The invention relates to a highly flexible thermoelectric composite for sensing temperature in an aircraft. The present invention relates to apparatus, systems and methods for using at least one highly flexible thermoelectric device placed in contact with and/or adjacent to a surface of a heat dissipating aircraft component for the purpose of collecting and/or converting energy in the form of heat to thereby generate an electrical current for powering the aircraft component.
本发明涉及用于在飞行器中感测温度的高柔性热电复合材料。涉及用于使用至少一个高柔性热电装置的装备、系统和方法,该高柔性热电装置放置为与散热飞行器组件表面接触和/或邻近,目的是收集和/或转换热量形式的能量,从而产生用于为飞行器部件供电的电流。
Highly flexible thermoelectric composite for sensing temperature in aircraft
用于在飞行器中感测温度的高柔性热电复合材料
2025-03-28
Patent
Electronic Resource
Chinese
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