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Experimental Studies on Micro-fracture Mechanics of High-Temperature Polymer Matrix Composites

Experimental Studies on Micro-fracture Mechanics of High-Temperature Polymer Matrix Composites
高温聚合物基复合材料微断裂力学实验研究
批准号:
04452111
负责人:
TAKEDA Nobuo
金额:
$4.29万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for General Scientific Research (B)
财政年份:
1992
资助国家:
日本
项目状态:
已结题
起止时间:
1992 至 1994

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项目成果

TAKEDA Nobuo的其他基金

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中文摘要
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英文摘要
The pupose of the present investigation is to study experimentally the micro-fracture process and mechanism of high-temperarture polymer matrix composite laminates under quasi-static monotonic and repeated fatigue loadings. Three diffirent types of microscopes with displacement-rate-controlled loading devices were used for in-situ microscopic observations of damage initiation and growth. Cross-ply laminates were chosen as basic laminate configurations for high-performance carbon fiber reinforced high-temperature epoxy composites. The damage evolution includes the following three stages : (1)Transverse crack initiation in transverse layrs, (2)Multiple transverse crack formation, and (3)Initiation and growth of delamination from tips of transverse cracks. Based on the above quantitative experimental results, some new theoretical models were proposed to predict the damage evolution.1. The tested CFRP materials include (1)a conventional 180゚C-cured TGDDM/DDS system (T300/3601), (2)an impro … More ved toughened system(T800H/3631), (3)an interlaminar-toughened system with interlaminar resin film layrs(T800H/3631-FM300), and(4)a new interlaminar-toughened system with nylon-particle-dispersed interlaminar layrs(T800H/3900-2). The laminate configurations were[0/90_n/0](n=4,8,12).2. In-situ microscopic observations were successfully conducted by a combination of an optical microscope(OM), a scanning electron microscope (SEM), and a scanning acoustic microscope (SAM) with each loading stage. The microscopic deformation and failure processes such as, (1)transverse crack initiation in transverse layrs, (2)multiple transverse crack formation, and(3)initiation and growth of delamination from tips of transverse cracks, were observed at 20゚C and 80゚C to study the temperatue effects.3. A new evolution law for transverse crack development was proposed based on the statistical strength distribution of 90゚layrs. A new evolution law for delamination from tips of transverse cracks was also proposed based on the energy balance concept. Both theoretical preditions were found to be sufficiently valid to explain the quantitative experimental results. An interaction between transverse cracks and delaminations was also considered for better prediction. These theories were also extended for fatigue-loaded specimens. Less
期刊论文(46)
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会议论文
SHIWA,Mitsuharu TAKEDA,Nobuo KISHI,Teruo: "Acoustic Emission Wave Propagation Properties on CFRP Laminates by Using Simulated AE Source (in Japanese)" Journal of the Japan Society for Composite Materials. Vol.20, No.3. 108-115 (1994)
SHIWA、Mitsuharu TAKEDA、Nobuo KISHI、Teruo:“使用模拟 AE 源研究 CFRP 层压板的声发射波传播特性(日语)”日本复合材料学会杂志。
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TAKEDA,Nobuo OGIHARA,Shinji: "Is Situ Observation and Probabilistic Prediction of Microscopic Failure Processes in CFRP Cross-ply Laminates" Composites Science and Tech. Vol.52, No.2. 183-195 (1994)
TAKEDA、Nobuo OGIHARA、Shinji:“CFRP 交叉层压板微观失效过程的现场观察和概率预测”复合材料科学与技术。
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志波光晴,武田展雄,岸輝雄: "CFRP積層板を伝播する疑似AE波の伝播特性" 日本複合材料学会誌. 20(3). 108-115 (1994)
Mitsuharu Shiba、Nobuo Takeda、Teruo Kishi:“通过 CFRP 层压板传播的伪 AE 波的传播特性”日本复合材料学会杂志 20(3) (1994)。
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N.Takeda,S.Ogiwara,A.Kobayashi: "In-situ Observation and Modelling of Micromechanical Failure Process in CFRP Cross-ply Laminates" Proc.9th Int.Comf.Comp.Mater.3. 351-358 (1993)
N.Takeda、S.Ogiwara、A.Kobayashi:“CFRP 正交层压板微机械失效过程的现场观察和建模”Proc.9th Int.Comf.Comp.Mater.3。
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20
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