| Literature DB >> 30966326 |
Maja Kuzmanović1, Laurens Delva2, Dashan Mi3,4, Carla Isabel Martins5, Ludwig Cardon6, Kim Ragaert7.
Abstract
The main goal of this research is to study the development of crystalline morphology and compare it to various mechanical properties of microfibrillar composites (MFCs) based on polypropylene (PP) and poly(ethylene terephthalate) (PET), by adding a functional compatibilizer and a non-functional rubber in two different steps in the processing sequence. The MFCs were prepared at a weight ratio of 80/20 PP/PET by twin screw extrusion followed by cold drawing and injection moulding. The non-functionalized polyolefin-based elastomer (POE) and the functional compatibilizer (i.e., POE grafted with maleic anhydride (POE-g-MA)) were added in a fixed weight percentage at two stages: during extrusion or during injection moulding. The morphology observations showed differences in crystalline structure, and the PP spherulite size was reduced in all MFCs due to the presence of PET fibrils. Their relationship with the mechanical performances of the composite was studied by tensile and impact tests. Adding the functional compatibilizer during extrusions showed better mechanical properties compared to MFCs. Overall, a clear relationship was identified between processing, structure and properties.Entities:
Keywords: crystalline morphology; crystallinity; mechanical properties; microfibrillar composites
Year: 2018 PMID: 30966326 PMCID: PMC6414988 DOI: 10.3390/polym10030291
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.329
Figure 1Morphology of blend during cold drawing with and without compatibilizer added during extrusion [4].
Formulations of the composites.
| Material | PP/PET wt % | CA wt % |
|---|---|---|
| MFC | 80/20 | 0 |
| POEEXT | 75.2/18.8 | 6 EXT |
| POE- | 75.2/18.8 | 6 EXT |
| POEIM | 75.2/18.8 | 6 IM |
| POE- | 75.2/18.8 | 6 IM |
Figure 2POM micrographs of neat PP sample in transferred direction to the injection flow.
Average diameter of PP spherulites and PET fibrils in the composites.
| Material | Spherulite Size (µm) | Fibril Diameter (µm) |
|---|---|---|
| PP | 22.3 ± 0.8 | - |
| POEEXT | 5.5 ± 0.7 | 0.8 ± 0.3 |
| POE- | 4.2 ± 0.3 | 0.5 ± 0.1 |
| POEIM | 7.2 ± 0.4 | 0.7 ± 0.3 |
| POE- | 7.6 ± 0.4 | 0.6 ± 0.2 |
Figure 3Microstructures of MFCs samples obtained via POM along the flow direction: (A) MFC; (B) POEEXT; (C) POE-g-MAEXT; (D) POEIM; (E) POE-g-MAIM. Microstructures of MFCs samples obtained via SEM in transverse direction: (A’) MFC (PP partially etched after 1.5 h in hot xylene); (B’) POEEXT (PP partially etched after 1.5 h in hot xylene); (C’) POE-g-MAEXT (PP partially etched after 3 h in hot xylene); (D’) POEIM (PP partially etched after 3 h in hot xylene); (E’) POE-g-MAIM (PP partially etched after 3 h in hot xylene).
Figure 4SEM micrographs of cryogenically fractured surface under liquid nitrogen of the injection moulded samples: (A) MFC (spherulite around fibril hole); (B) POEEXT (randomly oriented lamellae); (C) POE-g-MAEXT (non-reacted compatibilizer particles dispersed into matrix); (D) POEIM (rubber located at the interface); (E) POEIM (spherulite orientation around the fibril hole); and (F) POE-g-MAIM (compatibilizer particles located at the interface).
Thermal properties of PP, MFC, POEEXT, POE-g-MAEXT, POEIM, POE-g-MAIM during heating and cooling.
| Material | αcPP (%) | ||||
|---|---|---|---|---|---|
| PP | 171.5 ± 0.2 | 118.8 ± 0.1 | 122.5 ± 1.2 | 108.1 ± 1.4 | 47.05 ± 0.8 |
| POEEXT | 170.1 ± 0.4 | 123.1 ± 0.6 | 127.1 ± 0.2 | 113.2 ± 0.1 | 48.40 ± 0.5 |
| POE- | 170.1 ± 0.4 | 118.1 ± 0.6 | 121.5 ± 0.2 | 109.3 ± 0.9 | 50.01 ± 1.9 |
| POEIM | 169.3 ± 0.9 | 122.9 ± 0.4 | 127.1 ± 0.2 | 113.2 ± 0.3 | 51.65 ± 2.9 |
| POE- | 170.1 ± 1.2 | 116.4 ± 0.6 | 123.0 ± 0.1 | 108.3 ± 0.5 | 49.44 ± 2.8 |
Figure 5Tensile properties of MFC composites (A) Tensile modulus; (B) Yield strength at zero slope.
Strain at break of the composites.
| Material | Strain at Yield (%) | Strain at Break (%) |
|---|---|---|
| MFC | 3.74 ± 0.9 | 5.29 ± 0.9 |
| POEEXT | 6.84 ± 0.2 | 10.69 ± 1.7 |
| POE- | 11.90 ± 0.3 | 190.37 ± 162.8 |
Figure 6Tensile fracture model: (A) Case MFC; (B) POE-g-MAEXT; (C) Case POEEXT, POEIM or POE-g-MAIM.
Figure 7(A) Comparison of impact strength of MFC composites; (B) Impact fracture model of MFC.
Mechanical properties of injection moulding blends.
| Material | Tensile Modulus GPa | Yield Strength MPa | Strain at Break % | Impact Strength kJ/m2 |
|---|---|---|---|---|
| PP | 1.47 ± 0.1 | 17.3 ± 1.2 | >500 | 1.45 ± 0.2 |
| IMBPOEext | 1.58 ± 0.1 | 27.59 ± 0.7 | 10.43 ± 2.6 | 3.04 ± 0.5 |
| IMBPOE-g-MAext | 1.21 ± 0.1 | 29.54 ± 0.1 | 10.48 ± 4.8 | 6.55 ± 1.9 |