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,复合机翼和复合机翼SPAR

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量的热管理系统(10)包括支撑热负荷源(24)的至少一个复合结构构件(22)和与至少一种复合物热接触的热传递构件(12)构件(22)并且与散热器(23)热接触。系统(10)还包括至少一个导热第一紧固件(30),该第一紧固件与传热构件(12)热接触并将热负载源(24)耦合到至少一个复合结构构件(22)。 )。至少一个第一紧固件(30)将热量从热负荷源(24)传导到热传递构件(12)中。传热部件(12)将热从导热性第一紧固件(30)传导至散热器(23)。

著录项

  • 公开/公告号EP3409578A1

    专利类型

  • 公开/公告日2018-12-05

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20180165160

  • 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;

  • 国家 EP

  • 入库时间 2022-08-21 12:25:44

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