Abstract

The use of polymer matrix composites (PMC) for manufacturing primary load-bearing structural components has significantly increased in many industrial applications. Specifically in the aerospace industry, PMCs are also being considered for elevated temperature applications. Current aerospace-grade composite components subjected to fatigue loading are over-designed due to insufficient understanding of the material failure processes, and due to the lace of available generic fatigue prediction models. A comprehensive literature survey reveals that there are few fatigue studies conducted on woven and braided fabric reinforced PMC materials, and even fewer at elevated temperatures. It is therefore the objective of this study to characterize and subsequently model the elevated temperature fatigue behaviour of a triaxial braided PMC, and to investigate the elevated temperature of fatigue properties of two additional woven PMCs. An extensive experimental program is conducted using a unique test protocol on the braided and woven composites, which consists of static and fatigue testing at various test temperatures. The development of mechanically-induced damage is monitored using a combination of non-destructive techniques which included infrared thermography, fiber optic sensors and edge replication. The observed microscopic damage development is quantified and correlated to the exhibited macroscopic material behaviour at all test temperatures. The fiber-dominated PMC materials considered in this study did not exhibit notable time or temperature-dependent static properties. However, fatigue tests reveal that the local damage development is in fact notably influenced by temperature. The elevated temperature environment increases the toughness of the thermosetting polymers, which results in consistently slower fatigue crack propagation rates for the respective composite materials. This has a direct impact on the stiffness degradation rate and the fatigue lives for the braided and woven composites under investigation. The developed analytical fatigue damage prediction model, which is based on actual observed damage mechanisms, accurately predicted the development of damage and corresponding stiffness degradation for the braided PMC, for all test temperatures. An excellent correlation was found between the experimental the predicted results to within a 2% accuracy. The prediction model adequately captured the local temperature-induced phenomenon exhibited by the braided PMC material. The results presented in this study are novel for a braided composite material subjected to elevated temperature fatigue.

Highlights

  • The results presented in this study are novel for a braided composite material subjected to elevated temperature fatigue

  • The creep strain is only 0.01% in magnitude at the highest stress level. This confirms that the exhibited strain ratcheting observed during both the room temperature and elevated temperature fatigue tests was mainly due to fatigue damage accumulation, and that any creep effects can be neglected

  • An investigation focussed on the tensile static and fatigue behaviour of a triaxial braided carbon fiber reinforced thermosetting resin composite, at both room temperature and elevated temperature, was conducted in order to gain a better understanding of the intricate material behaviour

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Summary

Objectives

The main objective of the study is to investigate the fatigue behaviour of a braided carbon fiber reinforced resin at elevated temperatures, and to provide a better understanding of the effects of both temperature and cyclic loading on the material behaviour. The characterization of damage development and the corresponding material behaviour during both static and fatigue loading, at both room temperature and elevated temperatures, is considered in detail. A corresponding fatigue damage model is developed for the braided material, and used to predict the degradation of the material properties during cyclic loading. The predicted results of the fatigue damage model are compared to the observed experimental damage development. Consideration for the effects of cyclic loading of other woven composites at elevated temperatures is investigated to provide a basis for discussion and comparison to the aforementioned braided composite material

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