1. Introduction
The limitation of resources and energy demands for resource efficient lightweight constructions and energy reduced productions [
1]. Therefore, metal components are substituted with continuous fibre-reinforced plastics (FRP). In particular, thermoplastic matrix systems are brought into focus due to their ductile material behaviour achieving higher impact resistance in comparison to conventional technologies. Braided crash tubes made of glass fibre (GF) and polypropylene (PP) achieving a specific energy absorption of 36 kJ/kg where metallic tubes achieving 12.5 kJ/kg to 38 kJ/kg [
2]. Furthermore, the recycleability, an easier processability and tunability of the viscosity are advantages during component production. With their high specific material properties of stiffness and strength, novel components can be developed by integrative constructions and functional integration. Due to the anisotropic behaviour of the single layers of FRP, an application for load introduction areas with three-dimensional (3D) stress states is not appropriate. Therefore, joining technologies for metal and continuous fibre-reinforced thermoplastic composites (TPC) are required. Mechanical joining for metal TPC joints like clinching [
3], pinning [
4] or further non-adhesive joints [
5] are in the focus of ongoing work. In addition, for thermal-assisted joining technologies, the initial material structure is changed due to the tool motion [
6]. For pinning processes ([
4]), yarns with their initial cross section are displaced and deformed (
Figure 1). The resultant and deformed material structure influences the load bearing behaviour depending on load cases [
7]. The assessment of the load capacity in terms of stiffness and strength can be conducted by experimental investigations. To reduce the experimental effort and optimize the development process, the prediction of resultant material structure via numerical scale-specific process simulation is required [
8,
9].
For advanced process simulations of complex local forming processes like mechanical joining, the deformation behaviour of yarns and fibre bundles has to be investigated and modelled in detail. Hence, both a phenomenological description and a quantitative characterisation of fibre bundle deformation are necessary. The characterisation of fibre bundle deformation during forming processes often focuses on deformation by bending. Therefore, cantilever beam bending test [
10] or advanced test rig setups based on parallel-plate rheometer (PPR) [
11] for unidirectional (UD) TPC are carried out. For more complex textile architectures like fabrics, picture frame tests are conducted to investigate the in-plane shear behaviour [
12] and predict wrinkles. The material behaviour in transverse direction for UD fibre bundles under process conditions for compaction are investigated by [
13]. A simplified PPR setup in an in situ CT is used for compaction tests of fibre bundles. Within the CT, the compaction phenomena like squeeze flow, fibre reorientation and fibre–fibre interaction (FFI) can be seen in detail. Due to investigations of the forming phenomena of in- and out-of-plane deformation, matrix flow (percolation) and FFI during joining demand more complex test setups. The test setups should achieve a defined degree of forming within a complex forming process and measurement system to assess the resultant forming forces or strains and displacements for validation of forming simulations. Therefore, common pultrusion technology with the defined process conditions and defined degrees of formation are appropriate.
The pultrusion process enables a production of high quality parts within short cycle times due to a continuous production and novel manufacturing processes [
14] also for thick layups [
15]. Thermosetting matrix systems have been established, but, in the recent years, thermoplastic matrices are also a focus [
16]. Investigations of pultrusion processes with fibre reinforced thermoplastics are carried out with complex pultrusion test setups including a heating and a cooling die [
17,
18,
19,
20,
21,
22] and also for advanced injection pultrusion processes developed in [
23]. Within the papers, profiles are formed and focused on process optimization of the dies [
17], novel material combinations [
22], modelling [
18,
24,
25,
26] and simulation strategies [
27]. The resultant fibre volume content (FVC) can achieve approx. 50% for carbon fibre (CF)/PP and 52% GF/PP in [
17] or 44% in [
21] with GF/Polybutylenterephthalate (PBT). Process quality is often assessed on the basis of the resulting mechanical properties; in particular, the shear strength is investigated [
17,
20,
22,
28]. However, forming and deformation behaviour in the tapered forming element is not evaluated, despite the development of the modelling strategy of a pultrusion process in [
27]. For fibre bundle deformations, the pulling force is a necessary factor to assess modeling strategies and required joining forces.
The occurring forming phenomena of thermoplastic prepregs are driven by the temperature dependent material behaviour of the thermoplastic matrix. By increasing the temperature, the viscosity and therefore the viscous force against deformation decreases. In [
29], the viscosity
of the PP with approx. 400 Pa · s to 600 Pa · s for low shear rates at different temperature levels is given. In comparison with thermosetting matrix system (e.g., RTM6 [
30]), the viscosity can be approx. up to 1000× higher under process conditions. The pulling force depending on several mechanisms as stated in [
28] such as viscous resistance and compaction resistance.
An investigation of the pultrusion of GF/PBT bundles up to a pulling speed of
m/min is conducted by [
21]. Despite the continuous measurement of the pulling force, the maximum force at a speed of
m/min is just given with “below 500 N even at high pulling speeds of
m/min” for a pultruted beam profiles of 3.5 × 10
. In contrast, in [
19], a pulling speed of 10 mm/s for CF/Polyetheretherketone (PEEK) and 8 mm/s for GF/PP could be achieved. Two different rectangular forming element configurations were used. The pulling force for CF/PEEK was determined for a slightly over-filled forming element with less squeezed back material by around 1 kN for pulling speeds between 1 mm/s to 10 mm/s, whereas a highly over-filled forming element with a high squeezed back material flow shows a wide force range between approx. 2.5 kN to 4 kN by a velocity range of 2 mm/s to 4 mm/s. It can be concluded that the pulling force is less influenced by the velocity when using a slight over-filled forming element. In addition, the temperature influence to the pulling force is investigated. For increasing temperature, an exponential drop of the pulling force can be seen. For GF/Polyamide 66 (PA66), an oscillating motion of the mandrel is used to decrease the pulling force by [
31]. Due to the pultruted hollow profile and the applied textile architecture by using braiding, the forces differ between approx. 3 kN for oscillating setup and force range of approx. 4.5 kN to 6.5 kN for the non-oscillating mandrel.
Compacting and forming processes of thermoplastic prepreg material based on pultrusion were carried out by [
32]. The CF/PA12 material is used to generate a 3D lattice construction by heating up to 230 °C by a velocity of 100 mm/min. The pultrudate is assessed in terms of voids with 4% by micrographs without taking the pulling force into account.
The pultrusion in [
33] of rods with a diameter of 5 mm with hybrid fibres and commercially commingled yarns GF/Polycarbonate (PC) by varying temperature and pulling speed are assessed by determination of void content and resultant pulling force. It could be shown that the filling degree
m of the die with 50 N (
95%) up to 270 N (
105%) and the pultrusion speed with 80 N (
50 mm/min) up to 230 N (
100 mm/min) show the most influence on the pulling force.
The investigation of pulling forces with respect to the cooling temperature in the die are carried out by [
34]. With commingled yarn of CF/Polyetherimide (PEI) and CF/PEEK and different cooling temperatures, the process is assessed among other things by the resultant void content evaluated by microscopic analysis and the measured pulling forces. The resultant die diameter of
mm leading to pulling forces of approx. 100 N to 300 N for PEI and 40 N to 170 N for PEEK. The pulling forces are driven by adhesion and crystallisation effects caused by cooling strategy.
The experimental results show the influence of viscous and also friction induced drag through cooling. The assessment of the resultant material structure of the rod is well done but does not take the forming process of the used material into account.
However, the knowledge of fibre failure and forming behaviour of semi-finished prepreg material as a fibre bundle plays a key role in achieving high deformation grades, assessing the mechanical material behaviour and developing a modelling strategy for mechanical joining process on micro and meso scale. Therefore, in the present paper, a simplified pultrusion process setup is introduced. The setup enables the investigation of the dependency of tensile forces, forming element temperature, pultrusion speed, the achieved degree of forming and the inner material structure in the forming zone of the preimpregnated continuous fibre-reinforced unidirectional semi-finished thermoplastic material. The material structure is investigated in terms of a micrograph and CT analysis. The investigations gain a deeper knowledge of the forming phenomena in the forming element and the deformation induced fibre failures.