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 |