航空制造技术
航空製造技術
항공제조기술
AERONAUTICAL MANUFACTURING TECHNOLOGY
2014年
6期
119-121,128
,共4页
焦春荣%王岭%陈大明%焦健
焦春榮%王嶺%陳大明%焦健
초춘영%왕령%진대명%초건
凝胶固相反应法%BSAS%环境障涂层抗氧化性能
凝膠固相反應法%BSAS%環境障塗層抗氧化性能
응효고상반응법%BSAS%배경장도층항양화성능
Gel-solid reaction method%BSAS%Environmental barrier coatings (EBC) Oxidation re-sistance
采用凝胶固相反应法制备SiC陶瓷基复合材料EBC涂层用Ba0.75Sr0.25Al2Si2O8粉体,并以SiC陶瓷片为基体材料初步评价了BSAS涂层的抗氧化能力。通过DSC/TG确定了凝胶前驱体的热分解情况;利用XRD、SEM、粒度和热膨胀系数的测定对合成粉体进行了表征;对该粉体的抗氧化性能进行了初步评价。结果表明,1200℃下成功制备颗粒中位径3.9μm、分散均匀的BSAS粉体;粉体室温至1200℃的热膨胀系数为5.02×10-6 K-1,与SiC陶瓷有很好的热胀匹配;该涂层可在1300℃、大气环境下保持均匀无开裂,与基体结合紧密,可以基本满足现阶段国内航空用SiC陶瓷基复合材料抗氧化的要求。
採用凝膠固相反應法製備SiC陶瓷基複閤材料EBC塗層用Ba0.75Sr0.25Al2Si2O8粉體,併以SiC陶瓷片為基體材料初步評價瞭BSAS塗層的抗氧化能力。通過DSC/TG確定瞭凝膠前驅體的熱分解情況;利用XRD、SEM、粒度和熱膨脹繫數的測定對閤成粉體進行瞭錶徵;對該粉體的抗氧化性能進行瞭初步評價。結果錶明,1200℃下成功製備顆粒中位徑3.9μm、分散均勻的BSAS粉體;粉體室溫至1200℃的熱膨脹繫數為5.02×10-6 K-1,與SiC陶瓷有很好的熱脹匹配;該塗層可在1300℃、大氣環境下保持均勻無開裂,與基體結閤緊密,可以基本滿足現階段國內航空用SiC陶瓷基複閤材料抗氧化的要求。
채용응효고상반응법제비SiC도자기복합재료EBC도층용Ba0.75Sr0.25Al2Si2O8분체,병이SiC도자편위기체재료초보평개료BSAS도층적항양화능력。통과DSC/TG학정료응효전구체적열분해정황;이용XRD、SEM、립도화열팽창계수적측정대합성분체진행료표정;대해분체적항양화성능진행료초보평개。결과표명,1200℃하성공제비과립중위경3.9μm、분산균균적BSAS분체;분체실온지1200℃적열팽창계수위5.02×10-6 K-1,여SiC도자유흔호적열창필배;해도층가재1300℃、대기배경하보지균균무개렬,여기체결합긴밀,가이기본만족현계단국내항공용SiC도자기복합재료항양화적요구。
In this paper, barium strontium alu-minum silicate powders, used for environmental barrier coatings on SiC ceramic matrix composites, are prepared by the gel-solid reaction method. DSC/TG thermodynam-ics is used to analyze the thermal decomposition of the precursor. The XRD, SEM, the particle size distribution and the thermal expansion of the BSAS powders are inves-tigated, and its oxidation resistance is evaluated primarily. The results show that uniformly dispersed BSAS powders with a diameter of 3.9μm can be prepared at the tempera-ture of 1200℃;the thermal expansion of the BSAS pow-ders is determined as 5.02×10-6 K-1 from room temperature to 1200℃, which matches with the thermal expansion of SiC ceramics very well;the coating will maitain uniform and no-cracking till 1300℃in air, and it combines with the substrate closely. The coating materials meet with the oxi-dation resistance requirements of the SiC ceramic matrix composites for current domestic aeronautic application.