2012
DOI: 10.1088/1742-6596/382/1/012025
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Energy Harvesting for Aerospace Structural Health Monitoring Systems

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Cited by 31 publications
(34 citation statements)
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“…In case of tire pressure monitoring system (TPMS), the vibration is distributed over the frequency range from 100 to 1000 Hz with quite high acceleration [39]. Similar high frequency application environment is available from aerospace vehicles during their take-off and landing [40]. The reported devices can be useful under such circumstances for harvesting useful electrical energy.…”
Section: Normali Zed Power I Ntegral Density (N P I D)mentioning
confidence: 99%
“…In case of tire pressure monitoring system (TPMS), the vibration is distributed over the frequency range from 100 to 1000 Hz with quite high acceleration [39]. Similar high frequency application environment is available from aerospace vehicles during their take-off and landing [40]. The reported devices can be useful under such circumstances for harvesting useful electrical energy.…”
Section: Normali Zed Power I Ntegral Density (N P I D)mentioning
confidence: 99%
“…Because aircrafts flying at high altitudes are subject to large thermal gradients, the use of TEGs to power wireless SHM sensors for aerospace applications is a field of interest. Pearson et al [12] investigated using piezoelectric materials and TEGs to harvest ambient vibration and thermal gradients, respectively, present on aircraft. Simulation results utilizing temperature data taken from thermocouples placed at various positions on an aircraft ( Figure 12) yield peak Figure 12: Locations of thermocouples used for the TEG power output simulation [12].…”
Section: Thermal Energymentioning
confidence: 99%
“…Pearson et al [12] investigated using piezoelectric materials and TEGs to harvest ambient vibration and thermal gradients, respectively, present on aircraft. Simulation results utilizing temperature data taken from thermocouples placed at various positions on an aircraft ( Figure 12) yield peak Figure 12: Locations of thermocouples used for the TEG power output simulation [12]. power levels ranging from 5.46 to 34.15 mW depending on the location of the thermocouple as shown in Table 2 [12].…”
Section: Thermal Energymentioning
confidence: 99%
“…Engine and engine bay, auxiliary power unit, bleed system, electrical and hydraulic actuators, electronic systems, cabin lining and crown of an aircraft are the promising spots for the placement of a thermoelectric generator on an aircraft [4]. Our application deals with the utilization of aircraft engine case as a heat source.…”
Section: Introductionmentioning
confidence: 99%