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首页> 外文期刊>日本セラミックス協会学術論文誌 >Influence of Heat Treatment on Phases, Microstructures and Mechanical Properties of Laminated Fabric (SiC and Aluminosilicate)/Mullite Matrix Composites (Part 2)
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Influence of Heat Treatment on Phases, Microstructures and Mechanical Properties of Laminated Fabric (SiC and Aluminosilicate)/Mullite Matrix Composites (Part 2)

机译:热处理对层合织物(SiC和铝硅酸盐)/莫来石基复合材料的相,微结构和力学性能的影响(第2部分)

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摘要

Influence of heat treatment at 1000-1500 deg C for 24 h on phases, microstructures and mechanical properties was studied for laminated SiC satin or aluminosilicate plain fabric/mullite matrix composites. Composites were produced by a polymer impregnation and pyrolysis method (PIP) using a mullite precursor. A mullite precursor solution of the mixtures of Si(OC_2H_5)_4 and Al(NO_3)_3 was impregnated into the green layered fabric/mullite powder (filler) composite and was pyrolyzed at 500 deg C in air. This polymer impregnation and pyrolysis process was repeated 10 times. The SiC fabric (25-27 vol percent)/mullite matrix composite with a relative density 72-75 percent showed weight loss after heat treatment in an Ar atmosphere (oxygen partial pressure approx 0.75 Pa) at 1300-1500 deg C. This weight loss was due to the formation of volatile SiO gas resulting from the pyrolysis of mullite matrix (3Al_2O_3 centre dot 2SiO_2 (s) -> 3Al_2O_3 (s) + 2SiO (g) + O_2 (g)) and active oxidation of the SiC fiber (SiC (s) + O_2 (g) ->SiO (g) + CO (g)). The heat-treated SiC fabric/mullite matrix composites showed an elastic deformation in the initial stage of the stress-displacement curve, followed by pseudoductility. The strength (186 MPa) after the 1000 deg C heat treatment decreased to 17 MPa after the 1500 deg C heat treatment. The energy of fracture was 1-4 kJ/ m2 in the heat treatment temperature range from 1000 to 1500 deg C.On the other hand, the aluminosilicate fabric (25-30 vol percent )/mullite matrix composite with a relative density 71-73 percent showed no weight loss after heat treatment at 1000-1500 deg C in air. The porosity of the composite decreased with increasing heat treatment temperature because of the densification of the mullite matrix. This composite also showed pseudoductility after the heat treatment. The strength for the composite was slightly enhanced by increasing the heat treatment temperature.
机译:研究了层压SiC缎或铝硅酸盐平纹织物/莫来石基质复合材料在1000-1500℃下热处理24小时对相,微观结构和力学性能的影响。使用莫来石前体通过聚合物浸渍和热解方法(PIP)生产复合材料。将Si(OC_2H_5)_4和Al(NO_3)_3的混合物的莫来石前体溶液浸渍到生的层状织物/莫来石粉末(填料)复合物中,并在空气中于500℃下热解。将该聚合物浸渍和热解过程重复10次。相对密度为72-75%的SiC纤维(25-27%(体积))/莫来石基复合材料在1300-1500℃的Ar气氛(氧分压约为0.75 Pa)中热处理后显示出重量损失。这是由于热解莫来石基质(3Al_2O_3中心点2SiO_2(s)-> 3Al_2O_3(s)+ 2SiO(g)+ O_2(g))以及SiC纤维(SiC (s)+ O_2(g)-> SiO(g)+ CO(g))。热处理后的SiC织物/莫来石基复合材料在应力-位移曲线的初始阶段显示出弹性变形,然后是假延性。 1000℃热处理后的强度(186MPa)降低到1500℃热处理后的17MPa。在1000到1500℃的热处理温度下断裂能量为1-4 kJ / m2。另一方面,相对密度为71-73的铝硅酸盐织物(25-30 vol%)/莫来石基复合材料。在空气中在1000-1500℃下热处理后,百分之十的重量没有损失。由于莫来石基体的致密化,复合材料的孔隙率随热处理温度的升高而降低。该复合材料在热处理后也显示出假延性。通过提高热处理温度,可以稍微提高复合材料的强度。

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