首页> 外国专利> A THERMAL MANAGEMENT SYSTEM, A COMPOSITE WING, AND A COMPOSITE WING SPAR

A THERMAL MANAGEMENT SYSTEM, A COMPOSITE WING, AND A COMPOSITE WING SPAR

机译:热管理系统,复合翼和复合翼翼梁

摘要

A thermal management system (10) for transferring heat from a heat load includes at least one composite structural member (22) that supports a heat load source (24) and a heat transfer member (12) in thermal contact with the at least one composite structural member (22) and in thermal contact with a heat sink (23). The system (10) further includes at least one thermally-conductive first fastener (30) that is in thermal contact with the heat transfer member (12) and couples the heat load source (24) to the at least one composite structural member (22). The at least one first fastener (30) conducts heat from the heat load source (24) into the heat transfer member (12). The heat transfer member (12) conducts heat from the thermally-conductive first fastener (30) to the heat sink (23).
机译:用于从热负荷传递热的热管理系统(10)包括至少一个复合结构构件(22),其在热载源(24)和传热构件(12)与至少一个复合材料的热接触中结构构件(22)和与散热器(23)的热接触。系统(10)还包括至少一个导热性第一紧固件(30),其与传热构件(12)热接触,并将热负荷源(24)耦合到所述至少一个复合结构构件(22 )。所述至少一个第一紧固件(30)将热来自热负荷源(24)传导到传热构件(12)中。传热构件(12)从导热的第一紧固件(30)传导热量到散热器(23)。

著录项

  • 公开/公告号EP3792175A1

    专利类型

  • 公开/公告日2021-03-17

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20200197832

  • 发明设计人 WHITE EDWARD V.;

    申请日2018-03-29

  • 分类号B64C1/40;B64D13;B64G1/50;B64C3/18;B64C3/26;B64C1;B64C13/50;B64C9;B32B27/06;B32B5/24;B32B7/08;B32B5/18;

  • 国家 EP

  • 入库时间 2022-08-24 17:45:04

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