CN103304227A - Alumina-based ceramic core for directional solidification and preparation method thereof - Google Patents
Alumina-based ceramic core for directional solidification and preparation method thereof Download PDFInfo
- Publication number
- CN103304227A CN103304227A CN2013102697595A CN201310269759A CN103304227A CN 103304227 A CN103304227 A CN 103304227A CN 2013102697595 A CN2013102697595 A CN 2013102697595A CN 201310269759 A CN201310269759 A CN 201310269759A CN 103304227 A CN103304227 A CN 103304227A
- Authority
- CN
- China
- Prior art keywords
- powder
- ceramic core
- alumina
- temperature
- based ceramic
- 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.)
- Granted
Links
- 239000000919 ceramic Substances 0.000 title claims description 73
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 title claims description 59
- 238000002360 preparation method Methods 0.000 title claims description 5
- 238000007711 solidification Methods 0.000 title description 12
- 230000008023 solidification Effects 0.000 title description 12
- 239000011162 core material Substances 0.000 claims description 87
- 239000000843 powder Substances 0.000 claims description 56
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 claims description 33
- 229910052863 mullite Inorganic materials 0.000 claims description 33
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 claims description 30
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 28
- 238000002156 mixing Methods 0.000 claims description 19
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims description 17
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 claims description 16
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 16
- 239000007924 injection Substances 0.000 claims description 15
- 238000002347 injection Methods 0.000 claims description 15
- 239000004408 titanium dioxide Substances 0.000 claims description 14
- 239000011812 mixed powder Substances 0.000 claims description 13
- 239000000945 filler Substances 0.000 claims description 10
- 239000000463 material Substances 0.000 claims description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 9
- 238000001746 injection moulding Methods 0.000 claims description 8
- WRIDQFICGBMAFQ-UHFFFAOYSA-N (E)-8-Octadecenoic acid Natural products CCCCCCCCCC=CCCCCCCC(O)=O WRIDQFICGBMAFQ-UHFFFAOYSA-N 0.000 claims description 5
- LQJBNNIYVWPHFW-UHFFFAOYSA-N 20:1omega9c fatty acid Natural products CCCCCCCCCCC=CCCCCCCCC(O)=O LQJBNNIYVWPHFW-UHFFFAOYSA-N 0.000 claims description 5
- QSBYPNXLFMSGKH-UHFFFAOYSA-N 9-Heptadecensaeure Natural products CCCCCCCC=CCCCCCCCC(O)=O QSBYPNXLFMSGKH-UHFFFAOYSA-N 0.000 claims description 5
- ZQPPMHVWECSIRJ-UHFFFAOYSA-N Oleic acid Natural products CCCCCCCCC=CCCCCCCCC(O)=O ZQPPMHVWECSIRJ-UHFFFAOYSA-N 0.000 claims description 5
- 239000005642 Oleic acid Substances 0.000 claims description 5
- 229910052742 iron Inorganic materials 0.000 claims description 5
- QXJSBBXBKPUZAA-UHFFFAOYSA-N isooleic acid Natural products CCCCCCCC=CCCCCCCCCC(O)=O QXJSBBXBKPUZAA-UHFFFAOYSA-N 0.000 claims description 5
- 238000007885 magnetic separation Methods 0.000 claims description 5
- ZQPPMHVWECSIRJ-KTKRTIGZSA-N oleic acid Chemical compound CCCCCCCC\C=C/CCCCCCCC(O)=O ZQPPMHVWECSIRJ-KTKRTIGZSA-N 0.000 claims description 5
- 239000012188 paraffin wax Substances 0.000 claims description 5
- 238000003756 stirring Methods 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- 229910010413 TiO 2 Inorganic materials 0.000 claims description 3
- 238000000465 moulding Methods 0.000 claims description 3
- 238000003723 Smelting Methods 0.000 claims description 2
- 238000010891 electric arc Methods 0.000 claims description 2
- 239000000203 mixture Substances 0.000 claims description 2
- 238000007493 shaping process Methods 0.000 claims description 2
- 238000009413 insulation Methods 0.000 claims 6
- 238000010792 warming Methods 0.000 claims 6
- 239000004902 Softening Agent Substances 0.000 claims 5
- 239000004411 aluminium Substances 0.000 claims 3
- 235000015895 biscuits Nutrition 0.000 claims 3
- 238000005303 weighing Methods 0.000 claims 3
- 230000004927 fusion Effects 0.000 claims 1
- 238000000227 grinding Methods 0.000 claims 1
- 238000012856 packing Methods 0.000 claims 1
- 238000005554 pickling Methods 0.000 claims 1
- 238000010298 pulverizing process Methods 0.000 claims 1
- 238000005728 strengthening Methods 0.000 description 27
- 238000010438 heat treatment Methods 0.000 description 24
- 239000004014 plasticizer Substances 0.000 description 22
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 17
- 238000000034 method Methods 0.000 description 17
- 238000010304 firing Methods 0.000 description 15
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 12
- 239000003795 chemical substances by application Substances 0.000 description 10
- 239000013078 crystal Substances 0.000 description 10
- 239000000377 silicon dioxide Substances 0.000 description 9
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 8
- BOTDANWDWHJENH-UHFFFAOYSA-N Tetraethyl orthosilicate Chemical compound CCO[Si](OCC)(OCC)OCC BOTDANWDWHJENH-UHFFFAOYSA-N 0.000 description 8
- VKYKSIONXSXAKP-UHFFFAOYSA-N hexamethylenetetramine Chemical compound C1N(C2)CN3CN1CN2C3 VKYKSIONXSXAKP-UHFFFAOYSA-N 0.000 description 8
- 238000009966 trimming Methods 0.000 description 8
- 238000006243 chemical reaction Methods 0.000 description 7
- 238000000354 decomposition reaction Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 6
- 238000002844 melting Methods 0.000 description 6
- 230000008018 melting Effects 0.000 description 6
- 239000002245 particle Substances 0.000 description 5
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 4
- 239000004698 Polyethylene Substances 0.000 description 4
- 229910004298 SiO 2 Inorganic materials 0.000 description 4
- 238000001816 cooling Methods 0.000 description 4
- 239000000498 cooling water Substances 0.000 description 4
- 239000012153 distilled water Substances 0.000 description 4
- 238000001035 drying Methods 0.000 description 4
- 235000010299 hexamethylene tetramine Nutrition 0.000 description 4
- 239000004312 hexamethylene tetramine Substances 0.000 description 4
- 230000007062 hydrolysis Effects 0.000 description 4
- 238000006460 hydrolysis reaction Methods 0.000 description 4
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 4
- 235000021110 pickles Nutrition 0.000 description 4
- -1 polyethylene Polymers 0.000 description 4
- 229920000573 polyethylene Polymers 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 239000002966 varnish Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 239000000654 additive Substances 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 229910052593 corundum Inorganic materials 0.000 description 3
- 239000010431 corundum Substances 0.000 description 3
- 238000005452 bending Methods 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 229910052681 coesite Inorganic materials 0.000 description 2
- 229910052906 cristobalite Inorganic materials 0.000 description 2
- 239000000395 magnesium oxide Substances 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 229920003986 novolac Polymers 0.000 description 2
- SIWVEOZUMHYXCS-UHFFFAOYSA-N oxo(oxoyttriooxy)yttrium Chemical compound O=[Y]O[Y]=O SIWVEOZUMHYXCS-UHFFFAOYSA-N 0.000 description 2
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N phenol group Chemical group C1(=CC=CC=C1)O ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 2
- 239000011819 refractory material Substances 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- 229910010271 silicon carbide Inorganic materials 0.000 description 2
- 235000012239 silicon dioxide Nutrition 0.000 description 2
- 229910052814 silicon oxide Inorganic materials 0.000 description 2
- 229910052682 stishovite Inorganic materials 0.000 description 2
- 229910000601 superalloy Inorganic materials 0.000 description 2
- 229910052905 tridymite Inorganic materials 0.000 description 2
- 229910006501 ZrSiO Inorganic materials 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- JNDMLEXHDPKVFC-UHFFFAOYSA-N aluminum;oxygen(2-);yttrium(3+) Chemical compound [O-2].[O-2].[O-2].[Al+3].[Y+3] JNDMLEXHDPKVFC-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000006555 catalytic reaction Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- RKTYLMNFRDHKIL-UHFFFAOYSA-N copper;5,10,15,20-tetraphenylporphyrin-22,24-diide Chemical compound [Cu+2].C1=CC(C(=C2C=CC([N-]2)=C(C=2C=CC=CC=2)C=2C=CC(N=2)=C(C=2C=CC=CC=2)C2=CC=C3[N-]2)C=2C=CC=CC=2)=NC1=C3C1=CC=CC=C1 RKTYLMNFRDHKIL-UHFFFAOYSA-N 0.000 description 1
- 238000004925 denaturation Methods 0.000 description 1
- 230000036425 denaturation Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 229910019901 yttrium aluminum garnet Inorganic materials 0.000 description 1
Images
Landscapes
- Compositions Of Oxide Ceramics (AREA)
Abstract
本发明涉及一种定向凝固用氧化铝基陶瓷型芯及制备方法,该氧化铝基陶瓷型芯使用的耐火材料有EC95电熔莫来石、硅酸锆、二氧化硅粉、二氧化钛粉、铝粉。粉料中按重量百分比含EC95电熔莫来石65~95%,硅酸锆5~30%,二氧化硅粉2~8%,二氧化钛粉1~5%,铝粉1~10%。其中EC95电熔莫来石中粒度为F200号粉料占10~30%,F320号粉料含量40~70%,F600号粉料占10~30%。制备方法为把上述粉料球磨混合均匀,放入熔化的增塑剂中混炼,在陶瓷型芯成型机上热压注成型。热压注成型的陶瓷芯经修整、校型后放入箱式电阻炉中焙烧。出炉后的陶瓷型芯采用高温强化剂和室温强化剂进行高温强化和室温强化。本发明制备的氧化铝基陶瓷型芯具有高温强度高、抗蠕变性能好、烧成收缩小、烧成温度低、冶金化学性能好的特征。
The invention relates to an alumina-based ceramic core for directional solidification and a preparation method thereof. The refractory materials used in the alumina-based ceramic core include EC95 fused mullite, zirconium silicate, silica powder, titanium dioxide powder, aluminum pink. The powder contains 65-95% EC95 fused mullite, 5-30% zirconium silicate, 2-8% silicon dioxide powder, 1-5% titanium dioxide powder and 1-10% aluminum powder in percentage by weight. Among them, in EC95 fused mullite, F200 powder accounts for 10-30%, F320 powder accounts for 40-70%, and F600 powder accounts for 10-30%. The preparation method is as follows: ball milling and mixing the above-mentioned powder materials evenly, putting them into molten plasticizer for mixing, and hot-pressing injection molding on a ceramic core molding machine. The hot-press injection molded ceramic core is put into a box-type resistance furnace for firing after trimming and calibration. After being released from the furnace, the ceramic core is strengthened at high temperature and at room temperature with high temperature strengthening agent and room temperature strengthening agent. The alumina-based ceramic core prepared by the invention has the characteristics of high high-temperature strength, good creep resistance, small firing shrinkage, low firing temperature and good metallurgical and chemical properties.
Description
技术领域 technical field
本发明涉及一种燃气轮机部件,具体是一种定向凝固用氧化铝基陶瓷型芯及制备方法。这种氧化铝基陶瓷型芯高温强度高、抗蠕变性能好、烧成收缩小、烧成温度低、不与高温合金熔体发生化学反应。不仅可以用于铸造小尺寸的航空发动机等轴晶、定向和单晶叶片,而且可用于铸造大尺寸的重型燃气轮机等轴晶、定向和单晶叶片。 The invention relates to a gas turbine component, in particular to an alumina-based ceramic core for directional solidification and a preparation method thereof. The alumina-based ceramic core has high high-temperature strength, good creep resistance, small firing shrinkage, low firing temperature, and no chemical reaction with high-temperature alloy melt. Not only can it be used to cast small-sized equiaxed, oriented and single-crystal blades for aero-engines, but it can also be used to cast large-sized equiaxed, oriented and single-crystal blades for heavy-duty gas turbines.
背景技术 Background technique
高压涡轮叶片是燃气轮机的重要部件,为不断提高涡轮前燃气进口温度,世界各国从实心叶片制造发展到空心叶片制造,从多晶叶片到现在的定向和单晶叶片,其目的就在于不断改善燃气轮机的综合性能。目前先进的航空发动机涡轮前进口温度已达到1757℃,重型燃气轮机涡轮前进口温度也达到1600℃,涡轮前进口温度达1700℃的重型燃气轮机也正在设计和制造中。这就需要改善叶片内腔冷却结构,提高冷却效率。叶片内腔冷却结构越复杂,对用于形成其内腔的陶瓷型芯性能要求也越高。氧化硅基陶瓷型芯高温条件下易发生软化变性,偏芯、漏芯,高于1550℃时,氧化硅易于和高温合金中的活性元素Al、Hf、C等发生化学反应,致使叶片内部气冷通道发生化学粘砂,恶化叶片的内腔质量,降低叶片的气冷效果。而氧化铝由于自身所具有的高耐火度、高化学稳定性、高热稳定性等特点,用其制造的氧化铝陶瓷型芯化学性能稳定、抗蠕变性能好。 High-pressure turbine blades are important components of gas turbines. In order to continuously increase the gas inlet temperature before the turbine, countries around the world have developed from solid blades to hollow blades, from polycrystalline blades to the current directional and single crystal blades. The purpose is to continuously improve gas turbines. comprehensive performance. At present, the temperature of the front inlet of the advanced aero-engine turbine has reached 1757°C, and the temperature of the front inlet of the heavy-duty gas turbine turbine has also reached 1600°C, and the heavy-duty gas turbine with a temperature of 1700°C before the turbine inlet is also being designed and manufactured. Therefore, it is necessary to improve the cooling structure of the inner cavity of the blade and improve the cooling efficiency. The more complex the cooling structure of the inner cavity of the blade, the higher the performance requirements for the ceramic core used to form the inner cavity. Silicon oxide-based ceramic cores are prone to softening and denaturation under high temperature conditions, core eccentricity, and core leakage. When the temperature is higher than 1550 ° C, silicon oxide is prone to chemical reactions with active elements Al, Hf, and C in superalloys, resulting in gas inside the blade. Chemical sticky sand occurs in the cold channel, which deteriorates the quality of the inner cavity of the blade and reduces the air cooling effect of the blade. Due to the high refractoriness, high chemical stability and high thermal stability of alumina itself, the alumina ceramic core made of it has stable chemical properties and good creep resistance.
公知的制备氧化铝基陶瓷型芯采用的基体材料为电熔刚玉粉,其它的矿化剂和添加剂有活性氧化铝、多孔氧化铝、氧化铝空心球、碳化硅、氧化镁、氧化钇、氧化镧、石墨粉等。中国专利(专利号:CN1994964A)披露了一种采用氧化铝空心球的复合氧化铝陶瓷型芯材料及成型制备工艺,原料中各组分重量百分比为电熔刚玉粉32.5~60.5%,氧化铝空心球20~50%,碳化硅3~5%,其余为增塑剂,压注成型。美国专利(专利号:5143777)披露了一种采用200目的电熔刚玉粉和0-0.25mm的氧化铝空心球,比例为30:70,加入粘结剂,重力灌浆成型氧化铝陶瓷型芯的方法。这两种方法虽然提高了氧化铝基陶瓷型芯的孔隙率,但是由于氧化铝空心球的密度较小,而电熔刚玉的密度较大,原料混合不均匀,陶瓷型芯性能不稳定。中国专利(专利号:CN101229975A)披露了一种采用重量百分比为45~66%电熔刚玉粉,15~30%的活性氧化铝,1~5% 石墨粉,热压注成型氧化铝基陶瓷型芯的方法,由于多孔活性氧化铝焙烧时逐渐转变为γ-Al2O3和α-Al2O3的过程中伴随着较大的体积收缩,致使此陶瓷芯收缩率较大。美国专利(专利号:4837187,5409871, 5580837)分别披露了在氧化铝中添加1~20%左右的氧化钇、1~5%的MgO,1~7%左右的石墨粉,或在氧化铝中添加10~40%的钇铝石榴石,压注成型氧化铝基陶瓷型芯的方法提高陶瓷型芯性能的高温性能,但是型芯的烧结温度高达1600~1700℃。 The known matrix material used to prepare alumina-based ceramic cores is fused corundum powder, and other mineralizers and additives include activated alumina, porous alumina, alumina hollow spheres, silicon carbide, magnesia, yttrium oxide, oxide Lanthanum, graphite powder, etc. Chinese patent (patent number: CN1994964A) discloses a composite alumina ceramic core material and molding preparation process using alumina hollow balls. 20-50% balls, 3-5% silicon carbide, and the rest are plasticizers, injection molding. U.S. Patent (Patent No.: 5143777) discloses a fused alumina powder of 200 meshes and 0-0.25mm alumina hollow balls at a ratio of 30:70, adding a binder, and forming an alumina ceramic core by gravity grouting. method. Although these two methods increase the porosity of the alumina-based ceramic core, due to the low density of the alumina hollow sphere and the high density of the fused corundum, the raw materials are not mixed uniformly, and the performance of the ceramic core is unstable. Chinese patent (patent number: CN101229975A) discloses a hot press injection molding alumina-based ceramic type with 45-66% by weight of fused corundum powder, 15-30% of activated alumina, and 1-5% of graphite powder. The core method, because the porous active alumina is gradually transformed into γ-Al 2 O 3 and α-Al 2 O 3 during firing is accompanied by a large volume shrinkage, resulting in a large shrinkage rate of the ceramic core. U.S. patents (patent numbers: 4837187, 5409871, 5580837) respectively disclose adding 1-20% of yttrium oxide, 1-5% of MgO, 1-7% of graphite powder to alumina, or adding Adding 10-40% of yttrium-aluminum garnet and injection-molding the alumina-based ceramic core improves the high-temperature performance of the ceramic core, but the sintering temperature of the core is as high as 1600-1700°C.
发明内容 Contents of the invention
本发明的目的,是针对上述氧化铝基陶瓷型芯存在性能不稳定、烧成收缩大、烧成温度高的问题,提供一种定向凝固用氧化铝基陶瓷型芯。通过添加合适的添加剂,使氧化铝基陶瓷型芯1550℃的抗弯强度≥5MPa,自重变形量≤1mm,烧成收缩≤1%,烧成温度低于1450℃。可保证高温合金涡轮叶片的尺寸精度和优良的内腔表面质量。 The object of the present invention is to provide an alumina-based ceramic core for directional solidification to solve the problems of unstable performance, large firing shrinkage and high firing temperature of the above-mentioned alumina-based ceramic core. By adding appropriate additives, the bending strength of the alumina-based ceramic core at 1550 ° C is ≥ 5 MPa, the self-weight deformation is ≤ 1 mm, the firing shrinkage is ≤ 1%, and the firing temperature is lower than 1450 ° C. It can ensure the dimensional accuracy and excellent surface quality of the inner cavity of the superalloy turbine blade.
本发明的另一个目的,是提供一种定向凝固用氧气铝基陶瓷型芯的制备方法。 Another object of the present invention is to provide a method for preparing an alumina-based ceramic core for directional solidification.
采用的技术方案是: The technical solutions adopted are:
一种定向凝固用氧化铝基陶瓷型芯,其特征是以EC95电熔莫来石为基料,EC95电熔莫来石是以优质铝氧粉加重量百分比为2~6%的矿化剂于电弧炉中经≥2000℃高温冶炼而成。 An alumina-based ceramic core for directional solidification, which is characterized by using EC95 fused mullite as the base material, and EC95 fused mullite is a mineralizer with a weight percentage of 2-6% of high-quality alumina powder It is smelted at a high temperature of ≥2000°C in an electric arc furnace.
冶炼后的EC95电熔莫来石以a-Al2O3,3Al2O3·2SiO2为主要结晶体,其中α-Al2O3含量80~95%,3Al2O3·2SiO2含量5~20%,是一种具有结构致密、抗折强度大、膨胀均匀、热稳定性能好、荷重软化温度高、高温蠕变值小等良好的高温抗蠕变性能和高温稳定性的高级耐火材料。经粉碎整形,磁选去铁,筛分成粒度为F200号、F320号、F600号的粉料,并酸洗干燥。 The EC95 fused mullite after smelting has a-Al 2 O 3 , 3Al 2 O 3 2SiO 2 as the main crystals, in which the content of α-Al 2 O 3 is 80-95%, and the content of 3Al 2 O 3 2SiO 2 is 5% ~20%, it is a kind of advanced refractory material with good high-temperature creep resistance and high-temperature stability, such as compact structure, high flexural strength, uniform expansion, good thermal stability, high load softening temperature, and low high-temperature creep value. . After crushing and shaping, magnetic separation to remove iron, sieve into powders with particle sizes of F200, F320, and F600, and pickle and dry.
矿化剂采用硅酸锆、二氧化硅粉、二氧化钛粉和铝粉。硅酸锆粒度为F320号,二氧化硅粉,粒度为F320号,粉料中SiO2含量≥96%,二氧化钛粉尺寸≤30μm,TiO2含量≥97%,铝粉尺寸≤50μm,活性Al含量≥98%。 The mineralizer adopts zirconium silicate, silicon dioxide powder, titanium dioxide powder and aluminum powder. The particle size of zirconium silicate is F320, the silica powder is F320, the SiO2 content in the powder is ≥96%, the titanium dioxide powder size is ≤30μm, the TiO2 content is ≥97%, the aluminum powder size is ≤50μm, and the active Al content ≥98%.
一种定向凝固用氧化铝基陶瓷型芯的制备方法,其特征在于包括以下工艺步骤: A method for preparing an alumina-based ceramic core for directional solidification, characterized in that it comprises the following process steps:
1、称取粉料:分别称量一定重量的EC95电熔莫来石粉、硅酸锆粉、二氧化硅粉、二氧化钛粉、铝粉放入球磨罐中。粉料中按重量百分比EC95电熔莫来石65~95%,硅酸锆5~30%,二氧化硅粉2~8%,二氧化钛粉1~5%,铝粉1~10%。其中EC95电熔莫来石中F200号粉料占10~30%,F320号粉料含量40~70%,F600号粉料占10~30%。 1. Weigh the powder: Weigh a certain weight of EC95 fused mullite powder, zirconium silicate powder, silicon dioxide powder, titanium dioxide powder and aluminum powder respectively and put them into the ball mill tank. In the powder, EC95 fused mullite is 65-95% by weight, zirconium silicate is 5-30%, silicon dioxide powder is 2-8%, titanium dioxide powder is 1-5%, and aluminum powder is 1-10%. Among them, F200 powder in EC95 fused mullite accounts for 10-30%, F320 powder accounts for 40-70%, and F600 powder accounts for 10-30%.
2、球混:添加占粉料重量0.5~2%的油酸,按球料比1.5:1加入氧化锆陶瓷球混合,球混时间4~8h。 2. Ball mixing: Add 0.5-2% oleic acid in the weight of the powder, add zirconia ceramic balls for mixing according to the ball-to-material ratio of 1.5:1, and the ball mixing time is 4-8 hours.
3、配增塑剂:称取占步骤1中所述混合粉料重量14~18%的增塑剂,增塑剂中石蜡和聚乙烯的比例为46~49:1。把增塑剂放入芯料搅拌机中加热熔化,熔化温度为90~110℃。 3. Prepare plasticizer: weigh the plasticizer which accounts for 14-18% of the weight of the mixed powder mentioned in step 1. The ratio of paraffin wax to polyethylene in the plasticizer is 46-49:1. Put the plasticizer into the core material mixer and heat to melt, the melting temperature is 90-110°C.
4、混炼:把步骤1中所述混合均匀的混合粉料缓慢加入到芯料搅拌机中,继续搅拌6~8h,使增塑剂和粉料混炼均匀。 4. Mixing: Slowly add the uniformly mixed powder described in step 1 into the core material mixer, and continue stirring for 6-8 hours to make the plasticizer and powder mix evenly.
5、热压注成型。利用陶瓷型芯压注机,根据陶瓷型芯的尺寸和复杂程度,控制注射温度为90℃、模具温度45℃、注射压力2MPa、保压时间120s等成型参数,把混炼均匀的芯料压注到陶瓷芯模具中,制成陶瓷芯素坯。 5. Hot pressing injection molding. Using a ceramic core injection machine, according to the size and complexity of the ceramic core, control the molding parameters such as injection temperature at 90°C, mold temperature at 45°C, injection pressure at 2MPa, and pressure holding time at 120s to press the uniformly mixed core material Inject into the ceramic core mold to make the ceramic core blank.
6、修整、校型:陶瓷芯素坯经修整、校型后,放入匣钵中用工业氧化铝填料埋实。 6. Trimming and calibration: after trimming and calibration, the ceramic core blank is put into a sagger and buried with industrial alumina filler.
7、焙烧。把装有陶瓷芯素坯和工业氧化铝填料的匣钵放入箱式电阻炉中进行焙烧,焙烧制度为:以2~5℃/min的升温速率升温至200~300℃,保温3~6h,以3~6℃/min的升温速率升温至400~500℃,保温2~4h,以4~7℃/min的升温速率升温至600~700℃,保温1~2h,以6~9℃/min升温速率升温至900~1000℃,保温1~2h,以6~9℃/min的升温速率升温至1100~1200℃,保温2~3h,以1~2℃/min的升温速率升温至1300~1450℃,保温4~8h,然后随炉冷却至室温。 7. Roasting. Put the sagger with ceramic core blank and industrial alumina filler into a box-type resistance furnace for firing. The firing system is as follows: heat up to 200-300°C at a heating rate of 2-5°C/min, and keep warm for 3-6 hours , heat up to 400-500°C at a heating rate of 3-6°C/min, keep warm for 2-4 hours, heat up to 600-700°C at a heating rate of 4-7°C/min, keep warm for 1-2 hours, and keep warm at 6-9°C /min heating rate to 900-1000°C, keep warm for 1-2 hours, heat up to 1100-1200°C at a heating rate of 6-9°C/min, keep warm for 2-3 hours, and heat up at a heating rate of 1-2°C/min to 1300~1450℃, keep warm for 4~8h, then cool down to room temperature with the furnace.
焙烧过程中氧化铝基陶瓷型芯发生复杂的物理化学变化。低于500℃,陶瓷芯素坯中的增塑剂熔化、向填料中迁移,直至分解挥发。在500~1100℃铝粉氧化生成γ-Al2O3并伴随28%的体积膨胀,氧化生成的γ-Al2O3具有很高的活性。温度升高到1200℃,在二氧化钛的催化作用下硅酸锆分解生成SiO2和ZrO2,分解生成的SiO2具有高活性。高活性的SiO2与铝粉氧化生成的高活性γ-Al2O3反应生成莫来石。温度高于1200℃,在高活性的SiO2与铝粉氧化生成的高活性Al2O3反应生成的莫来石籽晶基质上,添加剂二氧化硅和EC95中的α-Al2O3反应生成莫来石。莫来石的生成伴随着6~10%的体积膨胀。同时,二氧化钛固溶到二氧化锆中,起稳定二氧化锆的作用,避免了二氧化锆从高温四方晶型转变为低温单斜晶型。未参与反应的γ-Al2O3在大于1200℃发生晶型转变生成α-Al2O3。整个过程的化学反应如下: Complex physical and chemical changes occur in the alumina-based ceramic core during the firing process. Below 500°C, the plasticizer in the ceramic core blank melts and migrates into the filler until it decomposes and volatilizes. At 500~1100℃, aluminum powder is oxidized to form γ-Al 2 O 3 with a volume expansion of 28%, and the γ-Al 2 O 3 produced by oxidation has high activity. When the temperature rises to 1200°C, zirconium silicate decomposes to generate SiO 2 and ZrO 2 under the catalysis of titanium dioxide, and the SiO 2 generated by the decomposition has high activity. The highly active SiO 2 reacts with the highly active γ-Al 2 O 3 generated by the oxidation of aluminum powder to form mullite. The temperature is higher than 1200 ℃, on the mullite seed matrix formed by the reaction of highly active SiO 2 and the highly active Al 2 O 3 generated by the oxidation of aluminum powder, the additive silica reacts with α-Al 2 O 3 in EC95 Generate mullite. The formation of mullite is accompanied by a volume expansion of 6-10%. At the same time, titanium dioxide dissolves into zirconium dioxide to stabilize zirconium dioxide and prevent zirconium dioxide from changing from a high-temperature tetragonal crystal to a low-temperature monoclinic crystal. The γ-Al 2 O 3 that did not participate in the reaction undergoes a crystal transformation to α-Al 2 O 3 at temperatures above 1200°C. The chemical reaction of the whole process is as follows:
4Al+3O4Al+3O 22 →2γ-Al→2γ-Al 22 Oo 33
ZrSiOZrSiO 44 →ZrO→ZrO 22 +SiO+SiO2 22
3γ-Al3γ-Al 22 Oo 33 +2SiO+2SiO 22 →3Al→3Al 22 Oo 33 ·2SiO2SiO2 22
3α-Al3α-Al 22 Oo 33 +2SiO+2SiO 22 →3Al→3Al 22 Oo 33 ·2SiO2SiO2 22
ZrOZrO 22 +TiO+TiO 22 →ZrO→ZrO 22 ·TiO·TiO 22
γ-Alγ-Al 22 Oo 33 →α-Al→α-Al 22 Oo 33
8、高温强化。出炉后的陶瓷型芯采用硅酸乙酯水解液进行高温强化。强化剂按重量百分比含硅酸乙酯81~83%,酒精11~12%,蒸馏水4~6%,盐酸1~1.5%含量进行配比,水解过程中严格控制水解液的温度,温度高于54℃要立刻用冷却水冷却。 8. High temperature strengthening. After being fired, the ceramic core is strengthened at high temperature with ethyl silicate hydrolyzate. The strengthening agent contains 81-83% ethyl silicate, 11-12% alcohol, 4-6% distilled water, and 1-1.5% hydrochloric acid by weight. During the hydrolysis process, the temperature of the hydrolyzate is strictly controlled, and the temperature is higher than 54 ℃ to immediately cool with cooling water.
9、室温强化。对高温强化并干燥后的陶瓷型芯进行室温强化,强化剂中按重量百分比含酚醛醇溶清漆50~55%,乙醇40~45%,六次甲基四胺2~5%。 9. Room temperature strengthening. The room temperature strengthening is performed on the ceramic core after high temperature strengthening and drying, and the strengthening agent contains 50-55% of novolac varnish, 40-45% of ethanol, and 2-5% of hexamethylenetetramine in weight percentage.
本发明的优点在于: The advantages of the present invention are:
(1)降低烧成收缩。焙烧过程中,铝粉氧化生成氧化铝以及二氧化硅与氧化铝反应生成莫来石发生的体积膨胀,补偿了型芯焙烧发生的体积收缩。使氧化铝基陶瓷芯的烧成收缩降低到1%以下。 (1) Reduce firing shrinkage. During the roasting process, the volume expansion of the aluminum powder oxidized to form alumina and the reaction of silica and alumina to form mullite compensates for the volume shrinkage of the core roasting. Reduce the firing shrinkage of the alumina-based ceramic core to less than 1%.
(2)降低烧成温度。硅酸锆的分解温度为1540℃,二氧化钛促进硅酸锆分解,使硅酸锆的分解温度降低到1200℃。莫来石的生成温度也为1540℃左右。而铝粉氧化生成的高活性氧化铝和硅酸锆分解生成的高活性二氧化硅反应生成莫来石的温度为1200℃,大大降低了莫来石的生成温度。氧化铝基陶瓷芯的烧成温度降低到1300~1450℃。 (2) Lower the firing temperature. The decomposition temperature of zirconium silicate is 1540°C, and titanium dioxide promotes the decomposition of zirconium silicate, reducing the decomposition temperature of zirconium silicate to 1200°C. The formation temperature of mullite is also about 1540°C. However, the high-activity alumina produced by the oxidation of aluminum powder and the high-activity silica produced by the decomposition of zirconium silicate react to form mullite at a temperature of 1200 ° C, which greatly reduces the formation temperature of mullite. The firing temperature of the alumina-based ceramic core is reduced to 1300-1450°C.
(3)提高高温性能。化学反应生成的高温粘结剂莫来石,是一种性能优异的耐火材料。熔点为1890±90℃,高温强度和荷重软化温度高,有良好的抗热震性能和高温蠕变性能。而硅酸锆分解生成的二氧化锆熔点高达2680℃,强化了氧化铝基陶瓷芯的高温性能。通过莫来石和二氧化锆的强化作用,氧化铝陶瓷芯1550℃的抗弯强度≥5MPa,自重变形量≤1mm。 (3) Improve high temperature performance. The high-temperature binder mullite produced by chemical reaction is a refractory material with excellent performance. The melting point is 1890±90°C, the high temperature strength and load softening temperature are high, and it has good thermal shock resistance and high temperature creep performance. The melting point of zirconium dioxide produced by the decomposition of zirconium silicate is as high as 2680°C, which strengthens the high-temperature performance of the alumina-based ceramic core. Through the strengthening effect of mullite and zirconia, the bending strength of the alumina ceramic core at 1550°C is ≥5MPa, and the self-weight deformation is ≤1mm.
附图说明 Description of drawings
图1是氧化铝基陶瓷芯制备过程流程图。 Figure 1 is a flowchart of the preparation process of alumina-based ceramic cores.
图2是氧化铝基陶瓷芯焙烧制度示意图。 Fig. 2 is a schematic diagram of the firing system of the alumina-based ceramic core.
具体实施方式 Detailed ways
具体实施例1Specific embodiment 1
一种定向凝固用氧化铝基陶瓷型芯,其特征是以EC95电熔莫来石为基料,EC95电熔莫来石是以优质铝氧粉加重量百分比为2%的矿化剂于电弧炉中经2100℃高温冶炼而成。冶炼后的EC95电熔莫来石以a-Al2O3,3Al2O3·2SiO2为主要结晶体,其中α-Al2O3含量93%,3Al2O3·2SiO2含量7%。 An alumina-based ceramic core for directional solidification, which is characterized in that it uses EC95 fused mullite as the base material, and the EC95 fused mullite is made of high-quality alumina powder plus a mineralizer with a weight percentage of 2%. It is smelted at a high temperature of 2100°C in a furnace. The smelted EC95 fused mullite has a-Al 2 O 3 and 3Al 2 O 3 ·2SiO 2 as the main crystals, of which the content of α-Al 2 O 3 is 93%, and the content of 3Al 2 O 3 ·2SiO 2 is 7%.
一种定向凝固用氧化铝基陶瓷型芯的制备方法,包括下述步骤: A method for preparing an alumina-based ceramic core for directional solidification, comprising the steps of:
1、称取粉料:把冶炼后的EC95电熔莫来石粉碎 整形,磁选去铁,筛分成粒度为F200号、F320号、F600号的粉料,并酸洗干燥。按重量百分比称取15%的F200号EC95、50%的F320号EC95、15%的F600号EC95,10%的硅酸锆粉,5%的二氧化硅粉,2%的二氧化钛,3%的铝粉。 1. Weigh the powder: crush and shape the smelted EC95 fused mullite, remove iron by magnetic separation, sieve into powders with particle sizes of F200, F320, and F600, and pickle and dry. Weigh 15% F200 EC95, 50% F320 EC95, 15% F600 EC95, 10% zirconium silicate powder, 5% silica powder, 2% titanium dioxide, 3% Aluminum powder.
2、球混:添加占步骤1中所述混合粉料重量1%的油酸,按球料比1.5:1加入氧化锆陶瓷球混合,球混时间4h。 2. Ball mixing: Add oleic acid accounting for 1% of the weight of the mixed powder mentioned in step 1, and add zirconia ceramic balls for mixing according to the ball-to-material ratio of 1.5:1, and the ball mixing time is 4 hours.
3、配增塑剂:称取占步骤1中所述混合粉料重量14%的增塑剂,增塑剂中石蜡和聚乙烯的比例为49:1。把增塑剂放入芯料搅拌机中加热熔化,熔化温度为110℃。 3. Prepare plasticizer: Weigh the plasticizer accounting for 14% of the weight of the mixed powder described in step 1. The ratio of paraffin wax to polyethylene in the plasticizer is 49:1. Put the plasticizer into the core material mixer and heat to melt, and the melting temperature is 110°C.
4、混炼:把步骤1中所述混合均匀的混合粉料缓慢加入到芯料搅拌机中,继续搅拌8h,使增塑剂和粉料混炼均匀。 4. Mixing: Slowly add the homogeneously mixed powder described in step 1 into the core material mixer, and continue stirring for 8 hours to make the plasticizer and powder knead evenly.
5、热压注成型:利用陶瓷型芯压注机,控制注射温度为90℃、模具温度45℃、注射压力2MPa、保压时间120s,把混炼均匀的芯料压注到陶瓷芯模具中,制成陶瓷芯素坯。 5. Hot pressure injection molding: Use a ceramic core injection machine to control the injection temperature at 90°C, mold temperature at 45°C, injection pressure at 2MPa, and pressure holding time of 120s, and press-inject the uniformly mixed core material into the ceramic core mold , made of ceramic core blank.
6、修整、校型:陶瓷芯素坯经修整、校型后,放入匣钵中用工业氧化铝填料埋实。 6. Trimming and calibration: after trimming and calibration, the ceramic core blank is put into a sagger and buried with industrial alumina filler.
7、焙烧:把装有陶瓷芯素坯和工业氧化铝填料的匣钵放入箱式电阻炉中进行焙烧,焙烧制度为:以2℃/min的升温速率升温至240℃,保温4h,以3℃/min的升温速率升温至500℃,保温4h,以4℃/min的升温速率升温至700℃,保温1.5h,以6℃/min升温速率升温至1000℃,保温1h,以7℃/min的升温速率升温至1200℃,保温2.5h,以2℃/min的升温速率升温至1350℃,保温6h,然后随炉冷却至室温。 7. Roasting: put the sagger with ceramic core blank and industrial alumina filler into a box-type resistance furnace for roasting, the roasting system is: heat up to 240°C at a heating rate of 2°C/min, keep warm for 4h, and Heat up to 500°C at a heating rate of 3°C/min, hold for 4 hours, heat up to 700°C at a heating rate of 4°C/min, hold for 1.5 hours, heat up to 1000°C at a heating rate of 6°C/min, hold for 1 hour, and heat at 7°C Raise the temperature to 1200°C at a heating rate of 2°C/min, keep it warm for 2.5 hours, raise the temperature to 1350°C at a heating rate of 2°C/min, keep it warm for 6 hours, and then cool to room temperature with the furnace.
8、高温强化:出炉后的陶瓷型芯采用硅酸乙酯水解液进行高温强化。强化剂按重量百分比含硅酸乙酯81%,酒精12%,蒸馏水6%,盐酸1%含量进行配比,水解过程中严格控制水解液的温度,温度高于54℃要立刻用冷却水冷却。 8. High temperature strengthening: The ceramic core after being released from the furnace is strengthened at high temperature with ethyl silicate hydrolyzate. The strengthening agent contains 81% ethyl silicate, 12% alcohol, 6% distilled water, and 1% hydrochloric acid by weight. During the hydrolysis process, the temperature of the hydrolyzate is strictly controlled. If the temperature is higher than 54°C, it should be cooled with cooling water immediately. .
9、室温强化:对高温强化并干燥后的陶瓷型芯进行室温强化,强化剂中按重量百分比含酚醛醇溶清漆53%,乙醇44%,六次甲基四胺3%。 9. Strengthening at room temperature: Carry out room temperature strengthening to the ceramic core after high temperature strengthening and drying. The strengthening agent contains 53% novolac varnish by weight, 44% ethanol, and 3% hexamethylenetetramine.
具体实施例2Specific embodiment 2
一种定向凝固用氧化铝基陶瓷型芯,其特征是以EC95电熔莫来石为基料,EC95电熔莫来石是以优质铝氧粉加重量百分比为3.5%的矿化剂于电弧炉中经2150℃高温冶炼而成。冶炼后的EC95电熔莫来石以a-Al2O3,3Al2O3·2SiO2为主要结晶体,其中α-Al2O3含量88%,3Al2O3·2SiO2含量12%。 An alumina-based ceramic core for directional solidification, which is characterized in that it uses EC95 fused mullite as the base material, and the EC95 fused mullite is made of high-quality alumina powder plus a mineralizer with a weight percentage of 3.5% in the arc It is smelted at a high temperature of 2150°C in a furnace. The smelted EC95 fused mullite has a-Al 2 O 3 and 3Al 2 O 3 ·2SiO 2 as the main crystals, of which the content of α-Al 2 O 3 is 88%, and the content of 3Al 2 O 3 ·2SiO 2 is 12%.
一种定向凝固用氧化铝基陶瓷型芯的制备方法,包括下述步骤: A method for preparing an alumina-based ceramic core for directional solidification, comprising the steps of:
1、称取粉料:把冶炼后的EC95电熔莫来石粉碎 整形,磁选去铁,筛分成粒度为F200号、F320号、F600号的粉料,并酸洗干燥。按重量百分比称取10%的F200号EC95、45%的F320号EC95、12%的F600号EC95,20%的硅酸锆粉,2%的二氧化硅粉,1%的二氧化钛,10%的铝粉。 1. Weigh the powder: crush and shape the smelted EC95 fused mullite, remove iron by magnetic separation, sieve into powders with particle sizes of F200, F320, and F600, and pickle and dry. Weigh 10% F200 EC95, 45% F320 EC95, 12% F600 EC95, 20% zirconium silicate powder, 2% silica powder, 1% titanium dioxide, 10% Aluminum powder.
2、球混:添加占步骤1中所述混合粉料重量1.5%的油酸,按球料比1.5:1加入氧化锆陶瓷球混合,球混时间6h。 2. Ball mixing: Add oleic acid accounting for 1.5% of the weight of the mixed powder mentioned in step 1, and add zirconia ceramic balls for mixing according to the ball-to-material ratio of 1.5:1, and the ball mixing time is 6 hours.
3、配增塑剂:称取占步骤1中所述混合粉料重量16%的增塑剂,增塑剂中石蜡和聚乙烯的比例为48:1。把增塑剂放入芯料搅拌机中加热熔化,熔化温度为100℃。 3. Adding a plasticizer: Weigh a plasticizer accounting for 16% of the weight of the mixed powder described in step 1. The ratio of paraffin wax to polyethylene in the plasticizer is 48:1. Put the plasticizer into the core material mixer and heat to melt, and the melting temperature is 100°C.
4、混炼:把步骤1中所述混合均匀的混合粉料缓慢加入到芯料搅拌机中,继续搅拌7h,使增塑剂和粉料混炼均匀。 4. Mixing: Slowly add the homogeneously mixed powder described in step 1 into the core material mixer, and continue stirring for 7 hours to make the plasticizer and powder knead evenly.
5、热压注成型:利用陶瓷型芯压注机,控制注射温度为95℃、模具温度40℃、注射压力3MPa、保压时间150s,把混炼均匀的芯料压注到陶瓷芯模具中,制成陶瓷芯素坯。 5. Hot pressure injection molding: use a ceramic core injection machine, control the injection temperature to 95°C, mold temperature to 40°C, injection pressure to 3MPa, pressure holding time to 150s, and inject the uniformly mixed core material into the ceramic core mold , made of ceramic core blank.
6、修整、校型:陶瓷芯素坯经修整、校型后,放入匣钵中用工业氧化铝填料埋实。 6. Trimming and calibration: after trimming and calibration, the ceramic core blank is put into a sagger and buried with industrial alumina filler.
7、焙烧:把装有陶瓷芯素坯和工业氧化铝填料的匣钵放入箱式电阻炉中进行焙烧,焙烧制度为:以2.5℃/min的升温速率升温至260℃,保温5h,以4℃/min的升温速率升温至480℃,保温3h,以5℃/min的升温速率升温至650℃,保温2h,以7℃/min升温速率升温至950℃,保温1.5h,以9℃/min的升温速率升温至1150℃,保温3h,以1.5℃/min的升温速率升温至1400℃,保温4h,然后随炉冷却至室温。 7. Roasting: put the sagger with the ceramic core green body and the industrial alumina filler into the box-type resistance furnace for roasting, the roasting system is: heat up to 260 °C at a heating rate of 2.5 °C/min, keep the temperature for 5 hours, and Heat up to 480°C at a heating rate of 4°C/min, hold for 3 hours, heat up to 650°C at a heating rate of 5°C/min, hold for 2 hours, heat up to 950°C at a heating rate of 7°C/min, hold for 1.5 hours, and heat at 9°C Raise the temperature to 1150°C at a heating rate of 1.5°C/min, hold for 3 hours, raise the temperature to 1400°C at a heating rate of 1.5°C/min, hold for 4 hours, and then cool to room temperature with the furnace.
8、高温强化:出炉后的陶瓷型芯采用硅酸乙酯水解液进行高温强化。强化剂按重量百分比含硅酸乙酯82%,酒精11%,蒸馏水5.5%,盐酸1.5%含量进行配比,水解过程中严格控制水解液的温度,温度高于54℃要立刻用冷却水冷却。 8. High temperature strengthening: The ceramic core after being released from the furnace is strengthened at high temperature with ethyl silicate hydrolyzate. The strengthening agent contains 82% ethyl silicate, 11% alcohol, 5.5% distilled water, and 1.5% hydrochloric acid by weight. During the hydrolysis process, the temperature of the hydrolyzate is strictly controlled. If the temperature is higher than 54°C, it should be cooled with cooling water immediately. .
9、室温强化:对高温强化并干燥后的陶瓷型芯进行室温强化,强化剂中按重量百分比含酚醛醇溶清漆50%,乙醇45%,六次甲基四胺5%。 9. Strengthening at room temperature: Carry out room temperature strengthening to the ceramic core after high temperature strengthening and drying. The strengthening agent contains 50% phenolic alcohol-soluble varnish, 45% ethanol, and 5% hexamethylenetetramine in the strengthening agent.
具体实施例3
一种定向凝固用氧化铝基陶瓷型芯,其特征是以EC95电熔莫来石为基料,EC95电熔莫来石是以优质铝氧粉加重量百分比为5.5%的矿化剂于电弧炉中经2200℃高温冶炼而成。冶炼后的EC95电熔莫来石以a-Al2O3,3Al2O3·2SiO2为主要结晶体,其中α-Al2O3含量80.5%,3Al2O3·2SiO2含量19.5%。 An alumina-based ceramic core for directional solidification, which is characterized in that it uses EC95 fused mullite as the base material, and the EC95 fused mullite is made of high-quality alumina powder plus a mineralizer with a weight percentage of 5.5% in the arc It is smelted at a high temperature of 2200°C in a furnace. The smelted EC95 fused mullite has a-Al 2 O 3 and 3Al 2 O 3 ·2SiO 2 as the main crystals, of which the content of α-Al 2 O 3 is 80.5%, and the content of 3Al 2 O 3 ·2SiO 2 is 19.5%.
一种定向凝固用氧化铝基陶瓷型芯的制备方法,包括下述步骤: A method for preparing an alumina-based ceramic core for directional solidification, comprising the steps of:
1、称取粉料:把冶炼后的EC95电熔莫来石粉碎 整形,磁选去铁,筛分成粒度为F200号、F320号、F600号的粉料,并酸洗干燥。按重量百分比称取12%的F200号EC95、40%的F320号EC95、13%的F600号EC95,25%的硅酸锆粉,1%的二氧化硅粉,4%的二氧化钛,5%的铝粉。 1. Weigh the powder: crush and shape the smelted EC95 fused mullite, remove iron by magnetic separation, sieve into powders with particle sizes of F200, F320, and F600, and pickle and dry. Weigh 12% F200 EC95, 40% F320 EC95, 13% F600 EC95, 25% zirconium silicate powder, 1% silica powder, 4% titanium dioxide, 5% Aluminum powder.
2、球混:添加占步骤1中所述混合粉料重量0.5%的油酸,按球料比1.5:1加入氧化锆陶瓷球混合,球混时间8h。 2. Ball mixing: add oleic acid accounting for 0.5% of the weight of the mixed powder described in step 1, and add zirconia ceramic balls for mixing according to the ball-to-material ratio of 1.5:1, and the ball mixing time is 8 hours.
3、配增塑剂:称取占步骤1中所述混合粉料重量16%的增塑剂,增塑剂中石蜡和聚乙烯的比例为47:1。把增塑剂放入芯料搅拌机中加热熔化,熔化温度为105℃。 3. Prepare plasticizer: Weigh the plasticizer accounting for 16% of the weight of the mixed powder described in step 1. The ratio of paraffin wax to polyethylene in the plasticizer is 47:1. Put the plasticizer into the core material mixer and heat it to melt, and the melting temperature is 105°C.
4、混炼:把步骤1中所述混合均匀的混合粉料缓慢加入到芯料搅拌机中,继续搅拌8h,使增塑剂和粉料混炼均匀。 4. Mixing: Slowly add the homogeneously mixed powder described in step 1 into the core material mixer, and continue stirring for 8 hours to make the plasticizer and powder knead evenly.
5、热压注成型:利用陶瓷型芯压注机,控制注射温度为100℃、模具温度50℃、注射压力5MPa、保压时间180s,把混炼均匀的芯料压注到陶瓷芯模具中,制成陶瓷芯素坯。 5. Hot pressure injection molding: use a ceramic core injection machine, control the injection temperature to 100°C, the mold temperature to 50°C, the injection pressure to 5MPa, and the pressure holding time to 180s, and inject the uniformly mixed core material into the ceramic core mold , made of ceramic core blank.
6、修整、校型:陶瓷芯素坯经修整、校型后,放入匣钵中用工业氧化铝填料埋实。 6. Trimming and calibration: after trimming and calibration, the ceramic core blank is put into a sagger and buried with industrial alumina filler.
7、焙烧:把装有陶瓷芯素坯和工业氧化铝填料的匣钵放入箱式电阻炉中进行焙烧,焙烧制度为:以4℃/min的升温速率升温至300℃,保温6h,以6℃/min的升温速率升温至500℃,保温2h,以6℃/min的升温速率升温至600℃,保温1h,以8℃/min升温速率升温至900℃,保温2h,以8℃/min的升温速率升温至1100℃,保温2h,以2℃/min的升温速率升温至1450℃,保温8h,然后随炉冷却至室温。 7. Roasting: Put the sagger with the ceramic core green body and the industrial alumina filler into the box-type resistance furnace for roasting. The roasting system is: heat up to 300 °C at a heating rate of 4 °C/min, keep the temperature for 6 hours, and Heat up to 500°C at a heating rate of 6°C/min, hold for 2 hours, heat up to 600°C at a heating rate of 6°C/min, hold for 1 hour, heat up to 900°C at a heating rate of 8°C/min, hold for 2 hours, and heat at 8°C/min Raise the temperature to 1100°C at a heating rate of 1 min, keep it warm for 2 hours, raise the temperature to 1450°C at a heating rate of 2°C/min, keep it warm for 8 hours, and then cool to room temperature with the furnace.
8、高温强化:出炉后的陶瓷型芯采用硅酸乙酯水解液进行高温强化。强化剂按重量百分比含硅酸乙酯82%,酒精12%,蒸馏水5%,盐酸1%含量进行配比,水解过程中严格控制水解液的温度,温度高于54℃要立刻用冷却水冷却。 8. High temperature strengthening: The ceramic core after being released from the furnace is strengthened at high temperature with ethyl silicate hydrolyzate. The strengthening agent contains 82% ethyl silicate, 12% alcohol, 5% distilled water, and 1% hydrochloric acid by weight. During the hydrolysis process, the temperature of the hydrolyzate is strictly controlled. If the temperature is higher than 54°C, it should be cooled with cooling water immediately. .
9、室温强化:对高温强化并干燥后的陶瓷型芯进行室温强化,强化剂中按重量百分比含酚醛醇溶清漆55%,乙醇43%,六次甲基四胺2%。 9. Strengthening at room temperature: Carry out room temperature strengthening to the ceramic core after high temperature strengthening and drying. The strengthening agent contains 55% phenolic alcohol-soluble varnish, 43% ethanol, and 2% hexamethylenetetramine in the strengthening agent. the
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310269759.5A CN103304227B (en) | 2013-07-01 | 2013-07-01 | Alumina-based ceramic core for directional solidification and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310269759.5A CN103304227B (en) | 2013-07-01 | 2013-07-01 | Alumina-based ceramic core for directional solidification and preparation method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN103304227A true CN103304227A (en) | 2013-09-18 |
CN103304227B CN103304227B (en) | 2014-08-13 |
Family
ID=49129989
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201310269759.5A Active CN103304227B (en) | 2013-07-01 | 2013-07-01 | Alumina-based ceramic core for directional solidification and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN103304227B (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103553635A (en) * | 2013-10-30 | 2014-02-05 | 东方电气集团东方汽轮机有限公司 | Method for producing ceramic die core |
CN103693196A (en) * | 2013-12-29 | 2014-04-02 | 陈俞任 | Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft |
CN104311144A (en) * | 2014-09-19 | 2015-01-28 | 大连理工大学 | Layered alumina-epoxy resin composite material containing whisker perpendicular to bed interface and in directional alignment and preparation method thereof |
CN104402415A (en) * | 2014-11-10 | 2015-03-11 | 无锡康伟工程陶瓷有限公司 | Production method of silicon controlled rectifier deep diameter product |
CN105669198A (en) * | 2016-01-16 | 2016-06-15 | 上海大学 | Preparation method of lanthanum oxide-based ceramic core |
CN110128159A (en) * | 2019-06-01 | 2019-08-16 | 安徽齐鑫新材料科技有限公司 | A kind of preparation method of rare earth oxide Al-base ceramic core |
CN110256077A (en) * | 2019-07-09 | 2019-09-20 | 中国航发北京航空材料研究院 | A kind of hot investment casting yttria-base ceramic core and preparation method thereof |
CN110342914A (en) * | 2019-07-03 | 2019-10-18 | 金永和精工制造股份有限公司 | A kind of ceramic core and preparation method |
US10782222B2 (en) | 2015-10-20 | 2020-09-22 | Bayerische Motoren Werke Aktiengesellschaft | Diesel particulate sensor |
CN112047726A (en) * | 2020-09-02 | 2020-12-08 | 上海交通大学 | Preparation method of mullite whisker reinforced aluminum-based ceramic core for directional solidification |
CN113354398A (en) * | 2021-07-08 | 2021-09-07 | 西安石油大学 | Aluminum oxide-based high-entropy eutectic ceramic and preparation method thereof |
CN113370344A (en) * | 2021-04-28 | 2021-09-10 | 潍坊科技学院 | Preparation process of directional solidification ceramic part |
CN113860896A (en) * | 2021-11-03 | 2021-12-31 | 贵州安吉华元科技发展有限公司 | High-temperature precision casting low-creep corundum mullite and manufacturing method thereof |
CN114349491A (en) * | 2022-01-19 | 2022-04-15 | 北航(四川)西部国际创新港科技有限公司 | Composition for preparing silicon-based ceramic core, silicon-based ceramic core blade of aircraft engine and preparation method of silicon-based ceramic core blade |
CN116924815A (en) * | 2023-07-27 | 2023-10-24 | 中国科学院金属研究所 | A kind of hot pressing ceramic core and its preparation method |
CN119910128A (en) * | 2025-04-03 | 2025-05-02 | 成都航宇超合金技术有限公司 | Integrated casting method of hollow turbine blades with air film holes |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101386546A (en) * | 2008-10-14 | 2009-03-18 | 华南理工大学 | Self-reactive alumina-based composite ceramic core for precision casting and preparation method thereof |
CN101734910A (en) * | 2009-12-04 | 2010-06-16 | 沈阳黎明航空发动机(集团)有限责任公司 | Method for preparing porous alumina ceramic core |
CN102531648A (en) * | 2011-12-26 | 2012-07-04 | 北京航空航天大学 | Calcium oxide-based ceramic core for casting titanium alloy and manufacturing method thereof |
CN102989994A (en) * | 2012-11-28 | 2013-03-27 | 沈阳铸造研究所 | Preparation method of composite mold core for casting of titanium alloy |
-
2013
- 2013-07-01 CN CN201310269759.5A patent/CN103304227B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101386546A (en) * | 2008-10-14 | 2009-03-18 | 华南理工大学 | Self-reactive alumina-based composite ceramic core for precision casting and preparation method thereof |
CN101734910A (en) * | 2009-12-04 | 2010-06-16 | 沈阳黎明航空发动机(集团)有限责任公司 | Method for preparing porous alumina ceramic core |
CN102531648A (en) * | 2011-12-26 | 2012-07-04 | 北京航空航天大学 | Calcium oxide-based ceramic core for casting titanium alloy and manufacturing method thereof |
CN102989994A (en) * | 2012-11-28 | 2013-03-27 | 沈阳铸造研究所 | Preparation method of composite mold core for casting of titanium alloy |
Non-Patent Citations (1)
Title |
---|
张世东 等: "定向凝固铸造用氧化铝型壳热强度性能研究", 《铸造》, vol. 60, no. 04, 30 April 2011 (2011-04-30) * |
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103553635A (en) * | 2013-10-30 | 2014-02-05 | 东方电气集团东方汽轮机有限公司 | Method for producing ceramic die core |
CN103693196A (en) * | 2013-12-29 | 2014-04-02 | 陈俞任 | Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft |
CN104311144A (en) * | 2014-09-19 | 2015-01-28 | 大连理工大学 | Layered alumina-epoxy resin composite material containing whisker perpendicular to bed interface and in directional alignment and preparation method thereof |
CN104402415A (en) * | 2014-11-10 | 2015-03-11 | 无锡康伟工程陶瓷有限公司 | Production method of silicon controlled rectifier deep diameter product |
CN104402415B (en) * | 2014-11-10 | 2016-05-18 | 无锡康伟工程陶瓷有限公司 | The production method of the dark footpath of a kind of controllable silicon product |
US10782222B2 (en) | 2015-10-20 | 2020-09-22 | Bayerische Motoren Werke Aktiengesellschaft | Diesel particulate sensor |
CN105669198A (en) * | 2016-01-16 | 2016-06-15 | 上海大学 | Preparation method of lanthanum oxide-based ceramic core |
CN105669198B (en) * | 2016-01-16 | 2018-08-03 | 上海大学 | A kind of preparation method of lanthanum oxide-based ceramic core |
CN110128159A (en) * | 2019-06-01 | 2019-08-16 | 安徽齐鑫新材料科技有限公司 | A kind of preparation method of rare earth oxide Al-base ceramic core |
CN110342914A (en) * | 2019-07-03 | 2019-10-18 | 金永和精工制造股份有限公司 | A kind of ceramic core and preparation method |
CN110256077A (en) * | 2019-07-09 | 2019-09-20 | 中国航发北京航空材料研究院 | A kind of hot investment casting yttria-base ceramic core and preparation method thereof |
CN112047726A (en) * | 2020-09-02 | 2020-12-08 | 上海交通大学 | Preparation method of mullite whisker reinforced aluminum-based ceramic core for directional solidification |
CN113370344A (en) * | 2021-04-28 | 2021-09-10 | 潍坊科技学院 | Preparation process of directional solidification ceramic part |
CN113370344B (en) * | 2021-04-28 | 2023-02-21 | 潍坊科技学院 | A preparation process of directionally solidified ceramic parts |
CN113354398A (en) * | 2021-07-08 | 2021-09-07 | 西安石油大学 | Aluminum oxide-based high-entropy eutectic ceramic and preparation method thereof |
CN113860896A (en) * | 2021-11-03 | 2021-12-31 | 贵州安吉华元科技发展有限公司 | High-temperature precision casting low-creep corundum mullite and manufacturing method thereof |
CN114349491A (en) * | 2022-01-19 | 2022-04-15 | 北航(四川)西部国际创新港科技有限公司 | Composition for preparing silicon-based ceramic core, silicon-based ceramic core blade of aircraft engine and preparation method of silicon-based ceramic core blade |
CN116924815A (en) * | 2023-07-27 | 2023-10-24 | 中国科学院金属研究所 | A kind of hot pressing ceramic core and its preparation method |
CN119910128A (en) * | 2025-04-03 | 2025-05-02 | 成都航宇超合金技术有限公司 | Integrated casting method of hollow turbine blades with air film holes |
Also Published As
Publication number | Publication date |
---|---|
CN103304227B (en) | 2014-08-13 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103304227B (en) | Alumina-based ceramic core for directional solidification and preparation method thereof | |
CN103242036B (en) | Method for preparing composite ceramic core | |
CN101386546B (en) | Self-reacting alumina-base composite ceramic mold core for fine casting and preparation method thereof | |
CN102432332B (en) | A method for preparing alumina porous ceramics by gel-foaming method | |
CN106145969A (en) | Composition of ceramic powders, straight-bore ceramic filter and preparation method thereof | |
CN108424124B (en) | A kind of magnesia whisker in-situ synthesis of spinel reinforced magnesia-based crucible and preparation method thereof | |
CN109467419A (en) | A kind of graphene enhancing alumina based ceramic core and preparation method thereof | |
CN105732007B (en) | A kind of calcium oxide-based ceramic-mould fast preparation method for complex parts manufacture | |
CN101734910A (en) | Method for preparing porous alumina ceramic core | |
CN105272181A (en) | Preparation technology of composite ceramic core | |
CN104387073A (en) | Method for manufacturing ultrafine high-toughness silicon carbide ceramic material based on reaction sintering technology | |
CN103964874B (en) | Zirconium mullite sagger | |
CN108059445A (en) | Calcium oxide-based ceramic-mould that a kind of non-aqueous gel casting quickly manufactures and preparation method thereof | |
CN112390633A (en) | ZrB2Nano powder reinforced silica-based ceramic core and preparation method thereof | |
CN107619273B (en) | A method for preparing terbium aluminum garnet-based magneto-optical transparent ceramics by non-aqueous gel injection molding | |
CN108546093B (en) | A kind of alumina short fiber reinforced magnesia-based crucible and preparation method thereof | |
CN108218444A (en) | A kind of toughening saggar of andalusite containing zirconium and preparation method | |
CN103894537A (en) | Composite oxide shell for directional solidification technology as well as application thereof | |
CN109081687A (en) | A kind of highly heatproof and shockproof ceramic crucible and preparation method thereof suitable for calcining anode material of lithium battery | |
CN101486572A (en) | Process for preparing ZrO2-Al2TiO5 composite material | |
CN107879735B (en) | A kind of preparation method of medium-high temperature and low expansion coefficient forsterite-spodumene composite ceramic material | |
CN114082881B (en) | A preparation method of a silicon-based ceramic core for an aeroengine blade | |
CN110256077A (en) | A kind of hot investment casting yttria-base ceramic core and preparation method thereof | |
CN109574661A (en) | A kind of preparation method and application of barium zirconate ceramic core | |
CN116477960A (en) | Composite ceramic core for single crystal turbine blade and preparation method thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CP01 | Change in the name or title of a patent holder | ||
CP01 | Change in the name or title of a patent holder |
Address after: No.17, Yunfeng South Street, Tiexi District, Shenyang City, Liaoning Province Patentee after: SHENYANG RESEARCH INSTITUTE OF FOUNDRY Co.,Ltd. Address before: No.17, Yunfeng South Street, Tiexi District, Shenyang City, Liaoning Province Patentee before: Shenyang Research Institute OF Foundry Address after: No.17, Yunfeng South Street, Tiexi District, Shenyang City, Liaoning Province Patentee after: Shenyang Foundry Research Institute Co., Ltd. of China National Machinery Research Institute Group Address before: No.17, Yunfeng South Street, Tiexi District, Shenyang City, Liaoning Province Patentee before: SHENYANG RESEARCH INSTITUTE OF FOUNDRY Co.,Ltd. |