Review Article
Recent Advances in Energy Harvesting Technologies for Structural Health Monitoring Applications
Table 2
Simulated power levels for temperature gradients on an aircraft [
12].
| | Peak temperature differential, °C | Peak power, mW | Average power, mW |
| Cargo skin | 40 | 34.15 | 22.58 | Cargo primary Insulation |
| Hydraulic pipeline 1 | 20 | 7.97 | 3.07 | Hydraulic pipeline 2 |
| Waste water tank | 15 | 5.46 | 2.99 | Waste water ambient |
| E-bay fuselage skin | 35 | 18.72 | 6.42 | E-bay primary insulation |
| Cabin wall fuselage skin | 30 | 13.36 | 3.97 | Cabin wall primary insulation |
| Cabin wall fuselage skin | 40 | 30.06 | 11.70 | Cabin wall secondary insulation |
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