GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM
    1.
    发明申请
    GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM 有权
    气体涡轮发动机热管理系统

    公开(公告)号:US20130104559A1

    公开(公告)日:2013-05-02

    申请号:US13285454

    申请日:2011-10-31

    IPC分类号: F02C7/141 F01P9/00 F02C3/00

    摘要: A thermal management system for a gas turbine engine includes a first heat exchanger that provides a first conditioned fluid, a second heat exchanger in series flow communication with the first heat exchanger and that exchanges heat with the first conditioned fluid to provide a second conditioned fluid, and a third heat exchanger in parallel flow communication with the second heat exchanger and that selectively exchanges heat with the first conditioned fluid to provide a third conditioned fluid. The second conditioned fluid and the third conditioned fluid combine to provide a mixed conditioned fluid. A first portion of the mixed conditioned fluid including a first temperature is communicated to a first engine system. A second portion of the mixed conditioned fluid including a second temperature is communicated to a second engine system. The second temperature includes a greater temperature than the first temperature.

    摘要翻译: 用于燃气涡轮发动机的热管理系统包括提供第一调节流体的第一热交换器,与第一热交换器串联流动连通的第二热交换器,并与第一调节流体交换热量以提供第二调节流体, 以及与所述第二热交换器并联流动连通的第三热交换器,并且与所述第一调节流体选择性地交换热量以提供第三调节流体。 第二调理流体和第三调理流体组合以提供混合的调节流体。 包括第一温度的混合调节流体的第一部分被传送到第一发动机系统。 包括第二温度的混合调节流体的第二部分被传递到第二发动机系统。 第二温度包括比第一温度更高的温度。

    Geared turbomachine fluid delivery system
    2.
    发明授权
    Geared turbomachine fluid delivery system 有权
    齿轮涡轮机输液系统

    公开(公告)号:US08257024B1

    公开(公告)日:2012-09-04

    申请号:US13359897

    申请日:2012-01-27

    IPC分类号: F01D25/18

    摘要: An exemplary geared turbomachine fluid delivery system includes a first fluid path configured to communicate fluid from a supply to a gear system of a geared turbomachine, and a second fluid path configured to communicate fluid from the supply to the gear system. The fluid introduced to the gear system by the first fluid path is cooler than that the fluid introduced to the gear system by the second fluid path.

    摘要翻译: 示例性的齿轮涡轮机输送系统包括被配置为将流体从供应件传递到齿轮传动涡轮机的齿轮系统的第一流体路径和被配置为将流体从供应件传递到齿轮系统的第二流体路径。 通过第一流体路径引入齿轮系统的流体比通过第二流体路径引入齿轮系统的流体更冷。

    Gas turbine engine thermal management system
    4.
    发明授权
    Gas turbine engine thermal management system 有权
    燃气轮机发动机热管理系统

    公开(公告)号:US08495857B2

    公开(公告)日:2013-07-30

    申请号:US13285454

    申请日:2011-10-31

    IPC分类号: F02C7/06 F02C1/00 F02K99/00

    摘要: A thermal management system for a gas turbine engine includes a first heat exchanger that provides a first conditioned fluid, a second heat exchanger in series flow communication with the first heat exchanger and that exchanges heat with the first conditioned fluid to provide a second conditioned fluid, and a third heat exchanger in parallel flow communication with the second heat exchanger and that selectively exchanges heat with the first conditioned fluid to provide a third conditioned fluid. The second conditioned fluid and the third conditioned fluid combine to provide a mixed conditioned fluid. A first portion of the mixed conditioned fluid including a first temperature is communicated to a first engine system. A second portion of the mixed conditioned fluid including a second temperature is communicated to a second engine system. The second temperature includes a greater temperature than the first temperature.

    摘要翻译: 用于燃气涡轮发动机的热管理系统包括提供第一调节流体的第一热交换器,与第一热交换器串联流动连通的第二热交换器,并与第一调节流体交换热量以提供第二调节流体, 以及与所述第二热交换器并联流动连通的第三热交换器,并且与所述第一调节流体选择性地交换热量以提供第三调节流体。 第二调理流体和第三调理流体组合以提供混合的调节流体。 包括第一温度的混合调节流体的第一部分被传送到第一发动机系统。 包括第二温度的混合调节流体的第二部分被传递到第二发动机系统。 第二温度包括比第一温度更高的温度。

    HEAT EXCHANGER
    5.
    发明申请
    HEAT EXCHANGER 有权
    热交换器

    公开(公告)号:US20130192254A1

    公开(公告)日:2013-08-01

    申请号:US13360745

    申请日:2012-01-29

    IPC分类号: F02C6/08

    摘要: A gas turbine engine has a fan, a compressor section, a combustor, and a turbine section. The fan delivers a portion of air into the compressor, and into a duct, as bypass air. A bleed air system bleeds a quantity of air from the compressor into a chamber at least at low power conditions of the engine. The bleed air system has an opening which may be selectively closed to block bleed air, or opened to allow bleed flow from the compressor into the chamber. A heat exchanger is positioned such that a first surface of the heat exchanger is contacted by bypass air in the duct, and a second surface of the heat exchanger is contacted by bleed air when the bleed air system directs air from the compressor into the chamber.

    摘要翻译: 燃气涡轮发动机具有风扇,压缩机部,燃烧器和涡轮部。 风扇将一部分空气输送到压缩机中,并作为旁路空气进入管道。 排气系统至少在发动机的低功率条件下将一定数量的空气从压缩机排出到室内。 排气系统具有可以选择性地关闭以阻止排出空气的开口,或者打开以允许从压缩机流入室中的流出。 热交换器被定位成使得热交换器的第一表面与管道中的旁路空气接触,并且当排气系统将空气从压缩机引导到室中时,热交换器的第二表面与排气接触。

    Heat exchanger
    6.
    发明授权
    Heat exchanger 有权
    热交换器

    公开(公告)号:US09267434B2

    公开(公告)日:2016-02-23

    申请号:US13360745

    申请日:2012-01-29

    摘要: A gas turbine engine has a fan, a compressor section, a combustor, and a turbine section. The fan delivers a portion of air into the compressor, and into a duct, as bypass air. A bleed air system bleeds a quantity of air from the compressor into a chamber at least at low power conditions of the engine. The bleed air system has an opening which may be selectively closed to block bleed air, or opened to allow bleed flow from the compressor into the chamber. A heat exchanger is positioned such that a first surface of the heat exchanger is contacted by bypass air in the duct, and a second surface of the heat exchanger is contacted by bleed air when the bleed air system directs air from the compressor into the chamber.

    摘要翻译: 燃气涡轮发动机具有风扇,压缩机部,燃烧器和涡轮部。 风扇将一部分空气输送到压缩机中,并作为旁路空气进入管道。 排气系统至少在发动机的低功率条件下将一定数量的空气从压缩机排出到室内。 排气系统具有可以选择性地关闭以阻止排出空气的开口,或者打开以允许从压缩机流入室中的流出。 热交换器被定位成使得热交换器的第一表面与管道中的旁路空气接触,并且当排气系统将空气从压缩机引导到室中时,热交换器的第二表面与排气接触。