发明名称 Thermopile Generator for Airplanes and Other Applications
摘要 An airframe having an integrated thermoelectric generator and a method thereof for providing electricity in an aircraft. A plurality of thermocouple wires is disposed about an aircraft frame to form a thermopile circuit in which electrical current is generated as a result of a temperature difference observed at a cruising altitude. The temperature difference is created by a hot side, interior to the aircraft frame, and a cold side, exterior to the aircraft frame. The thermopile circuit is formed by a first thermoelectric material and a second thermoelectric material that are selected to produce a desired voltage when exposed to the temperature difference. The electric current is harnessed by a transfer cable and directed to an aircraft electrical system to provide power to the desired devices.
申请公布号 US2017057654(A1) 申请公布日期 2017.03.02
申请号 US201615256201 申请日期 2016.09.02
申请人 Elnahhas Mohamed Ahmed Abdelhalim 发明人 Elnahhas Mohamed Ahmed Abdelhalim
分类号 B64D41/00;H01L35/30;H01L35/32 主分类号 B64D41/00
代理机构 代理人
主权项 1. An airframe having an integrated thermoelectric generator comprises: an aircraft frame; a plurality of thermocouple wires; the plurality of thermocouple wires comprising a first thermoelectric material; the plurality of thermocouple wires being operably disposed about the aircraft frame in order to form a thermopile circuit; the first thermoelectric material being electrically connected to a second thermoelectric material; the thermopile circuit being formed in combination by the first thermoelectric material and the second thermoelectric material; and the first thermoelectric material and the second thermoelectric material being electrically connected to a step transformer, wherein the step transformer is electrically connected to an aircraft electrical system.
地址 Kuwait KW