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Fabrication Of ZrO2 Modified C/SiC Composites Via Precursor Infiltration Pyrolysis Method And Properties Investigation

Posted on:2012-09-24Degree:MasterType:Thesis
Country:ChinaCandidate:S X WangFull Text:PDF
GTID:2211330362960210Subject:Materials Science and Engineering
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Carbon fibre reinforced silicon carbide(C/SiC) composites is a new type of high temperature structural material with the potential application in the aeronautic, astronautic and military fields.However,C/SiC cannot be long-term utilized above 1650℃and properties are obviously declined above 1700℃due to the shortage of high temperature endurance and oxidation resistance. In this dissertation, ZrO2 modified C/SiC composites were designed and fabricated by precursor infiltration pyrolysis (PIP) method. Systematic investigation were studied of the induction route of ZrO2, oxidation and ablation behavior of matrix modified by ZrO2,and the effect of content of ZrO2 on the properties of C/SiC composites.Firstly, this paper focused on the choice of precursor on candidation of zirconium-2,4-pentanedionate(Zr(AcAc)4), zirconium n-butoxide(Zr(OBu)4) and zirconium n-propoxide(Zr(OPr)4) as organical precursor, ZrOCl2?8H2O as inorganical precursor. The result revealed that the organical precursor can dissolve into PCS and divinylbenzene(DVB) mixture, and Zr(OBu)4 is the most suitable precursor with the proportion of PCS:DVB:Zr(OBu)4=2:1:2 of which the yield is 43.93%. ZrOCl2?8H2O can be utilized as precursor due to high solubility in methanol and good infiltration in SiC ceramics and C/SiC composites and the yield is 12.3%.For the purpose of investigating the effect of ZrO2 additional to properties of matrix, ZrO2 modified SiC ceramics were prepared. ZrO2 existed in the form of thin grains among SiC blocks.With increasing content of ZrO2, the porosity increased consistently, the porosity of ceremics with 29wt% ZrO2 was 23.6% and density was 2.16g/cm3. Infiltration with pressure can decrease the porosity. Ceramics prepared by this method of which ZrO2 content was 14.3wt% had porosity 23.6%, and density 2.31g/cm3. After oxidation at 1700℃, with the content of ZrO2 increasing, weight loss increased and retention of flexural strength decreased. Compared to ceremics with 7wt% ZrO2, weight retention of ceremics with 29wt% ZrO2 decreased from 59.16% to 36.84%. Oxidation behavior of ZrO2 modified SiCceramics may be divided into three steps according to the temperature gradient. Firstly, oxidation of free C and passive oxidation of SiC forming SiO2 happened at 800℃to 1500℃. Secondly, according to the temperature rising and pressure of O2 decreasing, active oxidation of SiC gradually became dominant which formed SiO gas at 1500℃to 1600℃. Then, above 1600℃, carbo-thermal reaction began and pyrolysis of PCS continued with gas forming, which caused the protective SiO2 destroyed and the inner region of the ceramics was oxided. The ablation rate decreased with content of ZrO2. when ZrO2 increased from 7wt% to 29wt%, the mass loss rate changed from 0.0367g/s to 0.0195g/s, and the linear recession rate changed from cracked to 0361mm/s. After ablation, proportion of ZrO2 decreased from the ablation center to edge, ZrO2 existed mostly at the ablation center and SiO2 at the edge.ZrO2 modified C/SiC composites were fabricated on base of the ceramics, and the structure and properties were investigated, the mechanisms of oxidation and ablation were also researched. The result showed that, C fibers were efficiently protected by ways of infiltrating PCS/Xylene at the former cycles.Flexual strength was obviously improved, flexural strength of composites with 25wt% ZrO2 was 216MPa and the one without protection was only 103MPa. Infiltration with pressure can make up this limitation. Composites fabricated with pressure had ZrO2 content 9.0wt%, porosity 4.78% and flexural strength 292MPa. The intrinsically resistant to oxidation of ZrO2 emerged at 1700℃, which improved the oxidation resistance of whole material. Composites with ZrO2 61wt%,25wt% and 16wt% had weight loss of 29.98%, 34.71% and 35.07%. Compared to C/SiC composites(0.0223g/s and 0.0602mm/s), the mass loss rate and linear recession rate of 61wt% ZrO2 composites was 0.0161g/s and 0.0185mm/s.
Keywords/Search Tags:ultra high temperature, C/SiC composite, precursor infiltration and pyrolysis(PIP), ZrO2, Zirconium n-butoxide, ZrOCl2?8H2O
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