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FATIGUE MODELING OF MARINE COMPOSITES

机译:船舶复合材料的疲劳建模

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摘要

Fatigue of aerospace-grade composite materials has been a research topic for many years. The vast majority of these studied material systems include various laminate configurations constructed from unidirectional carbon-epoxy, autoclave-cured prepregs. To date, however, no protocols demonstrating N-year service life for these materials have been standardized. Marine composites have generally migrated towards E-glass fibers and polyester, vinyl ester, or epoxy resins processed via wet layup and liquid infusion techniques and out-of-autoclave cure schedules. Although fatigue research of marine composite materials has been increasing, the relative number of databases is small compared to those generated with aerospace-grade composites. Also, the lack of a legacy standard life-prediction protocol for guidance has resulted in composite marine structures employing large safety factors and load-path redundancy in their design. This paper attempts to add to the current research by offering an approach to structural life prediction through fatigue modeling based upon coupon-level characterization, and demonstrated with subelement testing and non-destructive monitoring.
机译:航空航天级复合材料的疲劳是多年来的研究课题。绝大多数研究的材料系统包括由单向碳 - 环氧树脂,高压釜固化的预浸料构成的各种层压构型。然而,迄今为止,没有证明这些材料的N年使用寿命的协议已经标准化。海洋复合材料一般迁移到通过湿覆盖和液体输注技术和外灭菌性调节的外玻璃纤维,乙烯基酯,乙烯基酯或环氧树脂。虽然海洋复合材料的疲劳研究已经增加,但与航空级复合材料产生的那些,数据库的相对数量小。此外,缺乏用于指导的遗留标准寿命预测协议导致了在其设计中采用大安全因子和负载路径冗余的复合海洋结构。本文试图通过基于优惠券级别表征通过疲劳建模提供结构寿命预测的方法来增加当前研究,并用子元件测试和非破坏性监测。

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