the laminates are fully impregnated and no phase separation is visible the stitching thread is completely melted and has become a part of the matrix the realized fiber volume content is about 45 fig1 comparison of tensile properties of laminates made from hybrid perform and commercial cfrtp laminates made from woven fabrics all values are related to a total fiber volume content of 50 is showing the determined tensile properties of produced pa6 laminates made from side by side hybrid preforms and pps laminates made from commingled yarns compared with properties of commercial cfrtp laminates u201c n n mechanical data for carbon cd0286 pps tencate 2006 u201d for the aircraft industry for easy comparison with the commercial woven 0 u00b0 90 u00b0 laminates fiber volume content of 50 the values of the test laminates are scaled up to the identical fiber volume content actually the realized mechanical properties are higher for the side by side laminate than for the commercial ones due to the more stretched fibers without woven undulations for the commingled yarn especially the tensile modulus is lower due to fiber breakages caused by the commingling process depending on later applications the used hybrid yarn can consist of different types of reinforcing fibers carbon glass basalt aramid and any type of thermoplastic resin preferable are high performance thermoplastic resins like vestskeep 2000 g peek evonik the hybrid yarn build up can be side by side commingled or wrapped in which the reinforcing fiber volume content can be designed regarding the later application e g aircraft industry 50 for the preliminary induction analyses modified matrix filaments are produced with a spinning tester in vertical direction sdl.