Table 8.
Type of Polymer | Type of CNT | CNT Content (wt.%) | Improvement Properties | Potential Application | Reference |
---|---|---|---|---|---|
- | SWCNT | 100 wt.% | Up to 3500 W/m·K | Heat sinks, connectors, batteries, light-emitting diode devices, automotive electronic control units, printed circuit boards, electronic assembly, and packaging | [177] |
Polyacrylate composites | MWCNT | 50–80 wt.% | ˄ ~0.50 to 1.67 W/m K | Aerospace and aeronautics material | [183] |
PLA | MWCNT | 0.25–2.5 wt.% | 27.5 mW·m−1K−1 | High performance thermal insulator | [184] |
Poly-dimethyl siloxane | MWCNT | ~2 wt.% | ˄ ~1.5 W/m·K | Thermal insulator/high thermal conductivity polymer composites | [185] |
Poly-dimethyl siloxane/Si | MWCNT | ~30% | ˄ ~10% of 3000 W/m·K ≈3300 W/m·K |
||
Polymer-based composite | CNTs | 30% | 1000–4000 W/m·K | Light-emitting diodes and thermal dissipation | [179] |
Polystyrene | MWCNT | 1% | ~30.2 mW/m-K without using any insulation gas | Super-thermal insulation properties | [186] |
Poly (vinylidene fluoride) | MWCNT/graphene(1:1) | 10% of (s-MWCNTs)/graphene (GE) | ˄ ~711.1% of 0.19 W/m·K ≈135.11 W/m·K |
Heat exchanger | [187] |
PC | MWCNT | 2% | ˄ ~1.27 W/m·K | High performance thermal insulator | [188] |
Resol-type phenolic resin | MWCNT | up to 1% | ˄ ~35 °C of maximum degradation temperature | Strong network char layer without any cracks or opening | [189] |
Carbon prepreg (IM7) composite | SWCNT | 30% | ˄ 30% heat capacity | Pipes and heat exchangers, replacer material for heavy-lift rocket under the Space Launch System (SLS), and promising high performance material for future space vehicles. | [190] |
˄ 30% thermal diffusivity | |||||
˄ ~120–150% thermal conductivity | |||||
Epoxy | MWCNT | 0.3 wt.% | ˄ 35–42% of critical buckling temperature | Coefficient of thermal expansion (CTE) and thermal buckling of epoxy-based composites | [191] |
Epoxy | SWCNT | 1 wt.% | ˄ ~125% W/m·K (method raw laser-oven) |
High performance thermal insulator | [90] |
3 wt.% | ˄ ~30% W/m·K |