Thermal management system for an aircraft
    1.
    发明授权
    Thermal management system for an aircraft 有权
    飞机热管理系统

    公开(公告)号:US07260926B2

    公开(公告)日:2007-08-28

    申请号:US10760663

    申请日:2004-01-20

    IPC分类号: F02K7/224 F02K7/22 F02K7/236

    摘要: A fuel based thermal management system includes a fuel stabilization system which permits the fuel to exceed the traditional coking temperatures. High temperature components are arranged along the fuel flow path such that even at the higher operating temperatures the fuel operates as a heat sink to transfer heat from high temperature components to the fuel. An optimal high temperature ester-based oil permits an oil-loop to exceed current oil temperature limits and achieve a high temperature to permit efficient rejection of heat to the fuel late in the fuel flow path.

    摘要翻译: 基于燃料的热管理系统包括允许燃料超过传统焦化温度的燃料稳定系统。 高温部件沿着燃料流动路径布置,使得即使在更高的操作温度下,燃料作为散热器工作,以将热量从高温部件传递到燃料。 最佳的高温酯基油允许油循环超过当前的油温限制并实现高温以允许在燃料流动路径中晚期有效地排出燃料到燃料。