7)重复过程:重复步骤(3)~(6),共21次,经检测,最后一次处理后,三维碳纤维增强氧化铝-氧化锆复合材料中间体相比于上一次处理后的增重率为0.85%,复合过程完毕,得到三维碳纤维增强氧化铝-氧化锆复合材料。(7) Repeat process: Repeat steps (3) to (6) for a total of 21 times. After testing, after the last treatment, the three-dimensional carbon fiber reinforced alumina-zirconia composite intermediate has increased in weight compared with the last treatment. The ratio was 0.85%, the composite process was completed, and a three-dimensional carbon fiber reinforced alumina-zirconia composite material was obtained.
经检测,本实施例制备得到的氧化锆的孔隙率为16.1%,弯曲强度为218.4MPa,断裂韧性为11.3MPa·m1/2。经1500℃高温惰性气氛中热处理1h后,强度保留率92.5%;经1500℃静态空气氧化0.5h后,强度保留率91.8%。其组成包括三维碳纤维预制件和氧化铝-氧化锆复相陶瓷,其中,氧化铝-氧化锆复相陶瓷为基体,氧化锆在复相陶瓷中的摩尔含量为95%,三维碳纤维预制件为增强相,氧化铝-氧化锆复相陶瓷均匀填充于三维碳纤维预制件的空隙中After testing, the porosity of the zirconia prepared in this example is 16.1%, the bending strength is 218.4 MPa, and the fracture toughness is 11.3 MPa·m 1/2 . After heat treatment at 1500℃ for 1h in a high temperature inert atmosphere, the strength retention rate was 92.5%; after static air oxidation at 1500℃ for 0.5h, the strength retention rate was 91.8%. Its composition includes three-dimensional carbon fiber preforms and alumina-zirconia composite ceramics, wherein the alumina-zirconia composite ceramics are the matrix, the molar content of zirconia in the composite ceramics is 95%, and the three-dimensional carbon fiber preforms are reinforced. Phase, alumina-zirconia composite ceramics are uniformly filled in the voids of 3D carbon fiber preforms
实施例4:Example 4:
一种本发明的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,包括以下具体工艺步骤:A preparation method of a three-dimensional carbon fiber reinforced alumina-zirconia composite material of the present invention comprises the following specific process steps:
(1)溶胶选取:选取固相含量为40wt%的氧化铝-氧化锆复合溶胶作为氧化铝-氧化锆复相陶瓷基体的原料,其中氧化铝与-氧化锆摩尔比为1∶3,在上述氧化铝-氧化锆复合溶胶中加入HNO3作为稳定剂,HNO3加入量为氧化铝溶胶重量的30%。(1) Sol selection: Select the alumina-zirconia composite sol with a solid phase content of 40wt% as the raw material of the alumina-zirconia composite ceramic matrix, wherein the alumina to-zirconia molar ratio is 1:3. HNO 3 was added to the alumina-zirconia composite sol as a stabilizer, and the amount of HNO 3 was 30% of the weight of the alumina sol.
(2)预制件预处理:选取碳纤维布与网胎交替叠层针刺得到的三维碳纤维预制件为增强相,三维碳纤维预制件中纤维的体积分数为28%。将选取的三维碳纤维预制件置于真空下,以10℃/min的速率升温至1400℃并保温4h,然后随炉降温,完成预制件的预处理。(2) Pre-treatment of preforms: The three-dimensional carbon fiber preforms obtained by alternately laminating and needle punching carbon fiber cloth and mesh tires are selected as the reinforcing phase, and the volume fraction of fibers in the three-dimensional carbon fiber preforms is 28%. The selected three-dimensional carbon fiber preforms were placed under vacuum, heated to 1400°C at a rate of 10°C/min and kept for 4 h, and then cooled with the furnace to complete the pretreatment of the preforms.
(3)真空浸渍:将经预处理的三维碳纤维预制件置于真空罐中,抽真空至真空度达到500Pa时,吸入步骤(1)的氧化铝-氧化锆复合溶胶,使氧化铝-氧化锆复合溶胶淹没三维碳纤维预制件,浸泡8h。(3) Vacuum impregnation: place the pretreated three-dimensional carbon fiber preform in a vacuum tank, and when the vacuum degree reaches 500Pa, inhale the alumina-zirconia composite sol of step (1) to make the alumina-zirconia composite sol. The composite sol submerged the three-dimensional carbon fiber preform for 8 hours.
(4)气压辅助浸渍:将预制件(仍浸泡在溶胶中)移至压力釜中,充气至2MPa,进行气压辅助浸渍,保持6h。(4) Air pressure-assisted impregnation: move the preform (still immersed in the sol) into the autoclave, inflate to 2MPa, carry out air-pressure-assisted impregnation, and keep it for 6h.
(5)干燥:将三维碳纤维预制件从溶胶中取出,在惰性气氛中400℃下干燥6h。(5) Drying: The three-dimensional carbon fiber preform was taken out from the sol and dried at 400 °C for 6 h in an inert atmosphere.
(6)热处理:将干燥后的三维碳纤维预制件在高纯惰性气体保护下,以10℃/min的速率升温至1100℃,并保温2h,然后随炉降温,得到三维碳纤维增强氧化铝-氧化锆复合材料中间体。(6) Heat treatment: under the protection of high-purity inert gas, the dried three-dimensional carbon fiber preform is heated to 1100 °C at a rate of 10 °C/min, and kept for 2 hours, and then cooled with the furnace to obtain three-dimensional carbon fiber reinforced alumina-oxidized Zirconium composite intermediates.
(7)重复过程:重复步骤(3)~(6),共27次,经检测,最后一次处理后,三维碳纤维增强氧化铝-氧化锆复合材料中间体相比于上一次处理后的增重率为0.93%,复合过程完毕,得到三维碳纤维增强氧化铝-氧化锆复合材料。(7) Repeat process: Repeat steps (3) to (6) for a total of 27 times. After the last treatment, the three-dimensional carbon fiber reinforced alumina-zirconia composite intermediate has a weight gain compared to the last treatment. The ratio was 0.93%, the composite process was completed, and the three-dimensional carbon fiber reinforced alumina-zirconia composite material was obtained.
经检测,本实施例得到的三维碳纤维增强氧化铝-氧化锆复合材料的孔隙率为14.6%,弯曲强度为154.3MPa,断裂韧性为7.7MPa·m1/2。经1500℃高温惰性气氛中热处理1h后,强度保留率93.6%;经1500℃静态空气氧化0.5h后,强度保留率91.0%。其组成包括三维碳纤维预制件和氧化铝-氧化锆复相陶瓷,其中,氧化铝-氧化锆复相陶瓷为基体,氧化铝陶瓷与氧化锆陶瓷的摩尔比为1∶3,三维碳纤维预制件为增强相,氧化铝-氧化锆复相陶瓷均匀填充于三维碳纤维预制件的空隙中。After testing, the three-dimensional carbon fiber reinforced alumina-zirconia composite material obtained in this example has a porosity of 14.6%, a bending strength of 154.3 MPa, and a fracture toughness of 7.7 MPa·m 1/2 . After heat treatment at 1500℃ for 1 hour in a high temperature inert atmosphere, the strength retention rate is 93.6%; after static air oxidation at 1500℃ for 0.5h, the strength retention rate is 91.0%. Its composition includes a three-dimensional carbon fiber preform and an alumina-zirconia composite ceramic, wherein the alumina-zirconia composite ceramic is a matrix, the molar ratio of the alumina ceramic and the zirconia ceramic is 1:3, and the three-dimensional carbon fiber preform is The reinforcing phase, alumina-zirconia composite ceramics, is uniformly filled in the voids of the three-dimensional carbon fiber preform.
实施例5:Example 5:
一种本发明的三维碳纤维增强氧化铝-氧化锆复合材料的制备方法,包括以下具体工艺步骤:A preparation method of a three-dimensional carbon fiber reinforced alumina-zirconia composite material of the present invention comprises the following specific process steps:
(1)溶胶选取:选取固相含量为30wt%的氧化铝-氧化锆复合溶胶作为氧化铝-氧化锆复相陶瓷基体的原料,其中氧化铝与氧化锆的摩尔比为1∶1,在上述氧化铝-氧化锆复合溶胶中加入HNO3作为稳定剂,HNO3加入量为氧化铝溶胶重量的25%。(1) Sol selection: select an alumina-zirconia composite sol with a solid phase content of 30 wt% as the raw material of the alumina-zirconia composite ceramic matrix, wherein the molar ratio of alumina and zirconia is 1:1. HNO 3 was added to the alumina-zirconia composite sol as a stabilizer, and the amount of HNO 3 was 25% of the weight of the alumina sol.
(2)预制件预处理:选取三维五向编织结构的三维碳纤维预制件为增强相,三维碳纤维预制件中纤维的体积分数为50%。将选取的三维碳纤维预制件置于高纯氩气气氛中,以15℃/min的速率升温至1600℃并保温2h,然后随炉降温,完成预制件的预处理。(2) Pre-processing of preforms: The three-dimensional carbon fiber preform with a three-dimensional five-way braided structure is selected as the reinforcement phase, and the volume fraction of fibers in the three-dimensional carbon fiber preform is 50%. The selected three-dimensional carbon fiber preforms were placed in a high-purity argon atmosphere, heated to 1600°C at a rate of 15°C/min and kept for 2 hours, and then cooled with the furnace to complete the pretreatment of the preforms.
(3)真空浸渍:将经预处理的三维碳纤维预制件置于真空罐中,抽真空至真空度达到400Pa时,吸入步骤(1)的氧化铝-氧化锆复合溶胶,使氧化铝-氧化锆复合溶胶淹没三维碳纤维预制件,浸泡6h。(3) Vacuum impregnation: place the pretreated three-dimensional carbon fiber preform in a vacuum tank, and when the vacuum degree reaches 400Pa, inhale the alumina-zirconia composite sol of step (1) to make the alumina-zirconia composite sol. The composite sol submerged the three-dimensional carbon fiber preform for 6 hours.
(4)气压辅助浸渍:将预制件(仍浸泡在溶胶中)移至压力釜中,充气至6MPa,进行气压辅助浸渍,保持4h。(4) Air pressure-assisted impregnation: Move the preform (still immersed in the sol) into the autoclave, inflate to 6MPa, and carry out air-pressure-assisted impregnation for 4h.
(5)干燥:将三维碳纤维预制件从溶胶中取出,在惰性气氛中600℃下干燥3h。(5) Drying: The three-dimensional carbon fiber preform was taken out from the sol and dried at 600 °C for 3 h in an inert atmosphere.
(6)热处理:将干燥后的三维碳纤维预制件在高纯惰性气体保护下,以20℃/min的速率升温至1400℃,并保温1h,然后随炉降温,得到三维碳纤维增强氧化铝-氧化锆复合材料中间体。(6) Heat treatment: under the protection of high-purity inert gas, the dried three-dimensional carbon fiber preform is heated to 1400 °C at a rate of 20 °C/min, and kept for 1 h, and then cooled with the furnace to obtain three-dimensional carbon fiber reinforced alumina-oxidized Zirconium composite intermediates.
(7)重复过程:重复步骤(3)~(6),共25次,经检测,最后一次处理后,三维碳纤维增强氧化铝-氧化锆复合材料中间体相比于上一次处理后的增重率为0.79%,复合过程完毕,得到三维碳纤维增强氧化铝-氧化锆复合材料。(7) Repeat process: Repeat steps (3) to (6) for a total of 25 times. After the last treatment, the three-dimensional carbon fiber reinforced alumina-zirconia composite intermediate has a weight gain compared to the last treatment. The ratio was 0.79%, the composite process was completed, and the three-dimensional carbon fiber reinforced alumina-zirconia composite material was obtained.
经检测,本实施例制备得到的三维碳纤维增强氧化铝-氧化锆复合材料的孔隙率为10.7%,弯曲强度为334.6MPa,断裂韧性为14.5MPa·m1/2。经1500℃高温惰性气氛中热处理1h后,强度保留率98.6%;经1500℃静态空气氧化0.5h后,强度保留率98.8%。其组成包括三维碳纤维预制件和氧化铝-氧化锆复相陶瓷,其中,氧化铝-氧化锆复相陶瓷为基体,氧化铝陶瓷与氧化锆陶瓷的摩尔比为1∶1,三维碳纤维预制件为增强相,氧化铝-氧化锆复相陶瓷均匀填充于三维碳纤维预制件的空隙中。After testing, the porosity of the three-dimensional carbon fiber reinforced alumina-zirconia composite material prepared in this example is 10.7%, the bending strength is 334.6MPa, and the fracture toughness is 14.5MPa·m 1/2 . After heat treatment in a high temperature inert atmosphere at 1500℃ for 1h, the strength retention rate is 98.6%; after static air oxidation at 1500℃ for 0.5h, the strength retention rate is 98.8%. Its composition includes a three-dimensional carbon fiber preform and an alumina-zirconia composite ceramic, wherein the alumina-zirconia composite ceramic is a matrix, the molar ratio of the alumina ceramic and the zirconia ceramic is 1:1, and the three-dimensional carbon fiber preform is The reinforcing phase, alumina-zirconia composite ceramics, is uniformly filled in the voids of the three-dimensional carbon fiber preform.
由实施例1至5可知,本发明的制备方法制备得到的三维碳纤维增强氧化铝-氧化锆复合材料具有低孔隙率、高力学性能和优异的抗高温氧化性能。It can be seen from Examples 1 to 5 that the three-dimensional carbon fiber reinforced alumina-zirconia composite material prepared by the preparation method of the present invention has low porosity, high mechanical properties and excellent high temperature oxidation resistance.
综上所述,本发明立足氧化铝-氧化锆复相陶瓷的特点、研究现状与存在的问题,结合碳纤维、氧化铝-氧化锆复相陶瓷、三维预制件三者的优势,提供三维碳纤维预制件增强氧化铝-氧化锆复相陶瓷复合材料这一新型材料体系,并形成了能够获得优良性能的制备方法。To sum up, the present invention is based on the characteristics, research status and existing problems of alumina-zirconia composite ceramics, and combines the advantages of carbon fibers, alumina-zirconia composite ceramics and three-dimensional preforms to provide three-dimensional carbon fiber prefabricated products. A new material system of reinforced alumina-zirconia composite ceramic composites has been developed, and a preparation method capable of obtaining excellent properties has been formed.
在制备方法上,首先通过添加HNO3为添加剂,获得了稳定的氧化铝-氧化锆复合溶胶,为复合材料制备提供了可靠的原料保障,然后采用固相含量为20wt%~40wt% 的氧化铝-氧化锆复合溶胶(胶体粒径≤30nm)为基体原料,在有限周期内(25个周期)就能制备出孔隙率只有11%左右、弯曲强度可达334.6MPa、断裂韧性可达14.5MPa·m1/2的三维五向碳纤维增强氧化铝-氧化锆复相陶瓷复合材料。虽然没有完全对应的其它方法制备的三维五向碳纤维增强氧化铝-氧化锆复相陶瓷复合材料可以对比,但可与相类似的现有技术进行对比:一是现有技术中采用AlCl3·6H2O或Al(NO3)3·9H2O无机盐配制成的溶胶为基体原料,通过13个周期的“浸渍-干燥-1260℃热处理”制备三维四向碳纤维增强氧化铝复合材料,发现后续继续复合时密度不再增长,孔隙率30%左右,弯曲强度仅为100MPa~150MPa;二是以含Si有机盐与含Y有机盐溶液制备Y2SiO5涂层,需要脱除掉大量溶剂与添加剂,制备效率很低,一个典型参数是做了20次浸渍提拉热处理,厚度才2μm。因此,通过对比可以发现,采用高固相含量氧化铝-氧化锆复合溶胶作为氧化铝-氧化锆复相陶瓷基体原料,相比于从有机或无机盐的溶液出发的技术路线,在制备效率上的优势不言而喻。In the preparation method, firstly, by adding HNO 3 as an additive, a stable alumina-zirconia composite sol was obtained, which provided a reliable raw material guarantee for the preparation of composite materials, and then alumina with a solid content of 20wt% to 40wt% was used -Zirconium oxide composite sol (colloidal particle size ≤30nm) is used as the matrix raw material, the porosity is only about 11%, the bending strength can reach 334.6MPa, and the fracture toughness can reach 14.5MPa in a limited period (25 periods). m 1/2 three-dimensional pentagonal carbon fiber reinforced alumina-zirconia composite ceramic composites. Although there is no completely corresponding three-dimensional five-direction carbon fiber reinforced alumina-zirconia composite ceramic composite prepared by other methods, it can be compared with similar existing technologies: First, AlCl 3 ·6H is used in the prior art. The sol prepared from 2 O or Al(NO 3 ) 3 ·9H 2 O inorganic salt was used as the matrix raw material, and three-dimensional four-dimensional carbon fiber reinforced alumina composites were prepared by 13 cycles of "dipping-drying-1260 ℃ heat treatment". When the compound is continued, the density will not increase, the porosity is about 30%, and the bending strength is only 100MPa ~ 150MPa; the second is to prepare the Y 2 SiO 5 coating with Si-containing organic salt and Y-containing organic salt solution, and it is necessary to remove a large amount of solvent and Additives, the preparation efficiency is very low, a typical parameter is 20 times of dipping and pulling heat treatment, and the thickness is only 2μm. Therefore, by comparison, it can be found that the use of high solid content alumina-zirconia composite sol as the raw material of alumina-zirconia composite ceramic matrix, compared with the technical route starting from the solution of organic or inorganic salts, in terms of preparation efficiency The advantages are self-evident.
另外,采用扫描电子显微镜观测了本发明的三维碳纤维增强氧化铝-氧化锆复合材料的微观结构,如图2所示,可以看到,氧化铝-氧化锆复相陶瓷粒子烧结后成块状,均匀填充于纤维束内部即单根纤维之间的空隙,避免了泥浆原料容易出现的分布不均匀的问题。因此,本发明采用的氧化铝-氧化锆复合溶胶,既保持了无机盐或有机盐溶液原料能够均匀填充的优点,以及泥浆原料高效率浸渍的优点,又克服了无机盐或有机盐溶液原料致密化效率偏低的缺点,以及泥浆原料填充不均匀的缺点。In addition, the microstructure of the three-dimensional carbon fiber reinforced alumina-zirconia composite material of the present invention was observed by scanning electron microscope, as shown in FIG. It is evenly filled in the interior of the fiber bundle, that is, the space between the single fibers, avoiding the problem of uneven distribution of mud raw materials that is easy to occur. Therefore, the alumina-zirconia composite sol used in the present invention not only maintains the advantages of uniform filling of inorganic salt or organic salt solution raw materials, and the advantages of high-efficiency impregnation of mud raw materials, but also overcomes the density of inorganic salt or organic salt solution raw materials. The disadvantages of low chemical efficiency and uneven filling of mud raw materials.
接下来,本发明采用先真空浸渍然后气压辅助浸渍方式,先抽真空排除掉预制中空隙中的空气,为溶胶的渗入提供空间,由于溶胶中是纳米尺寸的单颗粒均匀分散的氧化铝-氧化锆复合胶体粒子,具有很好的稳定性,因而能够迅速、均匀地进入预制件的空隙中;然后通过外部气压作用,促进溶胶进一步向预制件内部渗入,进入一些孔道复杂的空隙中,甚至能够破坏一些闭孔使其变成开孔,从而提高浸渍效率和填充程度。Next, the present invention adopts the method of first vacuum impregnation and then air pressure-assisted impregnation, first vacuuming to remove the air in the prefabricated voids, and providing space for the infiltration of the sol. The zirconium composite colloidal particles have good stability, so they can quickly and evenly enter the voids of the preform; then, through the action of external air pressure, the sol is further infiltrated into the preform, entering into some complex pores, and even can Break some closed cells into open cells, thereby improving impregnation efficiency and filling degree.
最后,本发明所用溶胶中,氧化铝-氧化锆为无定形态,又为纳米尺度,其表面能很高,因而具有高的烧结活性。在此基础上,通过对氧化铝-氧化锆烧结收缩行为的研究,本发明把热处理温度设定为1100℃~1500℃,在这个温度范围内,既能确保氧化铝-氧化锆转化成氧化铝-氧化锆复相陶瓷,又能获得较高的基体致密度(提高基体承受载荷和传递载荷的能力),同时也不会导致基体与碳纤维间的反应(避免形成化学强结合界面以及损伤碳纤维的力学性能),最终获得综合性能优良的三维碳纤维增强氧化铝-氧化锆复合材料。Finally, in the sol used in the present invention, the alumina-zirconia is in an amorphous state and has a nanometer scale, and its surface energy is very high, so it has a high sintering activity. On this basis, through the research on the sintering shrinkage behavior of alumina-zirconia, the present invention sets the heat treatment temperature to 1100℃~1500℃, within this temperature range, it can not only ensure the conversion of alumina-zirconia into alumina -Zirconium oxide multiphase ceramics, which can achieve higher matrix density (improve the ability of the matrix to withstand and transmit loads), and will not cause the reaction between the matrix and carbon fibers (avoid the formation of chemically strong bonding interfaces and damage to carbon fibers. mechanical properties), and finally obtain a three-dimensional carbon fiber reinforced alumina-zirconia composite material with excellent comprehensive properties.
对氧化铝-氧化锆溶胶经干燥后得到的凝胶粉末进行XRD检测:XRD detection of the gel powder obtained by drying the alumina-zirconia sol:
采用D8 Advance型X射线衍射仪分析凝胶粉末(氧化铝与氧化锆的摩尔比为1∶0.3)的相组成。测试条件为:CuKα射线,管电流40mA,管电压40KV,2θ=10~60°,扫描速度4°/min。The phase composition of the gel powder (molar ratio of alumina to zirconia was 1:0.3) was analyzed by a D8 Advance X-ray diffractometer. The test conditions are: CuKα ray, tube current 40mA, tube voltage 40KV, 2θ=10~60°, scanning speed 4°/min.
检测结果参见图3,由图可知:图谱呈现“馒头”峰特征,没有出现尖锐的氧化铝或氧化锆特征衍射峰,表明经700℃干燥后的氧化铝-氧化锆凝胶粉末为典型的无定形状态,无定形的状态具有高表面能,可以促进烧结致密化。The detection results are shown in Figure 3. It can be seen from the figure that the spectrum shows the characteristics of "steamed bread" peaks, and no sharp diffraction peaks of alumina or zirconia appear, indicating that the alumina-zirconia gel powder dried at 700 °C is a typical non- Shaped state, amorphous state has high surface energy, which can promote sintering densification.
对氧化铝-氧化锆溶胶经干燥后得到的凝胶粉末,经压制成块后,对其在不同温度下热处理后的线收缩情况进行检测:After the gel powder obtained by drying the alumina-zirconia sol was pressed into a block, the linear shrinkage after heat treatment at different temperatures was tested:
将干燥后的氧化铝-氧化锆凝胶粉末(氧化铝与氧化锆的摩尔比为1∶0.3)放入直径40mm的金属模具中,在压机上于100MPa下将粉末压制成直径40mm、厚度5mm的圆块。将圆块放入热处理炉中,在不同温度下热处理1h后,测量热处理前后直径、厚度的变化率,测5个点取平均值为最终结果。Put the dried alumina-zirconia gel powder (the molar ratio of alumina to zirconia is 1:0.3) into a metal mold with a diameter of 40mm, and press the powder on a press at 100MPa to a diameter of 40mm and a thickness of 40mm. 5mm round block. Put the round block into the heat treatment furnace, after heat treatment at different temperatures for 1h, measure the change rate of diameter and thickness before and after heat treatment, and measure the average value of 5 points as the final result.
检测结果参见图4,由图可知:经1100℃~1500℃热处理后,线收缩率在12%~24%范围内随温度升高而逐渐增长,其中,当温度从1300℃升高到1400℃时,线收缩率变化很小,1400℃到1500℃又有明显增加,说明氧化铝-氧化锆具有较好的烧结活性。根据图4可推测,温度低于1100℃时,热处理后的线收缩率会明显降低,不利于烧结致密,本发明选择热处理温度的下限为1100℃;温度超过1500℃后,烧结线收缩率可能会进一步升高,促进致密化,但此时碳纤维与氧化锆发生碳热还原反应的可能性很大,所以本发明选择热处理温度的上限为1500℃。The test results are shown in Figure 4. It can be seen from the figure that after heat treatment at 1100°C to 1500°C, the linear shrinkage rate increases gradually with the increase of temperature in the range of 12% to 24%. At 1400°C to 1500°C, the linear shrinkage changed little, and it increased significantly, indicating that alumina-zirconia has better sintering activity. According to Fig. 4, it can be inferred that when the temperature is lower than 1100 °C, the linear shrinkage rate after heat treatment will be significantly reduced, which is not conducive to sintering and densification. will further increase to promote densification, but at this time, the carbon fiber and zirconia are likely to have a carbothermic reduction reaction, so the present invention selects the upper limit of the heat treatment temperature to be 1500°C.
对不同温度热处理后的氧化铝-氧化锆凝胶粉末进行XRD检测:XRD detection of alumina-zirconia gel powder after heat treatment at different temperatures:
将干燥后得到的氧化铝-氧化锆凝胶粉末(氧化铝与氧化锆的摩尔比为1∶0.3)置于不同温度下热处理1h,然后采用D8 Advance型X射线衍射仪分析粉末的相组成。测试条件为:CuKα射线,管电流40mA,管电压40KV,2θ=10~60°,扫描速度4°/min。The alumina-zirconia gel powder obtained after drying (molar ratio of alumina to zirconia is 1:0.3) was heat-treated at different temperatures for 1 h, and then the phase composition of the powder was analyzed by D8 Advance X-ray diffractometer. The test conditions are: CuKα ray, tube current 40mA, tube voltage 40KV, 2θ=10~60°, scanning speed 4°/min.
检测结果参见图5,由图可知:1100℃时就生成了氧化铝-氧化锆复合陶瓷相,1200℃时出现了氧化铝相,随着温度升高,两相的结晶程度明显增加。可以推测,低于1100℃时很可能呈现无定形态,所以本发明的热处理温度下限为1100℃;1500℃时两相的结晶程度很高了,同时考虑到超过1500℃后,碳纤维与-氧化锆发生碳热还原反应的可能性很大,所以本发明的热处理温度上限为1500℃。The test results are shown in Figure 5. It can be seen from the figure that the alumina-zirconia composite ceramic phase is formed at 1100 °C, and the alumina phase appears at 1200 °C. As the temperature increases, the crystallinity of the two phases increases significantly. It can be speculated that it is likely to present an amorphous state when it is lower than 1100 °C, so the lower limit of the heat treatment temperature of the present invention is 1100 °C; at 1500 °C, the crystallinity of the two phases is very high, and considering that after exceeding 1500 °C, carbon fiber and -oxidation Zirconium is highly likely to undergo a carbothermic reduction reaction, so the upper limit of the heat treatment temperature in the present invention is 1500°C.
以上所述仅是本发明的优选实施方式,本发明的保护范围并不仅局限于上述实施例。凡属于本发明思路下的技术方案均属于本发明的保护范围。应该指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下的改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above are only preferred embodiments of the present invention, and the protection scope of the present invention is not limited to the above embodiments. All the technical solutions under the idea of the present invention belong to the protection scope of the present invention. It should be pointed out that for those skilled in the art, improvements and modifications without departing from the principles of the present invention should also be regarded as the protection scope of the present invention.
Claims (9)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810008948.XA CN108178648B (en) | 2018-01-04 | 2018-01-04 | Three-dimensional carbon fiber reinforced alumina-zirconia composite material and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810008948.XA CN108178648B (en) | 2018-01-04 | 2018-01-04 | Three-dimensional carbon fiber reinforced alumina-zirconia composite material and preparation method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN108178648A CN108178648A (en) | 2018-06-19 |
CN108178648B true CN108178648B (en) | 2020-06-19 |
Family
ID=62549870
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810008948.XA Active CN108178648B (en) | 2018-01-04 | 2018-01-04 | Three-dimensional carbon fiber reinforced alumina-zirconia composite material and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108178648B (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109053188A (en) * | 2018-09-28 | 2018-12-21 | 中国人民解放军国防科技大学 | A kind of preparation method of ZrO2 base high temperature resistant composite material |
CN109610178B (en) * | 2018-11-16 | 2021-09-21 | 常州工学院 | Carbon fiber composite material, preparation method thereof and conveyor belt connecting piece made of carbon fiber composite material |
CN113135740B (en) * | 2021-03-01 | 2022-03-29 | 华南理工大学 | A kind of ceramic matrix composite material and its preparation method and application |
CN113636855A (en) * | 2021-08-30 | 2021-11-12 | 江西信达航科新材料科技有限公司 | Internal oxidation-resistant carbon-carbon composite material |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104446580A (en) * | 2014-12-16 | 2015-03-25 | 中国人民解放军国防科学技术大学 | Method for preparing continuous fiber cloth reinforced silica ceramic-based composite material |
CN105601309A (en) * | 2016-01-29 | 2016-05-25 | 中国人民解放军国防科学技术大学 | Three-dimensional fiber prefabricated member reinforced aluminum oxide composite material and preparation method thereof |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH07115958B2 (en) * | 1991-04-05 | 1995-12-13 | トヨタ自動車株式会社 | Carbon fiber reinforced carbon composite material with high friction coefficient |
-
2018
- 2018-01-04 CN CN201810008948.XA patent/CN108178648B/en active Active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104446580A (en) * | 2014-12-16 | 2015-03-25 | 中国人民解放军国防科学技术大学 | Method for preparing continuous fiber cloth reinforced silica ceramic-based composite material |
CN105601309A (en) * | 2016-01-29 | 2016-05-25 | 中国人民解放军国防科学技术大学 | Three-dimensional fiber prefabricated member reinforced aluminum oxide composite material and preparation method thereof |
Non-Patent Citations (1)
Title |
---|
氧化铝-氧化锆复合胶体的稳定性研究;傅超等;《科技广场》;20151231(第02期);2.3 PH 对胶体的稳定性的影响 * |
Also Published As
Publication number | Publication date |
---|---|
CN108178648A (en) | 2018-06-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105601309B (en) | Three-dimensional fiber prefabricated component enhancing alumina composite material and preparation method thereof | |
CN103553616B (en) | Growth in situ SiC nanowire strengthens C/SiC matrix material and preparation method thereof | |
CN110256082B (en) | Method for preparing single crystal silicon carbide nanofibers/silicon carbide ceramic matrix composites by reaction sintering | |
CN108178648B (en) | Three-dimensional carbon fiber reinforced alumina-zirconia composite material and preparation method thereof | |
CN111099911B (en) | A carbon fiber reinforced carbon-silicon carbide-zirconium carbide composite material and preparation method thereof | |
CN103910532B (en) | Coated inorganic fiber reinforced MAX phase ceramics compound substance, Preparation Method And The Use | |
CN107640976B (en) | Three-dimensional silicon carbide fiber prefabricated part reinforced yttrium silicate composite material and preparation method thereof | |
CN106866148B (en) | In-situ reinforced SiCf/SiC composites with SiC nanowires and their preparation methods | |
CN104860695B (en) | Three-dimensional fiber prefabricated component strengthens mullite composite material and preparation method thereof | |
CN104150939B (en) | A kind of electrophoretic deposition CNTs strengthens the preparation method of ceramic matric composite | |
CN109206146B (en) | Carbon fiber/nanofiber synergistic tough ceramic matrix composite and preparation method thereof | |
CN102021817B (en) | Silicon carbide fiber solid fabric for in-situ growing carbon nano tubes, composite material and preparation method thereof | |
CN106966742B (en) | Alumina fiber reinforced mullite ceramic containing interface phase and preparation method thereof | |
CN104628407A (en) | A kind of preparation method of Al2O3 fiber toughened MAX phase ceramic matrix composite material | |
CN115058885A (en) | A kind of carbon fiber cloth surface oriented SiC nanowire array and preparation method | |
CN111253159A (en) | An ordered and disordered SiC nanowire/whisker structure and its preparation method | |
CN109608218B (en) | A kind of self-healing ceramic matrix composite material and its low-temperature rapid preparation method | |
CN106966703A (en) | Alumina fibre enhancing aluminium oxide ceramics of the phase containing interface and preparation method thereof | |
CN108147796B (en) | Three-dimensional silicon carbide fiber reinforced silica-zirconia composite ceramic composite and preparation method thereof | |
CN115417683A (en) | A kind of preparation method of oxide continuous filament reinforced oxide ceramic matrix composite material | |
CN108727049A (en) | A kind of Cf/ SiC-HfC ultra-temperature ceramic-based composite materials and preparation method thereof | |
CN108033803B (en) | Three-dimensional silicon carbide fiber reinforced alumina-zirconia composite material and preparation method thereof | |
CN108083801B (en) | Three-dimensional carbon fiber preform reinforced yttria-zirconia composite ceramic composite and preparation method thereof | |
CN108147797B (en) | Three-dimensional carbon fiber reinforced silica-zirconia composite ceramic composite and preparation method thereof | |
CN107640975B (en) | Three-dimensional carbon fiber prefabricated part reinforced yttrium oxide-aluminum oxide composite ceramic composite material and preparation method thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |