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SiC_(f)/SiC复合材料表面Si/Yb_(2)Si_(2)O_(7)涂层1350℃抗热冲击和抗热冲刷性能研究
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作者 陈易诚 邓杨芳 +3 位作者 张乐 韦林 李其连 周国栋 《材料保护》 CAS CSCD 2024年第8期58-64,104,共8页
为了研究Si/Yb_(2)Si_(2)O_(7)涂层在1350℃条件下的抗热冲击和抗热冲刷性能,首先在SiC_(f)/SiC复合材料上采用真空等离子喷涂技术制备了Si/Yb_(2)Si_(2)O_(7)涂层,并采用金相、物相、SEM、EDS、燃气热冲击设备和燃气热冲刷设备对试样... 为了研究Si/Yb_(2)Si_(2)O_(7)涂层在1350℃条件下的抗热冲击和抗热冲刷性能,首先在SiC_(f)/SiC复合材料上采用真空等离子喷涂技术制备了Si/Yb_(2)Si_(2)O_(7)涂层,并采用金相、物相、SEM、EDS、燃气热冲击设备和燃气热冲刷设备对试样进行了结构及性能表征。结果表明:涂层与SiC_(f)/SiC复合材料的结合强度为25.01 MPa。经过1350℃燃气热冲击1000次,1350℃、550 m/s燃气热冲刷1 h后,Yb_(2)Si_(2)O_(7)涂层的表面物相均主要为Yb_(2)Si_(2)O_(7)、Yb_(2)SiO_(5)、Yb_(2)O_(3)和SiO_(2),抗热冲击和抗热冲刷2项性能测试结果均达设计要求。涂层结合强度很高,复合材料、Si层和Yb_(2)Si_(2)O_(7)层耐高温且热匹配性能较好,且面层的抗燃气腐蚀能力很强,是涂层热冲击、热冲刷性能良好的主要原因。燃气热冲刷的燃气燃烧时间比燃气热冲击的总时间短,且热冲刷为恒温连续冲刷,无冷热的剧烈交替变化,故燃气冲刷后涂层边缘处靠近工装装卡的地方未见明显开裂,且连续冲刷后的黑色烧蚀区域较燃气热冲击的面积小。 展开更多
关键词 sicf/sic复合材料 si/yb_(2)si_(2)o_(7)涂层 真空等离子喷涂 抗热冲击 抗热冲刷
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大气等离子喷涂Si/Mullite+BSAS/Yb_(2)Si_(2)O_(7)环境障涂层的制备与水氧腐蚀行为
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作者 崔永静 郭孟秋 +4 位作者 马玉洁 周邦阳 范尚武 焦健 成来飞 《航空材料学报》 CAS CSCD 北大核心 2024年第4期37-45,共9页
以固相烧结法制备的Yb_(2)Si_(2)O_(7)粉体作为原材料,采用大气等离子喷涂工艺在SiC基体表面制备Si/Mullite+BSAS/Yb_(2)Si_(2)O_(7)三层结构环境障涂层。利用扫描电子显微镜、能谱仪、X射线衍射分析仪、纳米压痕试验机等设备研究涂层... 以固相烧结法制备的Yb_(2)Si_(2)O_(7)粉体作为原材料,采用大气等离子喷涂工艺在SiC基体表面制备Si/Mullite+BSAS/Yb_(2)Si_(2)O_(7)三层结构环境障涂层。利用扫描电子显微镜、能谱仪、X射线衍射分析仪、纳米压痕试验机等设备研究涂层的显微组织、相结构和力学性能。结果表明:粉体材料由83%Yb_(2)Si_(2)O_(7)相和17%Yb_(2)SiO_(5)相(质量分数)组成,等离子喷涂获得的Yb_(2)Si_(2)O_(7)层孔隙率为(6.61±0.65)%,涂层结合强度达(22.82±3.55)MPa,涂层断裂韧度达(1.98±0.12)MPa·m1/2。此外,涂层1350℃条件下水氧耦合腐蚀测试结果显示Yb_(2)Si_(2)O_(7)单斜相含量先降低后提高,硅黏结层高温氧化形成的热生长氧化物SiO_(2)与Mullite+BSAS界面相容,未发现Mullite+BSAS与Yb_(2)Si_(2)O_(7)层互扩散现象,硅层的损耗是涂层使用寿命的主要限制环节。 展开更多
关键词 环境障涂层 等离子喷涂 碳化硅陶瓷基复合材料 yb_(2)si_(2)o_(7)
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SiC_(f)/SiC复合材料表面Si/Yb_(2)Si_(2)O_(7)双层涂层结合强度分析 被引量:3
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作者 张乐 张艺馨 +5 位作者 牛亚然 李其连 邓杨芳 周海滨 姚远 罗文东 《表面技术》 EI CAS CSCD 北大核心 2022年第3期199-207,共9页
目的 通过选择合适的复合材料拉伸方向和涂层制备工艺,在SiC_(f)/SiC复材上获得高结合强度的Si/Yb_(2)Si_(2)O_(7)双层涂层。方法 采用真空等离子喷涂技术在2.5D编织的SiC_(f)/SiC复合材料表面制备Si涂层、Si/Yb_(2)Si_(2)O_(7)双层涂... 目的 通过选择合适的复合材料拉伸方向和涂层制备工艺,在SiC_(f)/SiC复材上获得高结合强度的Si/Yb_(2)Si_(2)O_(7)双层涂层。方法 采用真空等离子喷涂技术在2.5D编织的SiC_(f)/SiC复合材料表面制备Si涂层、Si/Yb_(2)Si_(2)O_(7)双层涂层。采用金相、XRD、SEM和EDS对试样进行表征,采用拉伸试验测试涂层的结合强度,观察涂层拉伸后的断裂面形貌,分析涂层结合强度的影响因素。结果 采用胶粘拉拔法,2.5D编织的SiC_(f)/SiC复合材料拉伸后的强度值为(32.41±3.52) MPa,Si涂层和Yb_(2)Si_(2)O_(7)涂层的孔隙率分别为2.3%和5.2%,Si涂层与SiC_(f)/SiC复合材料的结合强度为(30.48±4.43)MPa,Si/Yb_(2)Si_(2)O_(7)双层涂层与SiCf/SiC复合材料的结合强度为(26.23±3.13)MPa。Si涂层在拉伸过程中,部分Si层、SiC_(f)/SiC复合材料表面纬向SiC纤维、SiC基体和粘接胶都发生了断裂。Si/Yb_(2)Si_(2)O_(7)双层涂层在拉伸过程中,大量Si层、复合材料表面纬向SiC纤维和SiC基体以及少量Yb_(2)Si_(2)O_(7)层被拉开。结论 Si/Yb_(2)Si_(2)O_(7)双层涂层与SiC_(f)/SiC复合材料结合强度较高的主要原因是SiC_(f)/SiC复合材料沿拉伸方向强度较高,Si涂层与复合材料结合强度高。真空等离子喷涂技术有利于减少涂层微观缺陷。Yb_(2)Si_(2)O_(7)的热膨胀系数与Si、SiC_(f)/SiC相近。Si涂层与Yb_(2)Si_(2)O_(7)涂层化学相容性好。 展开更多
关键词 sic_(f)/sic si/yb_(2)si_(2)o_(7)双层涂层 真空等离子喷涂 环境障涂层 结合强度
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掺杂SiC晶须的Yb_(2)Si_(2)O_(7)环境障涂层的制备及性能
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作者 王佳宁 王超会 +4 位作者 荣芷艺 刘慧男 刘佳琪 朱忠宇 王宇航 《高师理科学刊》 2022年第7期61-65,共5页
以SiC晶须作为增强相,增加Yb_(2)Si_(2)O_(7)环境障涂层(EBC)的使用寿命.采用喷雾造粒和真空煅烧法制备改性和未改性纳米结构粉体,利用大气等离子喷涂的方法制备了掺杂SiC晶须的Yb_(2)Si_(2)O_(7)涂层和未改性涂层,采用XRD,SEM等表征方... 以SiC晶须作为增强相,增加Yb_(2)Si_(2)O_(7)环境障涂层(EBC)的使用寿命.采用喷雾造粒和真空煅烧法制备改性和未改性纳米结构粉体,利用大气等离子喷涂的方法制备了掺杂SiC晶须的Yb_(2)Si_(2)O_(7)涂层和未改性涂层,采用XRD,SEM等表征方法对粉体及涂层的形貌、相组成和抗热震性能进行了分析.结果表明,掺杂晶须的Yb_(2)Si_(2)O_(7)涂层的抗热震性优于未改性涂层,涂层中存在晶须增韧的迹象,表明SiC晶须在一定程度上能有效提高涂层的使用寿命. 展开更多
关键词 yb_(2)si_(2)o_(7) sic晶须 环境障涂层 抗热震性
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Y_(2)O_(3)改性SiC陶瓷高温水氧行为研究 被引量:1
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作者 张俊敏 陈小武 +6 位作者 杨金山 张翔宇 阚艳梅 廖春景 胡建宝 周海军 董绍明 《中国材料进展》 CAS CSCD 北大核心 2023年第6期456-463,共8页
连续碳化硅纤维增强碳化硅陶瓷基复合材料(SiCf/SiC)因高温水氧侵蚀致使力学性能急剧下降,限制了其热端部件在航空发动机中的长寿命服役。研究证实,该侵蚀主要表现为SiC基体和纤维与水、氧气反应生成气相Si(OH)_(4),导致质量耗散。因此... 连续碳化硅纤维增强碳化硅陶瓷基复合材料(SiCf/SiC)因高温水氧侵蚀致使力学性能急剧下降,限制了其热端部件在航空发动机中的长寿命服役。研究证实,该侵蚀主要表现为SiC基体和纤维与水、氧气反应生成气相Si(OH)_(4),导致质量耗散。因此,从组分、结构调控角度提升SiC耐水氧侵蚀性能已成为研究热点。对比研究了添加和未添加Y_(2)O_(3)对SiC陶瓷水氧侵蚀行为的影响。与SiC陶瓷相比,SiC-Y_(2)O_(3)陶瓷的氧化速率及挥发速率均明显下降,且随着氧化温度的升高,两者差距愈发明显,可见添加Y_(2)O_(3)后SiC陶瓷的耐水氧侵蚀性能得到明显改善。氧化后的陶瓷微观结构表明,SiC-Y_(2)O_(3)陶瓷氧化层明显更薄且更致密,进一步分析表明这主要由Y组分在陶瓷表面的迁移以及聚集所致。在侵蚀过程中,陶瓷内部的Y_(2)O_(3)会向SiC陶瓷表面迁移,并与SiO_(2)反应形成β-Y_(2)Si_(2)O_(7),并逐渐聚集形成连续的Y_(2)Si_(2)O_(7)层。因此,在氧化层与SiC陶瓷交界处形成了一个富Y_(2)Si_(2)O_(7)/富Y_(2)O_(3)层。多层含Y氧化层在陶瓷表面形成水氧阻挡屏障,有效抑制了水氧介质向陶瓷内部的渗透与侵蚀。该研究结果为SiC_(f)/SiC复合材料的耐水氧结构设计与调控提供了重要思路。 展开更多
关键词 sic陶瓷 高温水氧环境 水氧行为 耐水氧侵蚀机理 连续Y_(2)si_(2)o_(7)层
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Si/(Yb_(1-x)Y_(x))_(2)Si_(2)O_(7)/LaMgAl_(11)O_(19)热/环境障涂层的高温性能研究
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作者 毛传勇 董淑娟 +2 位作者 蒋佳宁 邓龙辉 曹学强 《硅酸盐通报》 CAS 北大核心 2022年第7期2564-2573,共10页
采用等离子喷涂法在碳化硅纤维增强碳化硅陶瓷基复合材料(SiC_(f)/SiC-CMCs)表面制备了Si/(Yb_(1-x)Y_(x))_(2)Si_(2)O_(7)/LaMgAl_(11)O_(19)(x=0、0.5)热/环境障涂层(T/EBCs)体系。通过SEM、EDS和XRD等测试方法研究了不同组成的T/EBC... 采用等离子喷涂法在碳化硅纤维增强碳化硅陶瓷基复合材料(SiC_(f)/SiC-CMCs)表面制备了Si/(Yb_(1-x)Y_(x))_(2)Si_(2)O_(7)/LaMgAl_(11)O_(19)(x=0、0.5)热/环境障涂层(T/EBCs)体系。通过SEM、EDS和XRD等测试方法研究了不同组成的T/EBCs体系在1300℃下的热循环性能和抗水氧腐蚀性能,进而探讨了热循环失效和水氧腐蚀失效机理。结果表明,在T/EBCs体系中,Si/Yb_(2)Si_(2)O_(7)/LMA涂层体系的热循环寿命为403次,抗水氧腐蚀性能为50 h,Si/YbYSi_(2)O_(7)/LMA体系的热循环寿命降低至277次,而水氧腐蚀性能提高至80 h。YbYSi_(2)O_(7)与LMA之间较大的热失配应力以及层间含Al化合物或固溶体的生成是Si/YbYSi_(2)O_(7)/LMA热循环寿命降低的主要原因;YbYSi_(2)O_(7)-EBCs层较少的杂质氧化物减少了与水反应生成挥发性物质的几率,提高了Si/YbYSi_(2)O_(7)/LMA的抗水氧腐蚀能力。 展开更多
关键词 sic_(f)/sic-CMCs 热/环境障涂层 热障涂层 环境障涂层 热循环 高温水氧腐蚀 yb_(2)si_(2)o_(7) ybYsi_(2)o_(7)
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Yb_(2)Si_(2)O_(7)前驱体及其低压等离子喷涂用粉末制备研究
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作者 颜正 彭浩然 +1 位作者 冀晓鹃 章德铭 《热喷涂技术》 2022年第3期38-45,22,共9页
本文分别采用固相反应法和溶胶凝胶法制备Yb_(2)Si_(2)O_(7)前驱体粉末和陶瓷块材。采用固相法时,混合粉末经1500℃,5 h煅烧后由Yb_(2)Si_(2)O_(7)和Yb_(2)SiO_(5)两相构成,经冷压、1600℃,10 h煅烧后得到疏松块材,内部残留大量未完全... 本文分别采用固相反应法和溶胶凝胶法制备Yb_(2)Si_(2)O_(7)前驱体粉末和陶瓷块材。采用固相法时,混合粉末经1500℃,5 h煅烧后由Yb_(2)Si_(2)O_(7)和Yb_(2)SiO_(5)两相构成,经冷压、1600℃,10 h煅烧后得到疏松块材,内部残留大量未完全反应的氧化硅和中间相Yb_(2)SiO_(5)。采用溶胶凝胶法时,退火态干凝胶经1400℃,5 h煅烧后即可获得高纯Yb_(2)Si_(2)O_(7)粉末,经冷压、1600℃,10 h煅烧后,得到近Yb_(2)Si_(2)O_(7)纯相的、更完整致密块材。这些表明相较于固相反应法,溶胶凝胶法制备Yb_(2)Si_(2)O_(7)具有反应门槛较低、易制得高纯均匀材料的优势。进一步,采用二流体雾化工艺制备低压等离子喷涂用粉末,重点探索了PVA含量和雾化压力对粉末的影响规律。结果表明,PVA含量决定粉末形貌,当PVA含量适中时(10 wt.%)可获得球形度良好的实心粉末,雾化压力决定粉末粒度,雾化压力越大,粉末粒径越细,当雾化压力为1.2 MPa时,可获得所需的1~30μm超细粉末。 展开更多
关键词 环境障涂层 yb_(2)si_(2)o_(7) 固相反应法 溶胶凝胶法 二流体雾化造粒
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Water vapor corrosion behavior and failure mechanism of air sprayed bi-layer Yb_(2)Si_(2)O_(7)/SiC and tri-layer Yb_(2)Si_(2)O_(7)/(SiCw-Mullite)/SiC environmental barrier coating
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作者 Pengju Chen Peng Xiao +3 位作者 Zhuan Li Yichen Wang Xian Tang Yang Li 《Advanced Powder Materials》 2023年第1期15-24,共10页
To improve the corrosion resistance of Cf/SiC composites in a water vapor oxygen coupled environment,the bilayer Yb_(2)Si_(2)O_(7)/SiC and tri-layer Yb2Si2O7/(SiCw-Mullite,SM)/SiC environment barrier coatings were de... To improve the corrosion resistance of Cf/SiC composites in a water vapor oxygen coupled environment,the bilayer Yb_(2)Si_(2)O_(7)/SiC and tri-layer Yb2Si2O7/(SiCw-Mullite,SM)/SiC environment barrier coatings were designed and prepared on the surface of Cf/SiC composites by chemical vapor deposition and sol-gel method united with air spraying.Results show that the mass loss of bi-layer Yb_(2)Si_(2)O_(7)/SiC coating coated samples was 17.24×10^(-3) g cm^(-2) after 200 h oxidation at 1673 K,and the average compression strength retention rate was only 79.44% due to the formation of wide penetrating cracks.Comparatively,SiC whiskers in SM middle coating can not only increase the crack propagation resistance of mullite middle coating,but also alleviate the difference of coefficient of thermal expansion between Yb_(2)Si_(2)O_(7) outer coating and mullite middle coating.Therefore,the mass loss of trilayer Yb_(2)Si_(2)O_(7)/SM/SiC coating coated samples was only 2.93×10^(-3) g cm^(-2) after 200 h oxidation at 1673 K,and the average compression strength retention rate was up to 98.79%. 展开更多
关键词 yb_(2)si_(2)o_(7)/sm/sic EBCs Water Corrosion Mechanism
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(Lu_(1/7)Yb_(1/7)Sc_(1/7)Er_(1/7)Y_(1/7)Ho_(1/7)Dy_(1/7))_(2)Si_(2)O_(7)high entropy rare-earth disilicate with low thermal conductivity and excellent resistance to CMAS corrosion
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作者 Xu Wang Mingyu Meng +4 位作者 Feihan Xu Ling Liu Lihong Gao Shizhen Zhu Zhuang Ma 《Journal of Advanced Ceramics》 SCIE EI CAS CSCD 2024年第5期549-560,共12页
Low thermal conductivity,compatible thermal expansion coefficient,and good calcium–magnesium–aluminosilicate(CMAS)corrosion resistance are critical requirements for environmental barrier coatings used on silicon-bas... Low thermal conductivity,compatible thermal expansion coefficient,and good calcium–magnesium–aluminosilicate(CMAS)corrosion resistance are critical requirements for environmental barrier coatings used on silicon-based ceramics.RE2Si2O7(RE=rare earth)has been widely recognized as one of the most promising candidates for environmental barrier coatings due to its good water vapor corrosion resistance.However,the relatively high thermal conductivity and poor resistance to CMAS corrosion have limited its practical application.Inspired by the high entropy effect,in this work,a novel rare earth disilicate(Lu_(_(1/7))Yb_(_(1/7))Sc_(_(1/7))Er_(_(1/7))Y_(_(1/7))Ho_(_(1/7))Dy_(_(1/7)))2Si2O7((7RE_(_(1/7)))2Si2O7)has been designed and synthesized by a solid reaction process.(7RE_(_(1/7)))2Si2O7 showed a low thermal conductivity of 1.81 W·m^(−1)·K^(−1)at 1273 K.Furthermore,the thermal expansion coefficient of(7RE_(_(1/7)))_(2)Si_(2)O_(7)(4.07×10^(−6)℃^(−1)from room temperature(RT)to 1400℃)is close to that of the SiC-based ceramic matrix composites(SiC-CMCs)((4.5–5.5)×10^(−6)℃^(−1)).Additionally,(7RE_(_(1/7)))2Si2O7 exhibited excellent resistance to CMAS corrosion.When exposed to CMAS at 1300℃for 48 h,the reaction layer thickness was 22μm.The improved performance of(7RE_(_(1/7)))2Si2O7 highlights its potential as a promising candidate for thermal/environmental barrier coatings. 展开更多
关键词 high entropy disilicate (Lu_(1/7)yb_(1/7)Sc_(1/7)Er_(1/7)Y_(1/7)Ho_(1/7)Dy_(1/7))_(2)si_(2)o_(7)((7RE_(1/7))_(2)si_(2)o_(7)) high-temperature thermal properties calcium-magnesium-aluminosilicate(CMAS)corrosion
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Corrosion behavior and failure mechanism of SiC whisker and c-AlPO_(4) particle-modified novel tri-layer Yb_(2)Si_(2)O_(7)/mullite/SiC coating in burner rig tests 被引量:3
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作者 Pengju CHEN Peng XIAO +1 位作者 Xian TANG Yang LI 《Journal of Advanced Ceramics》 SCIE EI CAS CSCD 2022年第12期1901-1917,共17页
The corrosion behavior of environmental barrier coatings(EBCs)directly affects the service life and stability of ceramic matrix composite(CMC)structural parts in the aero-engines.The silicon carbide(SiC)whisker toughe... The corrosion behavior of environmental barrier coatings(EBCs)directly affects the service life and stability of ceramic matrix composite(CMC)structural parts in the aero-engines.The silicon carbide(SiC)whisker toughening phase and c-AlPO_(4) bonding phase are firstly used to improve the service life of novel tri-layer Yb_(2)Si_(2)O_(7)/mullite/SiC EBCs in the burner rig test.The formation of penetrating cracks in Yb_(2)Si_(2)O_(7)/mullite/SiC coating caused the failure of coating at 1673 K.The SiC whiskers in mullite middle coating significantly inhibited the formation of penetrating cracks in Yb_(2)Si_(2)O_(7)/mullite/SiC coating,and efficiently prevented the oxidation of carbon fiber reinforced silicon carbide(C_(f)/SiC)samples for 360-min thermal cycles(24 times)with a weight loss of 6.19×10^(−3) g·cm^(−2).Although c-AlPO_(4) particles further improved the service life of SiC_(w)-mullite(SM)coating,the overflow of PO_(x) gas aggravated the formation and expansion of cracks in the Yb_(2)Si_(2)O_(7) outer coating,and caused the service life of overall Yb_(2)Si_(2)O_(7)/c-AlPO_(4)-SiC_(w)-mullite(ASM)/SiC coating to be slightly lower than that of Yb_(2)Si_(2)O_(7)/SM/SiC coating.This study guides the design of modified tri-layer EBCs with long service life in high-temperature and high-speed gas environment. 展开更多
关键词 yb_(2)si_(2)o_(7) MULLITE tri-layer sol-gel burner rig test
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Microstructure and mechanical properties of h-BN/Yb_4Si_2O_7N_2 composites 被引量:1
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作者 Juanjuan CHEN Jixin CHEN +2 位作者 Hao ZHANG Minmin HU Meishuan LI 《Journal of Advanced Ceramics》 SCIE CSCD 2018年第4期317-324,共8页
A series of h-BN based composites with Yb_4Si_2O_7N_2 as a secondary phase were successfully synthesized by an in situ reaction hot pressing method. It was found that the relative density and room-temperature mechanic... A series of h-BN based composites with Yb_4Si_2O_7N_2 as a secondary phase were successfully synthesized by an in situ reaction hot pressing method. It was found that the relative density and room-temperature mechanical properties monotonically increased with increasing the content of Yb_4Si_2O_7N_2 from 20 to 50 vol%. When 50 vol% Yb_4Si_2O_7N_2 was introduced, the relative density of the composite reached 98.75%, and its flexural strength, compressive strength, fracture toughness, and hardness reached 338±10 MPa, 803±49 MPa, 2.06±0.06 MPa·m1/2, and 2.69±0.10 GPa, respectively. The strengthening effect of Yb_4Si_2O_7N_2 was mainly attributed to its high modulus and high hardness. Fine microstructure was also advantageous to strength and could lead to more tortuous crack propagation paths and then improve the fracture toughness of the composites simultaneously. Meanwhile, the composites maintained good machinability. 展开更多
关键词 h-BN/yb_4si_2o_7N_2 composites MICRoSTRUCTURE mechanical properties MACHINABILITY
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