发明名称 Fully integrated thermoelectric devices and their application to aerospace de-icing systems
摘要 A thermoelectric module and methods for making and applying same provide an integrated, layered structure comprising first and second, thermally conductive, surface volumes, each in thermal communication with a separate respective first and second electrically conductive patterned trace layers, and an array of n-type and p-type semiconducting elements embedded in amorphous silica dielectric and electrically connected between the first and second patterned trace layers forming a thermoelectric circuit.
申请公布号 US9490414(B2) 申请公布日期 2016.11.08
申请号 US201213602019 申请日期 2012.08.31
申请人 de Rochemont L. Pierre 发明人 de Rochemont L. Pierre
分类号 F25B21/02;H01L35/34;H01L35/32;H01L35/18;H01L35/30;B64D15/12 主分类号 F25B21/02
代理机构 Burns & Levinson, LLP 代理人 Burns & Levinson, LLP ;Gomes David W.;Cohen Jerry
主权项 1. A microelectronic circuit module comprising: a heat producing semiconductor chip mounted on a packaging element that has micro-channels through which a working fluid is passed to collect and transfer heat from the semiconductor chip; a thermoelectric module comprising a network of micro-channels embedded within silica dielectric through which the heated working fluid is circulated; and a first thermally isolated thermoelectric circuit embedded within silica dielectric that consists of a linear array of MAX-phase electrodes interleaved between alternating n-type and p-type semiconducting elements, wherein the MAX-phase electrodes contain micro-channels through which the working fluid is circulated and progressively cooled.
地址 Austin TX US