Flight Test Results of a Thermoelectric Energy Harvester for Aircraft

被引:33
作者
Samson, D. [1 ]
Kluge, M. [1 ]
Fuss, T. [2 ]
Schmid, U. [3 ]
Becker, Th. [1 ]
机构
[1] EADS Innovat Works Sensors Elect & Syst Integrat, D-81663 Munich, Germany
[2] Philotech GmbH, D-21614 Buxtehude, Germany
[3] Vienna Univ Technol, Dept Microsyst Technol, Inst Sensor & Actuator Syst, A-1040 Vienna, Austria
关键词
Energy harvesting; thermoelectric generator; flight test; aircraft operation envelope; vibration and temperature test;
D O I
10.1007/s11664-012-1928-6
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
The idea of thermoelectric energy harvesting for low-power wireless sensor systems in aircraft and its practical implementation was recently published. The concept of using a thermoelectric generator (TEG) attached to the aircraft inner hull and a thermal storage device to create an artificial temperature gradient at the TEG during take-off and landing from the temperature changes of the fuselage has passed initial tests and is now subject to flight testing. This work presents preflight test results, e.g., vibration and temperature testing of the harvesters, the practical installation of two harvesting devices inside a test plane, and the first test flight results. Several flight cycles with different flight profiles, flight lengths, and outside temperatures have been performed. Although the influence of different flight profiles on the energy output of the harvester can be clearly observed, the results are in good agreement with expectations from numerical simulations with boundary conditions evaluated from initial climate chamber experiments. In addition, the flight test demonstrates that reliable operation of thermoelectric energy harvesting in harsh aircraft environments seems to be feasible, therefore paving the way for realization of energy-autonomous, wireless sensor networks.
引用
收藏
页码:1134 / 1137
页数:4
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