| Literature DB >> 32605091 |
Amirbek Bekeshev1, Anton Mostovoy2, Lyazzat Tastanova1, Yulia Kadykova2, Svetlana Kalganova2, Marina Lopukhova2.
Abstract
The conducted studies have proven the possibility of the directed control of operational properties of epoxy composites, due to the addition of finely-ground ocher into their composition, and the use of microwave modification of the epoxy composition. The rational content of ocher as a modifying additive (0.5 parts by mass) and a filler (75 parts by mass) of the epoxy composition has been selected, which ensures the improvement of the studied complex of physical-mechanical properties. It has been proven that ocher affects the structure formation processes and the structure of the epoxy composite, thus increasing its thermal, heat and fire resistance. During the research, the application efficiency has been proven, and the optimal parameters of the microwave modification (power-350 W; duration-30 s) of epoxy compositions filled with ocher, which increase physical-mechanical characteristics of composites, have been selected.Entities:
Keywords: Epoxy resin, modification, filler, ocher, microwave modification
Year: 2020 PMID: 32605091 PMCID: PMC7407493 DOI: 10.3390/polym12071437
Source DB: PubMed Journal: Polymers (Basel) ISSN: 2073-4360 Impact factor: 4.329
Figure 1Schematic illustration for the preparation process of ocher/epoxy composites.
Figure 2Kinetics of the epoxy composition curing.
Chemical composition of ocher.
| Component | Concentration, % |
|---|---|
| FeO(OH) | 85.95 |
| Al2O3 | 4.63 |
| Cr2O3 | 2.80 |
| SiO2 | 2.31 |
| NiO | 2.88 |
| TiO2 | 0.38 |
| CuO | 0.66 |
| CaO | 0.24 |
| S | 0.08 |
| P | 0.07 |
Figure 3Fractional composition of ocher.
Figure 4SEM data of ocher particles.
Figure 5XRF pattern of ocher particles: 1—FeO(OH) goethite; 2—Fe2O3 hematite; 3—Fe3O4 magnetite.
Properties of epoxy composites.
| The Composition, Parts by Mass Cured by 15 Parts by Mass of PEPA | Gben, MPa | Eben, MPa | Gcom, MPa | Gten, MPa | Eten, MPa | aim, kJ/m2 |
|---|---|---|---|---|---|---|
| 100 ED-20 + 40 ORPP | 80 ± 3.2 | 2210 ± 88 | 100 ± 4.0 | 30 ± 1.5 | 1896 ± 75 | 6 ± 0.3 |
| 100 ED-20 + 40 ORPP + 0.1 ocher | 87 ± 3.5 | 3206 ± 120 | 102 ± 4.1 | 41 ± 2.0 | 2113 ± 84 | 7 ± 0.3 |
| 100 ED-20 + 40 ORPP + 0.5 ocher | 105 ± 4.2 | 3500 ± 140 | 105 ± 4.1 | 53 ± 2.6 | 2317 ± 92 | 11 ± 0.5 |
| 100 ED-20 + 40 ORPP + 1.0 ocher | 75 ± 3.0 | 4073 ± 152 | 110 ± 4.4 | 43 ± 2.2 | 3040 ± 121 | 5 ± 0.2 |
| 100 ED-20 + 40 ORPP + 10 ocher | 80 ± 3.2 | 4373 ± 164 | 114 ± 4.5 | 53 ± 2.6 | 3242 ± 122 | 5 ± 0.2 |
| 100 ED-20 + 40 ORPP + 30 ocher | 76 ± 2.8 | 5568 ± 220 | 125 ± 5.0 | 36 ± 1.8 | 3512 ± 140 | 7 ± 0.3 |
| 100 ED-20 + 40 ORPP + 50 ocher | 74 ± 2.2 | 7462 ± 240 | 145 ± 5.6 | 41 ± 2.0 | 4000 ± 156 | 5 ± 0.2 |
| 100 ED-20 + 40 ORPP + 75 ocher | 102 ± 4.1 | 10163 ± 350 | 156 ± 5.8 | 45 ± 2.3 | 4110 ± 160 | 9 ± 0.4 |
| 100 ED-20 + 40 ORPP + 100 ocher | 55 ± 2.0 | 12120 ± 445 | 95 ± 4.0 | 32 ± 1.6 | 4860 ± 184 | 4 ± 0.2 |
Note: Gben—bending stress; Eben—modulus of elasticity in bending; Gcom—compressive strength; Gten—tensile strength; Eten is the tensile modulus of elasticity; aim—impact strength.
Figure 6Model for the role of ocher as modifying additive in the epoxy composite.
Figure 7SEM of the surface of the destruction of epoxy composites: (a)—without ocher; (b)—with 75 parts by mass of ocher, relative to ED-20.
Figure 8Kinetic curves of the curing process of compositions, parts by mass: 1—100ED-20 + 40ORPP + 15PEPA; 2—100ED-20 + 40ORPP + 0.5Ocher + 15PEPA; 3—100ED-20 + 40ORPP + 75Ocher + 15PEPA.
Values of the curing process of epoxy composites.
| Composition, Parts by Mass, Cured by 15 Parts by Mass of PEPA | τgel, | τcur, | Tmax, |
|---|---|---|---|
| 100ED-20 + 40ORPP | 27 | 38 | 88 |
| 100ED-20+40ORPP+0.5 ocher | 21 | 30 | 99 |
| 100ED-20+40ORPP +75 ocher | 17 | 29 | 96 |
Note: τgel is the duration of gelation process, τcur is the duration of curing, Tmax is the maximum temperature of the sample self-heating during curing.
Physico-chemical properties of epoxy composites.
| Composition, Parts by Mass, Cured by 15 Parts by Mass of PEPA | Tin, °C | Tf °C | Yield of CS at Tf,% Mass | Tv, °C | OI, % vol. |
|---|---|---|---|---|---|
| 100ED-20 | 200 | 390 | 40 (390 °C) | 86 | 19 |
| 100ED-20 + 40ORPP | 230 | 370 | 54 (370 °C) | 132 | 28 |
| 100ED-20 + 40ORPP + 0.5 ocher | 240 | 360 | 58 (360 °C) | 148 | 28 |
| 100ED-20 + 40ORPP + 50 ocher | 242 | 370 | 69 (370 °C) | 170 | 30 |
| 100ED-20 + 40ORPP + 75 ocher | 245 | 370 | 72 (370 °C) | 190 | 31 |
| 100ED-20 + 40ORPP + 100 ocher | 245 | 370 | 76 (370 °C) | 210 | 32 |
Note: Tin, Tf—initial and final temperature of the main stage of thermolysis; CS—carbonized structures, Tv—Vicat heat resistance, OI—oxygen index.
Properties of epoxy composites.
| Parameters of Microwave Modification of Composition in parts by Mass: | Gben, MPa | Eben, MPa | Gt, MPa | Et, MPa | aim, kJ/m2 |
|---|---|---|---|---|---|
| Without microwave modification | 105 ± 4.2 | 3500 ± 140 | 58 ± 2.6 | 2317 ± 92 | 11 ± 0.5 |
| 200 W, 15 s | 108 ± 4.3 | 4192 ± 165 | 57 ± 2.3 | 2804 ± 112 | 11 ± 0.5 |
| 200 W, 30 s | 128 ±4.5 | 4438 ± 168 | 63 ± 2.8 | 2889 ± 115 | 13 ± 0.6 |
| 200 W, 45 s | 100 ± 4.0 | 4101 ± 145 | 55 ± 2.0 | 2039 ± 81 | 7 ± 0.4 |
| 250 W, 30 s | 130 ± 4.5 | 4892 ± 175 | 59 ±2.4 | 3162 ± 125 | 13 ±0.6 |
| 300 W, 30 s | 132 ± 4.6 | 3861 ± 145 | 75 ± 3.0 | 2674 ± 110 | 12 ± 0.5 |
| 350 W, 30 s | 158 ± 6.0 | 5193 ± 200 | 75 ± 3.0 | 3075 ± 123 | 15 ± 0.7 |
| 400 W, 30 s | 121 ± 4.8 | 3685 ± 142 | 58 ± 2.3 | 2628 ± 105 | 10 ± 0.5 |
| 500 W, 30 s | 115 ± 4.6 | 3470 ± 135 | 45 ± 1.8 | 2031 ± 81 | 8 ± 0.4 |
Note: Gben—bending stress; Ebe—modulus of elasticity in bending; Gt—tensile strength; Et—tensile modulus of elasticity; aim—impact strength.
Figure 9Physico-mechanical characteristics of epoxy composites: 1—epoxy composite, without filler and microwave modification; 2—epoxy composite with 0.1 parts by mass of ocher relative to ED-20, without microwave modification of composition; 3—epoxy composite with 0.1 parts by mass of ocher relative to ED-20, and after microwave modification of composition.
Figure 10SEM of the surface of the destruction of epoxy composites: (a)—without microwave modification; (b,c)—after microwave modification.