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