Abstract
Abstract The discussion of the possibility of application of the GPI (gas pressure infiltration) process to the manufacturing of composites based on selected aluminium alloys reinforced with carbon fibres coated with nickel protective layer, as well as the determination of selected properties of materials obtained using this technique, is presented in the article. The composites reinforced unidirectionally (UD) were produced, the suitable volume fraction of fibres was determined and the proper forming parameters were established. Basing on the obtained results, with application of the same components, the composites reinforced three-directionally (3D) were subjected to infiltration. The preforms were designed and prepared using plaiting and joining methods. The GPI process parameters were verified for the assumed fibre arrangement. Thermal expansion of matrix alloys and composites obtained with application of most favourable parameters was determined and the influence of fibre arrangement and chemical composition of the matrix on the obtained results was analysed. The comparative abrasion tests with application of different velocities were performed for the selected alloy and the composite reinforced unidirectionally. In order to evaluate the changes taking place in the matrix during infiltration, the analysis of chemical composition of composites was performed for materials reinforced unidirectionally, as an example. The correctness of distribution of fibres in the composite matrix was also evaluated by means of microstructure observation as well as non-destructive testing with application of computed tomography technique. The results obtained during the investigations provide information concerning suitability and limitations of the GPI method to the manufacturing of light structural parts from the proposed components.
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