Abstract
Nowadays, the aeronautical sector use composite materials reinforced with high performance fibers. In this field, the composites of thermoplastic matrix (TPCs) is reinforced with continuous carbon fibers wich combine both high strength and lightness thus offering a great potential to replacement, at least partially, the metal alloys. The thermoplastic matrix allows reducing manufacturing costs and minimizing recycling problems. The integration of TPCs sometimes forces to combine pieces which are very different in composition, forming a multimaterial.
During the development of the research , the manufacturing and physical-mechanical characterization of the CF-PEEK composite material and the union of said material with titanium was carried out.
Firstly, the characterization and optimization of the press forming process of the monolithic CF-PEEK has been developed. The characterization was carried out through DSC and TGA tests, mechanical tensile tests according to the standard UNE-EN 527-5 and microscopic analysis.
Then, the CF-PEEK-Ti joints were made and evaluated.In order to improve the quality of the joints has been used Ti-6Al-4V with two surface treatments (shot blasting and laser texturing) and enrich the surface with PEEK film.The mechanical characterization was carried out through the SLJ (Single Lap Joint) test according to the standard ASTM D5868.
The results have shown how the laser treatment improves the quality of the joint, achieving the highest efficiency by enriching the surface with PEEK film. The viability of multi-material joints has been demonstrated through direct production in the press.
Nowadays, the aeronautical sector use composite materials reinforced with high performance fibers. In this field, the composites of thermoplastic matrix (TPCs) is reinforced with continuous carbon fibers wich combine both high strength and lightness thus offering a great potential [...]