HEAT EXCHANGER FOR AN AIRCRAFT
    1.
    发明公开

    公开(公告)号:US20240287934A1

    公开(公告)日:2024-08-29

    申请号:US18659339

    申请日:2024-05-09

    CPC classification number: F02C7/14 F05D2220/323 F05D2260/213 F05D2260/606

    Abstract: A heat exchanger for an aircraft includes an inlet plenum housing defining an inlet plenum configured to receive a fluid and an outlet plenum housing defining an outlet plenum configured to discharge the fluid. Furthermore, the heat exchanger includes a core configured to heat or cool a first portion of the fluid, with the core defining a plurality of fluid passages extending from the inlet plenum to the outlet plenum. Moreover, the heat exchanger includes a passive bypass defining a passive bypass flow path fluidly coupled to and extending between the inlet plenum and the outlet plenum. As such, the passive bypass flow path is in parallel with at least a portion of the core such that a second portion of the fluid bypasses at least a portion of the core and flows continuously and unobstructed through the passive bypass flow path to the outlet plenum.

    Heat exchanger for an aircraft
    3.
    发明授权

    公开(公告)号:US12006870B2

    公开(公告)日:2024-06-11

    申请号:US17117336

    申请日:2020-12-10

    CPC classification number: F02C7/14 F05D2220/323 F05D2260/213 F05D2260/606

    Abstract: A heat exchanger for an aircraft includes an inlet plenum housing defining an inlet plenum configured to receive a fluid and an outlet plenum housing defining an outlet plenum configured to discharge the fluid. Furthermore, the heat exchanger includes a core configured to heat or cool a first portion of the fluid, with the core defining a plurality of fluid passages extending from the inlet plenum to the outlet plenum. Moreover, the heat exchanger includes a passive bypass defining a passive bypass flow path fluidly coupled to and extending between the inlet plenum and the outlet plenum. As such, the passive bypass flow path is in parallel with at least a portion of the core such that a second portion of the fluid bypasses at least a portion of the core and flows continuously and unobstructed through the passive bypass flow path to the outlet plenum.

    HEAT EXCHANGER FOR AN AIRCRAFT
    4.
    发明申请

    公开(公告)号:US20220186664A1

    公开(公告)日:2022-06-16

    申请号:US17117336

    申请日:2020-12-10

    Abstract: A heat exchanger for an aircraft includes an inlet plenum housing defining an inlet plenum configured to receive a fluid and an outlet plenum housing defining an outlet plenum configured to discharge the fluid. Furthermore, the heat exchanger includes a core configured to heat or cool a first portion of the fluid, with the core defining a plurality of fluid passages extending from the inlet plenum to the outlet plenum. Moreover, the heat exchanger includes a passive bypass defining a passive bypass flow path fluidly coupled to and extending between the inlet plenum and the outlet plenum. As such, the passive bypass flow path is in parallel with at least a portion of the core such that a second portion of the fluid bypasses at least a portion of the core and flows continuously and unobstructed through the passive bypass flow path to the outlet plenum.

    TUBE IN CROSS-FLOW CONDUIT HEAT EXCHANGER
    6.
    发明申请
    TUBE IN CROSS-FLOW CONDUIT HEAT EXCHANGER 有权
    管道交流热交换器

    公开(公告)号:US20160265850A1

    公开(公告)日:2016-09-15

    申请号:US14656789

    申请日:2015-03-13

    Abstract: A heat exchanger that includes an input cavity defined by inlet cavity walls; a heat exchanger portion in fluid communication with the input cavity and defined between a first side and a second side, and wherein a plurality of baffles are positioned within the heat exchanger portion; and an outlet cavity in fluid communication with the heat exchanger portion and defined by outlet cavity walls. The heat exchanger portion comprises: a plurality of first fluid paths defined between the baffles and extending from the input cavity to the outlet cavity, and a plurality of tubes extending through the heat exchanger portion from the first side to the second side. Each tube extends through the baffles so as to define a second fluid path through the heat exchanger portion. Heat exchanger systems are also generally provided, along with methods for cooling a hot fluid input with a heat exchanger.

    Abstract translation: 一种热交换器,包括由入口腔壁限定的输入腔; 热交换器部分,其与所述输入腔流体连通并且限定在第一侧和第二侧之间,并且其中多个挡板定位在所述热交换器部分内; 以及与所述热交换器部分流体连通并由出口空腔壁限定的出口腔。 热交换器部分包括:限定在挡板之间并从输入腔延伸到出口空腔的多个第一流体通道,以及从第一侧延伸穿过热交换器部分到第二侧的多个管。 每个管延伸穿过挡板以限定通过热交换器部分的第二流体路径。 还通常提供热交换器系统,以及用于用热交换器冷却热流体输入的方法。

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