共查询到20条相似文献,搜索用时 265 毫秒
1.
2.
国内评价高温下碳化硅质陶瓷膜材料的标准和方法较少,本文基于碳化硅陶瓷膜材料具体实际应用工况条件,就材料的强度,耐高温、高压性能,孔结构及透气性能等方面,提出了系列测试标准和方法,并进行了测试。实验测得山东工陶院生产的碳化硅质陶瓷膜材料的抗弯曲强度能够达到18MPa,支撑体气孔率和孔径分别为34%和60μm,分离膜平均孔径为17μm,材料的线胀系数在5×10-6/k,热震性能能够满足1000℃下10次不裂,在1m/min风速下材料的初始压降为750Pa。碳化硅陶瓷膜材料具有良好强度、高温热性能和较好的孔梯度结构。 相似文献
3.
4.
碳化硅纤维及其复合材料 总被引:9,自引:0,他引:9
赵稼祥 《高科技纤维与应用》2002,27(4):1-6,34
碳化硅纤维及其复合材料是目前使用温度最高的增强材料和先进复合材料,本文简要介绍先驱体转换法和化学气相沉积法制备碳化硅纤维的工艺,不同工艺方法制备的碳化硅纤维的性能比较,碳化硅纤维及其复合材料的现状与应用。 相似文献
5.
本文对自结合碳化硅及重结晶碳化硅进行了较详细的分析,澄清了人们的一些模糊认识。叙述了β—SiC结合碳化硅及重结晶碳化硅的生产工艺及基本性能。初步推测了提高重结晶碳化硅材料性能的途径。 相似文献
6.
分别采用固化剂D230、9035、acamine2636与环氧树脂E51混合,然后分别与用硅烷偶联剂(KH550、KH560、A171)处理的碳化硅颗粒混合,采用浇注法制备了碳化硅/环氧树脂复合材料。以材料的弯曲强度为评价方法,研究了3种不同固化剂构成的环氧树脂体系以及3种硅烷偶联剂对碳化硅/环氧树脂复合材料性能的影响,以及复合材料弯曲强度与材料中环氧树脂含量的关系。结果表明,3种固化剂中以D230、9035制备的材料性能为好;采用KH550、KH560处理碳化硅颗粒后的材料性能比不处理或采用A171处理碳化硅颗粒后的材料性能为好。随着复合材料中环氧树脂相含量的增加复合材料的弯曲强度下降。 相似文献
7.
8.
9.
碳化硅具有许多优良性能,但是碳化硅的断裂韧性不算太高。纤维增韧是改善材料韧性的最常用的一种方法。为此,有人研究了碳化硅短纤维增强碳化硅耐火材料的制备及其断裂性能。将碳化硅纤维切成长度为20mm的短纤维,按加入量(质量分数,下同)分别为0、0.1%、0.5%和1.0%加入到碳化硅 相似文献
10.
11.
通过对比不同温差热震后材料的残余强度 ,对反应烧结碳化硅材料的抗热震性能进行了研究。结果表明 :反应烧结碳化硅材料的抗热震性能与显微组织密切相关 ,低游离硅含量与小粒径的反应烧结碳化硅材料具有较好的抗热震断裂性能 ,而高游离硅含量或大碳化硅粒径的材料具有相对优异的抗热震损伤性。对反应烧结碳化硅材料的抗热震性与显微组织的关系进行了探讨。 相似文献
12.
氧氮化硅结合碳化硅制品的生产与使用 总被引:1,自引:1,他引:0
以工业用黑色碳化硅砂、硅粉为主要原料,研制出了导热性能优良、抗热震性好、耐高温、耐侵蚀及耐磨损,且生产工艺较简单、成本较低的氧氮化硅结合的碳化硅制品.该产品已广泛应用于冶金炉、化工设备及发电用锅炉的内衬,并取得了较满意的效果。 相似文献
13.
14.
15.
16.
Wei‐Ting Chen Ryan M. White Elizabeth C. Dickey 《Journal of the American Ceramic Society》2016,99(6):1837-1851
Borides and carbides generally have outstanding hardness, excellent wear resistance, and high melting points due to their covalent bonding. Directionally solidified eutectic (DSE) composites of boride and carbide constituent phases have been investigated since the 1970s as an approach to produce dense composite microstructures with added control over the microstructure. A variety of DSE ceramic composites have been developed and evaluated as potential materials for structural and functional applications due to their unique thermo‐electro‐mechanical properties. Renewed interest over the past few decades has been motivated, in part, by the needs for ultrahigh‐temperature composites for aerospace applications along with low‐density composites for armor applications. Some directionally solidified boride and carbide DSEs exhibit advantages in material properties over monolithic materials. This study reviews historical and recent research on processing methods, microstructure, crystallography, and material properties (mechanical, electrical, thermal properties, and oxidation resistance) of directionally solidified boride and carbide eutectic ceramic composites. Opportunities along with current limitations and needs for future developments are also reviewed and discussed. 相似文献
17.
JAMES J. GANGLER 《Journal of the American Ceramic Society》1950,33(12):367-374
An investigation of eight hot-pressed refractory oxides and carbides for possible gas-turbine application was undertaken. The properties, short-time tensile strength at elevated temperatures, thermal-shock resistance, coefficient of linear expansion, and density, were determined. The compositions of the ceramics included beryllium oxide, magnesium oxide, stabilized zirconia, zircon, boron carbide, 85% silicon carbide plus 15% boron carbide, titanium carbide, and zirconium carbide. The short-time tensile strengths of these ceramics were determined at 1800° and 2200°F. Resistance to thermal shock was determined by rapid cooling in air to room temperature from 1800°, 2000°, 2200°, and 2400°F. The thermal-expansion characteristics of these materials were studied from room temperature to 1100°F.
Zirconium carbide was the strongest material at 2200°F. with a maximum short-time tensile strength of 15,850 lb. per sq. in.; however, it exhibited extremely poor resistance to oxidation. Boron carbide had a short-time tensile strength of 22,550 lb. per sq. in. at 1800°F., and was the strongest material at this temperature. Boron carbide also had very poor resistance to oxidation and was among the worst compositions investigated in its ability to resist fracture by thermal shock. The evaluation of strength of boron carbide at 2200°F. was unsuccessful because it fluxed with the grips. Titanium carbide had the best resistance to thermal shock, and had strengths of 15,850 lb. per sq. in. at 1800°F. and 9400 lb. per sq. in. at 2200°F. It was the most promising of the eight compositions investigated. Hot-pressing of these eight highly refractory bodies indicated that a density of at least 93% of theoretical density could be obtained by this fabrication method. 相似文献
Zirconium carbide was the strongest material at 2200°F. with a maximum short-time tensile strength of 15,850 lb. per sq. in.; however, it exhibited extremely poor resistance to oxidation. Boron carbide had a short-time tensile strength of 22,550 lb. per sq. in. at 1800°F., and was the strongest material at this temperature. Boron carbide also had very poor resistance to oxidation and was among the worst compositions investigated in its ability to resist fracture by thermal shock. The evaluation of strength of boron carbide at 2200°F. was unsuccessful because it fluxed with the grips. Titanium carbide had the best resistance to thermal shock, and had strengths of 15,850 lb. per sq. in. at 1800°F. and 9400 lb. per sq. in. at 2200°F. It was the most promising of the eight compositions investigated. Hot-pressing of these eight highly refractory bodies indicated that a density of at least 93% of theoretical density could be obtained by this fabrication method. 相似文献
18.
等离子喷涂工艺参数对B4C涂层性能的影响 总被引:2,自引:0,他引:2
本文研究了喷涂距离对大气等离子喷涂B4C涂层的沉积效率、气孔率、显微硬度和抗热震性能的影响,发现喷涂距离会严重影响B4C粉末在等离子体射流中的熔融状态,从而对这些性能产生显著影响。实验结果表明,通过优化工艺参数,尤其是选择适当的喷涂距离,可以在大气呀涂条件下制得同高压等离子喷涂相近所孔率和显微硬度的B4C涂层。 相似文献
19.
20.
Polyimide (PI) aerogels enable promising application in many fields but are always inhibited by their weak resistance to high temperature and low mechanical properties. Herein, novel PI aerogel composites with efficient heat insulation and high compressive performance are prepared by introducing Silicon carbide whiskers (SiCw) as reinforcement. The SiCw in aerogel function as shrinkage inhibitor and high temperature stabilizer. The addition of SiCw exhibits obvious enhancement and toughening effect, the compressive strength of the PI aerogel composites increases from 1.09 to 1.96 MPa. These PI aerogel composites also show enhanced high temperature stability. The as-prepared PI aerogel composites possess integrated properties of high-temperature resistance, low thermal conductivity, and high compressive strength, which can be the candidate for the application in aerospace. 相似文献