宇航材料工艺
宇航材料工藝
우항재료공예
AEROSPACE MATERIALS & TECHNOLOGY
2001年
2期
48-55
,共8页
张绪虎%胡欣华%关盛勇%汪翔%杨盛良
張緒虎%鬍訢華%關盛勇%汪翔%楊盛良
장서호%호흔화%관성용%왕상%양성량
热暴露%B/Al%力学性能%界面
熱暴露%B/Al%力學性能%界麵
열폭로%B/Al%역학성능%계면
对经300℃、500℃高温热暴露的B/Al(LF6)复合材料的力学性能进行了研究,实验结果表明材料在300℃下热暴露时,性能下降速度较慢,100h后强度保留率约为76%,延伸率保留率为74%。而在500℃下热暴露时,5 h以上强度就有明显降低。高温长时间热暴露后复合材料的断裂也从累积型转变为典型的非累积型断裂。通过透射电镜(TEM)及扫描电镜(SEM)对固态热压制造态和高温热暴露的界面状况进行了分析,认为界面反应是造成B/Al复合材料力学性能下降的主要原因。
對經300℃、500℃高溫熱暴露的B/Al(LF6)複閤材料的力學性能進行瞭研究,實驗結果錶明材料在300℃下熱暴露時,性能下降速度較慢,100h後彊度保留率約為76%,延伸率保留率為74%。而在500℃下熱暴露時,5 h以上彊度就有明顯降低。高溫長時間熱暴露後複閤材料的斷裂也從纍積型轉變為典型的非纍積型斷裂。通過透射電鏡(TEM)及掃描電鏡(SEM)對固態熱壓製造態和高溫熱暴露的界麵狀況進行瞭分析,認為界麵反應是造成B/Al複閤材料力學性能下降的主要原因。
대경300℃、500℃고온열폭로적B/Al(LF6)복합재료적역학성능진행료연구,실험결과표명재료재300℃하열폭로시,성능하강속도교만,100h후강도보류솔약위76%,연신솔보류솔위74%。이재500℃하열폭로시,5 h이상강도취유명현강저。고온장시간열폭로후복합재료적단렬야종루적형전변위전형적비루적형단렬。통과투사전경(TEM)급소묘전경(SEM)대고태열압제조태화고온열폭로적계면상황진행료분석,인위계면반응시조성B/Al복합재료역학성능하강적주요원인。
Mechanical properties of the B/A1 composites exposed in hot air up to 300℃C,.500$ are investigated.Experimental results show that thermal treatment at 300℃ may result in less decrease with tensile strength remained about 72% ,and ultimate strain remained 74% after 100 h ,for example ,but thermal treatment at 500℃ only for 5 h can significantly decrease the tensile strength of the B/Al composites.Failure mode of the composite also changes from cumulative to typical noncumulative after long time exposure at 500℃.Interfacial microstructure and phase composition of the B/Al composite before and after exposure is studied by TEM and SEM.It is showed that interfacial reaction is the main reason of decrease ofmechanical properties of the B/M composites.