航空制造技术
航空製造技術
항공제조기술
Aeronautical Manufacturing Technology
2015年
3期
79-82
,共4页
赵冰%侯红亮%李志强%廖金华%曲海涛
趙冰%侯紅亮%李誌彊%廖金華%麯海濤
조빙%후홍량%리지강%료금화%곡해도
SiC纤维%Ti3Al钛基复合材料%界面%力学性能
SiC纖維%Ti3Al鈦基複閤材料%界麵%力學性能
SiC섬유%Ti3Al태기복합재료%계면%역학성능
SiC ifber%Ti3Al Titanium matrix com-posites%Interface%Mechanical properties
采用箔—纤维—箔方法制备了连续SiC纤维增强Ti3Al基复合材料(SiCf/Ti3Al),测定了两种SiC纤维增强Ti3Al基复合材料的力学性能,分析了热处理工艺对复合材料力学性能的影响,讨论了复合材料在不同条件下的断裂机制。研究表明,国产SiC纤维(无碳涂层)增强Ti3Al复合材料的界面结合强度高于有碳涂层纤维增强的复合材料,力学性能却低于SCS-6纤维(有碳涂层)增强的复合材料。当热处理时间延长时, SCS-6/Ti3Al复合材料界面反应层厚度增加,复合材料的力学性能下降。
採用箔—纖維—箔方法製備瞭連續SiC纖維增彊Ti3Al基複閤材料(SiCf/Ti3Al),測定瞭兩種SiC纖維增彊Ti3Al基複閤材料的力學性能,分析瞭熱處理工藝對複閤材料力學性能的影響,討論瞭複閤材料在不同條件下的斷裂機製。研究錶明,國產SiC纖維(無碳塗層)增彊Ti3Al複閤材料的界麵結閤彊度高于有碳塗層纖維增彊的複閤材料,力學性能卻低于SCS-6纖維(有碳塗層)增彊的複閤材料。噹熱處理時間延長時, SCS-6/Ti3Al複閤材料界麵反應層厚度增加,複閤材料的力學性能下降。
채용박—섬유—박방법제비료련속SiC섬유증강Ti3Al기복합재료(SiCf/Ti3Al),측정료량충SiC섬유증강Ti3Al기복합재료적역학성능,분석료열처리공예대복합재료역학성능적영향,토론료복합재료재불동조건하적단렬궤제。연구표명,국산SiC섬유(무탄도층)증강Ti3Al복합재료적계면결합강도고우유탄도층섬유증강적복합재료,역학성능각저우SCS-6섬유(유탄도층)증강적복합재료。당열처리시간연장시, SCS-6/Ti3Al복합재료계면반응층후도증가,복합재료적역학성능하강。
The method of foil-fiber-foil(FFF) is adapted to fabricate the continuous SiC ifber reinforced Ti3Al composites(SiCf/Ti3Al), the mechanical properties of SiCf/Ti3Al are tested. Two kinds of SiC ifber reinforced Ti3Al composites are compared, and the inlfuence of heat treatment on the mechanical property is analyzed, the fracture mechanisms are discussed. It is noted that the interface force of ifber(without C coating made in china) reinforced Ti3Al composites is higher than that of SCS-6 ifber(with C coating) reinforced Ti3Al composites, the ultra strength of SCS-6/ Ti3Al is higher than that of domestic ifber reinforced Ti3Al composites. With increasing of heat treatment, the thickness of interfacial reactions of SCS-6/Ti3Al composites increases, the mechanical property drops.