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Prefailure damage processes in highly filled glass/mica/epoxy composites

机译:高填充玻璃/云母/环氧树脂复合材料的预失效损伤过程

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AbstractIn the present study, the prefailure damage processes of a series of short glass fiber/mica/epoxy composites under three‐point bending were elucidated using acoustic emission (AE) coupled within situscanning electron microscopy (SEM) observations. This study consisted of a detailed investigation of the damage tolerance of composite systems that had constant inorganic content of 75 by weight with a varying ratio of glass fibers to mica. The flexural strength was found to increase from 11 to 21 ksi as the glass fiber content increased (mica content decreased), while the flexural modulus decreased from 5.0 to 2.5 Msi. By monitoring the AE during flexural deformation of the glass fiber‐to‐mica ratio composites, it was determined that low amplitude (0–42 db) AE events, which occurred throughout the deformation process, were caused by matrix cracking, whereas the high‐amplitude (43–100 db) AE events, which occurred just prior to failure, were caused by a fiber‐related mechanism.In situSEM observations of the composites during flexural deformation allowed a correlation between the AE and the damage mechanisms as a function of strain. In the all‐mica composite, microcracking initiated in the linear region at preexisting flaws, on the order of 10 μm, located at the mica interface. These microcracks grew along the mica contours over the majority of the deformation process, emitting low‐amplitude events, until final fracture occurred at relatively low strains. In the glass fiber‐containing composites, microcracking initiated in the linear region at preexisting flaws and voids, on the order of 10 μm. These microcracks grew slowly, emitting low‐amplitude events, as the strain increased, but were prevented from causing failure at low strains because of the toughening effect of the glass fibers. At sufficiently high strains, however, fiber breakage and fiber pull‐out occurred that corresponded to the high‐amplitude events detected by the AE. At strains just prior to failure, catastrophic crack growth occurred, producing a rapid increase in both low‐and high‐amplitude e
机译:摘要 本研究利用原位扫描电子显微镜(SEM)观测,利用声发射(AE)耦合,阐明了一系列短玻璃纤维/云母/环氧树脂复合材料在三点弯曲下的破坏前损伤过程。本研究包括对复合材料系统的损伤耐受性进行详细调查,这些复合材料的无机含量恒定为75%(按重量计),玻璃纤维与云母的比例不同。随着玻璃纤维含量的增加(云母含量降低),弯曲强度从11 ksi增加到21 ksi,而弯曲模量从5.0 msi降低到2.5 msi。通过监测玻璃纤维与云母比复合材料弯曲变形过程中的 AE,确定在整个变形过程中发生的低振幅 (0–42 db) AE 事件是由基体开裂引起的,而在失效前发生的高振幅 (43–100 db) AE 事件是由纤维相关机制引起的。在弯曲变形过程中对复合材料进行原位SEM观察,可以发现AE与损伤机制之间存在应变函数的相关性。在全云母复合材料中,位于云母界面处的线性区域在预先存在的缺陷处开始微裂纹,大约为10 μm。在大部分变形过程中,这些微裂纹沿着云母轮廓生长,发出低振幅事件,直到最终断裂发生在相对较低的应变下。在含玻璃纤维的复合材料中,在线性区域预先存在的缺陷和空隙处开始微裂纹,大约为10μm。随着应变的增加,这些微裂纹缓慢增长,发出低振幅事件,但由于玻璃纤维的增韧作用,在低应变下不会引起破坏。然而,在足够高的应变下,纤维断裂和纤维拉出与AE检测到的高振幅事件相对应。在失效前的应变中,发生了灾难性的裂纹扩展,导致低振幅和高振幅迅速增加

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