Table 3.
Mechanical properties and fabrication methods of different CF-based fiber hybrid composites
| Matrix | Brittle reinforcement/CF (x) | Ductile reinforcement (Y) | Fiber hybrid composite:CFRP:Y-reinforced composite | FVF in fiber hybrid composite (VFVF: VX/VY) | Fabrication method | References |
|---|---|---|---|---|---|---|
| Epoxy resin | Unidirectional plain weave CF | Chopped GF |
TS = 1:1.29:0.77 CS = 1:1.31:0.49 ILSS = 1:0.85:0.95 |
– | Hand lay-up | [103] |
| Epoxy | Carbon fabric | Bi- directional Jute fabric |
TS = 1:1.74:0.06 FS = 1:1.19:0.27 IS = 1:0.68:1.05 |
45 (49%/51%) | Hand lay-up | [104] |
| Epoxy resin | T300 CF 3 K | E-GF |
TS = 1:1.61:0.76 CS = 1:1.52:0.68 FS = 1:1.12:0.54 |
45 (50%/50%) | Hand lay-up | [8] |
| Epoxy resin | Satin weave T-300 carbon fabric | Plain weave E-glass fabric |
TS = 1:1.17:0.74 CS = 1:1.05:0.89 |
52 (47%/ 53%) | – | [105] |
| Epoxy | CF C120-3 K | Woven basalt fiber |
FS = 1:1.20:0.6 FM = 1:1.16:0.55 |
62 (60%/40%) | VARTM | [99] |
| PP-natural rubber | PAN-based CF | Kenaf fiber | FS = 1:1.89:1.5 | 20 (50%/50%) | Compression molding | [101] |
| ABS | SCF | Kevlar fiber |
FS = 1:0.95:0.81 FM = 1:1.08:0.75 |
– | 3DP | [102] |
| Epoxy resin | Unidirectional CF | Unidirectional GF |
TS = 1:1.14:0.68 FS = 1:1.21:0.68 Elongation (%) at max. stress = 1:0.91:1.84 |
48.8 (66.67%/33.33%) | Hand lay-up and vacuum infusion | [106] |
| PP | SCF | SGF |
TS = TSCFRP > TShybrid > TSGFRC Failure strain = failure strain CFRP < Failure strain hybrid < failure strain GFRC |
25 (50%/50%) | Injection molding | [39] |