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博碩士論文 etd-0707104-164603 詳細資訊
Title page for etd-0707104-164603
論文名稱
Title
石墨纖維/聚醚醚酮奈米複材積層板之研製與機械性能探討
Manufacturing and Mechanical Properties of AS4/PEEK Nanocomposite Laminates
系所名稱
Department
畢業學年期
Year, semester
語文別
Language
學位類別
Degree
頁數
Number of pages
66
研究生
Author
指導教授
Advisor
召集委員
Convenor
口試委員
Advisory Committee
口試日期
Date of Exam
2004-06-23
繳交日期
Date of Submission
2004-07-07
關鍵字
Keywords
高溫、疲勞、拉伸、奈米微粒、複合材料、機械性質
mechanical property, laminate, tensile test, composite, elevated temperature, Nano-particles
統計
Statistics
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中文摘要
本文首先研製碳纖維/聚醚醚酮奈米複材積層板。實驗中所採用之複材預浸布為碳纖維(AS-4)/聚醚醚酮(PEEK),考慮之疊序有兩種分別為十字疊及類似均向疊,皆為16層厚約2mm,並採用修正的隔膜成形法熱壓製成積層板。在奈米材料方面,採用平均粒徑為15±5nm的SiO2奈米微粒,將其溶解於乙醇中,並均勻塗佈於複材疊層間。經由機械性能之測試得知,塗抹10層SiO2奈米微粒的奈米複材積層板具有最佳之機械性能,其奈米微粒含量占複材全部重量之1% (基材重量之3%),而與原先未加奈米微粒的複材積層板比較可得,在十字疊試片方面,極限強度與彈性係數分別增強10.91%與6.7%,而類似均向疊試片方面,極限強度與彈性係數分別增強12.48%與19.93%。
接著為進行高溫的機械性能測試,環境溫度參數為50℃、75℃、100℃、125℃、150℃,進而獲致機械性能:破壞強度、勁度及應力-應變關係,由實驗結果可知,極限強度在溫度75℃以下時些微的下降,彈性模數則在溫度125℃以下時些微的下降,而兩種疊序的試片都在溫度為150℃( Tg)時有較高的衰減。
最後進行拉伸-拉伸疲勞實驗,在十字疊試片方面,104疲勞振次之前兩條應力-疲勞振次曲線仍然十分接近,但在105疲勞振次之後,塗抹奈米微粒十字疊試片的應力-疲勞振次曲線開始向下彎。而塗抹奈米微粒類似均向疊試片的應力-疲勞振次曲線始終在未添加奈米微粒試片的下方。
Abstract
The work aims to manufacture AS-4/PEEK APC-2 nano-composite laminates first. We used the prepreg form of AS-4 Graphite/PEEK laminae to make APC-2 laminates of 2 mm thick with two lay-ups of cross-ply and quasi-isotropic totally 16 plies by a hot press via the modified diaphragm curing. The nano-particles SiO2 with the average diameter of 15±5 nm were uniformly spread in the specific interfaces of laminate. From mechanical testing it is found that the nanocomposite specimens of spreading 10 plies nanoparticles (3% by wt. of matrix) possesses the highest mechanical properties. we see that in cross-ply specimens the ultimate strength increases 10.91 % and stiffness 6.7 %; while in quasi-isotropic specimens the ultimate strength increases 12.48 % and stiffness 19.93 %.
Second, repeat the tensile tests at 50, 75, 100, 125, 150℃ to receive respective stress-strain curve , strength and stiffness. At elevated temperatures the ultimate strength decreases slightly below 75℃ and the elastic modulus reduces slightly below 125℃, however, both properties degrade highly at 150℃ ( Tg) for two layups generally.
Finally, the constant stress amplitude tension-tension cyclic testing was conducted. It is found that both the stress-cycles (S-N) curves are very close below 104 cycles for cross-ply laminates w/wo nanoparticles, and the S-N curve of nano-laminate slightly bent down after 105 cycles. Whilst in quasi-isotropic laminates, the S-N curve of nano-laminate is always slightly below that of APC-2 laminate through the life.
目次 Table of Contents
目錄 ………………………………………………………………..I
表目錄 ………………………………………………………………III
圖目錄 ………………………………………………………………IV
摘要 …………………………………………………………………X
英文摘要 ……………………………………………………………XI
第一章 緒論 ………………………………………………………1
1-1前言 ……………………………………………………1
1-2材料簡介 ………………………………………………1
1-2-1 複合材料概述 ……………………………………1
1-2-2 奈米材料性質簡介 ………………………………2
1-2-3 奈米複合材料簡介 ………………………………3
1-3 研究方向 ………………………………………………4
1-4 文獻回顧 ………………………………………………5
1-5組織與章節 …………………………………………….7
第二章 實驗工作 ………………………………………………….8
2-1實驗材料簡介 ………………………………………….8
2-2 儀器設備 ………………………………………………8
2-3 奈米複材積層板之製程 ………………………………9
2-4 試片製作與分組 ……………………………………...11
2-5 拉伸與疲勞實驗 ……………………………………...12
2-6 掃瞄式電子顯微鏡實驗……………………………….13
第三章 實驗結果 …………………………………………………23
3-1靜態拉伸實驗 …………………………………………23
3-2疲勞實驗 ………………………………………………24
3-3電子顯微鏡觀察 ………………………………………27
3-4破壞機制觀察 …………………………………………27
第四章 分析與討論 ……………………………………………..55
4-1 SiO2奈米微粒對複材機械性能之影響 ………………55
4-1-1在極限強度與彈性模數方面 …………………….55
4-1-2在疲勞強度方面 ………………………………….56
4-2溫度效應之影響 ………………………………………57
4-3破壞模式之探討 ………………………………………59
第五章 結論與建議 ……………………………………………..61
5-1結論 ……………………………………………………61
5-2建議 ……………………………………………………62
5-3未來展望 ………………………………………………62
參考文獻 …………………………………………………………..64
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