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    HEAT EXCHANGER WITH SLOTTED GUARD FIN
    2.
    发明申请
    HEAT EXCHANGER WITH SLOTTED GUARD FIN 审中-公开
    热交换器带有保护盖

    公开(公告)号：US20160025425A1

    公开(公告)日：2016-01-28

    申请号：US14340632

    申请日：2014-07-25

    Applicant: HAMILTON SUNDSTRAND CORPORATION

    Inventor： Donald E. Army, JR. ,  George Kan ,  Michael Spineti ,  Kurt L. Stephens ,  Michael Zager

    IPC: F28F3/02 ,  B23P15/26

    CPC classification number: F28F3/02 ,  B23P15/26 ,  F28D9/0068 ,  F28D9/0093 ,  F28D2021/0026 ,  F28F2215/04 ,  F28F2265/26

    Abstract: In one aspect, a plate fin heat exchanger is provided. The heat exchanger includes a plurality of finned cold layers configured to conduct a first fluid and a plurality of finned warm layers configured to conduct a second fluid. The finned warm layers include an inlet side, an outlet side, a first portion of fins at the inlet side, and a second portion of fins at the outlet side. The fins of the first portion of fins have a thickness greater than a thickness of the fins of the second portion of fins

    Abstract translation: 一方面，提供了一种板翅式热交换器。 热交换器包括多个翅片冷层，其被配置为传导第一流体和多个鳍状暖层，构造成导入第二流体。 翅片暖层包括入口侧，出口侧，入口侧的翅片的第一部分和出口侧的翅片的第二部分。 翅片的第一部分的翅片的厚度大于翅片的第二部分的翅片的厚度

    Heat exchanger for aircraft application
    4.
    发明授权
    Heat exchanger for aircraft application 有权
    飞机用热交换器

    公开(公告)号：US09157683B2

    公开(公告)日：2015-10-13

    申请号：US13854999

    申请日：2013-04-02

    Applicant: HAMILTON SUNDSTRAND CORPORATION

    Inventor： Michael Doe ,  Brian R. Shea ,  Kurt L. Stephens ,  Matthew William Miller ,  Michael Zager ,  Irving C. Ostrander

    IPC: H05K7/20 ,  F28B1/00

    CPC classification number: F28B1/00 ,  F28D1/05391 ,  F28D15/00 ,  F28D2021/0021 ,  F28D2021/0031 ,  F28F1/022 ,  F28F2260/02

    Abstract: A heat exchanger includes a plurality of mini-channel tubes. The mini-channel tubes extends for an axial length defined between two manifolds. The mini-channel tubes include a plurality of generally rectangular flow passages. The generally rectangular flow passages are aligned adjacent to each other to define a lateral dimension. A first lateral width of the generally rectangular passages is defined with a ratio of the axial length to the first lateral width being between 201.3 and 215.3. An aircraft system is also disclosed.

    Abstract translation: 热交换器包括多个微通道管。 微通道管延伸到两个歧管之间限定的轴向长度。 迷你通道管包括多个大致矩形的流动通道。 大致矩形的流动通道彼此相邻排列以限定横向尺寸。 大致矩形通道的第一横向宽度被限定为轴向长度与第一横向宽度的比率在201.3和215.3之间。 还公开了一种飞机系统。

    PLATE FIN HEAT EXCHANGER
    6.
    发明申请
    PLATE FIN HEAT EXCHANGER 审中-公开
    板式热交换器

    公开(公告)号：US20160369698A1

    公开(公告)日：2016-12-22

    申请号：US14743778

    申请日：2015-06-18

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Donald E. Army, JR. ,  Michael Doe, JR. ,  Kurt L. Stephens

    IPC: F02C7/18 ,  F28D1/03

    CPC classification number: F02C7/185 ,  F28D1/0383 ,  F28D9/0062 ,  F28D9/0068 ,  F28D2021/0021 ,  F28F3/025

    Abstract: A plate fin heat exchanger is disclosed. The heat exchanger includes a plurality of plates defining a set of hot fluid passages between adjacent plates of the plurality of plates and a set of cold fluid passages between adjacent plates of the plurality of plates. A hot fluid inlet and outlet are located at a first face of the heat exchanger. A barrier is located between adjacent plates defining the hot fluid passages. The barrier extends between the adjacent plates and extends from the first face of the heat exchanger at a location between the hot fluid inlet and the hot fluid outlet in a direction perpendicular to the first face, and defines a first pass of hot fluid passages on a first side of the barrier and a second pass of hot fluid passages on a second side of the barrier.

    Abstract translation: 公开了一种板翅式热交换器。 热交换器包括多个板，其在多个板的相邻板之间限定一组热流体通道，以及在多个板的相邻板之间的一组冷流体通道。 热流体入口和出口位于热交换器的第一面。 挡板位于限定热流体通道的相邻板之间。 阻挡层在相邻板之间延伸并且在垂直于第一面的方向上从热交换器的第一面在热流体入口与热流体出口之间的位置处延伸，并且在第一面上限定热流体通道 阻挡层的第一侧和在阻挡层的第二侧上的热流体通道的第二次通过。

    COOLING TUBE INCLUDED IN AIRCRAFT HEAT EXCHANGER
    7.
    发明申请
    COOLING TUBE INCLUDED IN AIRCRAFT HEAT EXCHANGER 审中-公开
    冷却管包括在飞机热交换器中

    公开(公告)号：US20140299303A1

    公开(公告)日：2014-10-09

    申请号：US13856749

    申请日：2013-04-04

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Michael Doe ,  Brian R. Shea ,  Kurt L. Stephens ,  Michael Zager ,  Matthew William Miller ,  Irving C. Ostrander

    IPC: F28F1/00

    CPC classification number: F28D7/1615 ,  F28D7/1653 ,  F28D7/1684 ,  F28D2021/0021 ,  F28F1/022

    Abstract: A channel tube includes a body having first and second surfaces extending between first and second opposing ends to define a tube width. The first and second surfaces are separated from each other by a distance defining a tube height. A plurality of ports extend through the body and between the first and second surfaces to define a fluid path extending in a direction of the tube width. Each port defines a plurality of walls and a plurality of ribs having a thermal conductive surface to transfer heat therethrough. A first wall extends in a direction of the tube width. The second wall extends in a direction of the tube width and is disposed opposite the first wall. At least one rib is integrally formed between the first and second walls and extends perpendicular thereto.

    Abstract translation: 通道管包括具有在第一和第二相对端之间延伸以限定管宽度的第一和第二表面的主体。 第一和第二表面彼此隔开限定管高度的距离。 多个端口延伸穿过主体并且在第一和第二表面之间延伸以限定在管宽度的方向上延伸的流体路径。 每个端口限定多个壁和多个具有导热表面以传递热量的肋。 第一壁沿管宽方向延伸。 第二壁沿管宽度的方向延伸并且设置成与第一壁相对。 至少一个肋一体地形成在第一和第二壁之间并且垂直于其延伸。

    Heat Exchanger for Aircraft Application
    8.
    发明申请
    Heat Exchanger for Aircraft Application 有权
    飞机应用换热器

    公开(公告)号：US20140293540A1

    公开(公告)日：2014-10-02

    申请号：US13854999

    申请日：2013-04-02

    Applicant: HAMILTON SUNDSTRAND CORPORATION

    Inventor： Michael Doe ,  Brian R. Shea ,  Kurt L. Stephens ,  Matthew William Miller ,  Michael Zager ,  Irving C. Ostrander

    IPC: H05K7/20

    CPC classification number: F28B1/00 ,  F28D1/05391 ,  F28D15/00 ,  F28D2021/0021 ,  F28D2021/0031 ,  F28F1/022 ,  F28F2260/02

    Abstract: A heat exchanger includes a plurality of mini-channel tubes. The mini-channel tubes extends for an axial length defined between two manifolds. The mini-channel tubes include a plurality of generally rectangular flow passages. The generally rectangular flow passages are aligned adjacent to each other to define a lateral dimension. A first lateral width of the generally rectangular passages is defined with a ratio of the axial length to the first lateral width being between 201.3 and 215.3. An aircraft system is also disclosed.

    Abstract translation: 热交换器包括多个微通道管。 微通道管延伸到两个歧管之间限定的轴向长度。 迷你通道管包括多个大致矩形的流动通道。 大致矩形的流动通道彼此相邻排列以限定横向尺寸。 大致矩形通道的第一横向宽度被限定为轴向长度与第一横向宽度的比率在201.3和215.3之间。 还公开了一种飞机系统。

    Plate fin heat exchanger
    9.
    发明授权
    Plate fin heat exchanger 有权

    公开(公告)号：US10954858B2

    公开(公告)日：2021-03-23

    申请号：US14743778

    申请日：2015-06-18

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Donald E. Army, Jr. ,  Michael Doe, Jr. ,  Kurt L. Stephens

    IPC: F02C7/00 ,  F02C7/18 ,  F28F3/02 ,  F28D9/00 ,  F28D1/03 ,  F28D21/00

    Abstract: A plate fin heat exchanger is disclosed. The heat exchanger includes a plurality of plates defining a set of hot fluid passages between adjacent plates of the plurality of plates and a set of cold fluid passages between adjacent plates of the plurality of plates. A hot fluid inlet and outlet are located at a first face of the heat exchanger. A barrier is located between adjacent plates defining the hot fluid passages. The barrier extends between the adjacent plates and extends from the first face of the heat exchanger at a location between the hot fluid inlet and the hot fluid outlet in a direction perpendicular to the first face, and defines a first pass of hot fluid passages on a first side of the barrier and a second pass of hot fluid passages on a second side of the barrier.

    HEAT EXCHANGER WITH FIN WAVE CONTROL
    10.
    发明申请
    HEAT EXCHANGER WITH FIN WAVE CONTROL 审中-公开
    带有波形控制的热交换器

    公开(公告)号：US20160195342A1

    公开(公告)日：2016-07-07

    申请号：US14591285

    申请日：2015-01-07

    Applicant: HAMILTON SUNDSTRAND CORPORATION

    Inventor： Donald E. Army, JR. ,  George Kan ,  Kurt L. Stephens ,  Michael Spineti ,  Michael Zager

    IPC: F28F3/02 ,  B23P15/26 ,  B23H1/00 ,  F28F3/04

    Abstract: A plate fin heat exchanger includes a plurality of finned cold layers configured to conduct a first fluid, and a plurality of finned warm layers configured to conduct a second fluid. The finned warm layers include an inlet side and an outlet side. A first portion of fins of at least one finned warm layer of the plurality of finned warm layers includes a plurality of aligned peaks and valleys defining a wave configuration for each fin of the first portion of fins. An upstream leading edge of the first portion of fins begins at a point of the wave configuration that is at least one of the peaks and valleys.

    Abstract translation: 板翅式热交换器包括构造成导入第一流体的多个翅片冷层，以及被配置为导入第二流体的多个翅片暖层。 翅片暖层包括入口侧和出口侧。 多个翅片暖层中的至少一个翅片暖层的翅片的第一部分包括限定鳍片的第一部分的每个翅片的波形构型的多个对准的峰和谷。 翅片的第一部分的上游前缘开始于波形配置的至少一个峰和谷的点。

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