SHAPE MORPHING FINS FOR FROST REMOVAL
    1.
    发明公开

    公开(公告)号:US20240102751A1

    公开(公告)日:2024-03-28

    申请号:US18531562

    申请日:2023-12-06

    IPC分类号: F28F17/00

    CPC分类号: F28F17/00 F28F19/006

    摘要: A shape-morphing fin includes a fixed portion, a multistable portion, a coupling portion, and a vibration source. The multistable portion functions as a negative stiffness element. The multistable portion is selectively movable between a first position and a second position. The movement between first position and the second position is configured to remove the ice formation from the structure. The coupling portion couples the fixed portion to the multistable portion. The vibration source is configured to produce a resonant vibration to engage the movement of the multistable portion from the first position to the second position.

    GAS TURBINE INLET HAVING INTEGRATED COILS AND MIST REDUCING VANES
    8.
    发明申请
    GAS TURBINE INLET HAVING INTEGRATED COILS AND MIST REDUCING VANES 审中-公开
    具有集成线圈和减雾器的气体涡轮机入口

    公开(公告)号:US20150308338A1

    公开(公告)日:2015-10-29

    申请号:US14117661

    申请日:2013-01-11

    IPC分类号: F02C7/12 F01D25/32

    摘要: An integrated coil and fin system in a gas turbine inlet. The integrated system includes at least one wavy, non-planar, fin integrated with at least one heating/cooling coil, wherein the at least one coil is configured to heat or cool air moving through the gas turbine inlet, and wherein the at least one non-planar fin is configured to remove moisture in the air moving through the gas turbine inlet. In one embodiment, at least one hook can be included at an end or along a length of at least one non-planar fin.

    摘要翻译: 燃气轮机入口中的集成线圈和翅片系统。 集成系统包括与至少一个加热/冷却盘管集成的至少一个波浪形非平面翅片,其中至少一个线圈构造成加热或冷却通过燃气轮机入口移动的空气,并且其中至少一个 非平面翅片构造成去除移动通过燃气轮机入口的空气中的水分。 在一个实施例中,至少一个钩可以包括在至少一个非平面翅片的一端或一段长度上。

    GAS TURBINE ENGINE HEAT EXCHANGERS AND METHODS OF ASSEMBLING THE SAME
    10.
    发明申请
    GAS TURBINE ENGINE HEAT EXCHANGERS AND METHODS OF ASSEMBLING THE SAME 审中-公开
    气体涡轮发动机热交换器及其组装方法

    公开(公告)号:US20140044525A1

    公开(公告)日:2014-02-13

    申请号:US13912897

    申请日:2013-06-07

    IPC分类号: F01D25/12 F28F27/02

    摘要: A heat exchanger assembly for use in a gas turbine engine includes a bypass valve and at least one body portion. The body portion includes at least one de-congealing inlet channel in flow communication with the bypass valve, a plurality of cooling channels in flow communication with the bypass valve and the at least one de-congealing inlet channel, and at least one de-congealing outlet channel in flow communication with the bypass valve and the at least one de-congealing inlet channel. The bypass valve is configured to deliver a fluid between the at least one de-congealing inlet channel and the plurality of cooling channels during a first mode of operation to facilitate reducing a temperature of the fluid. The bypass valve is further configured to deliver the fluid between the at least one de-congealing inlet channel and the at least one de-congealing outlet channel during a second mode of operation.

    摘要翻译: 用于燃气涡轮发动机的热交换器组件包括旁通阀和至少一个主体部分。 主体部分包括与旁通阀流动连通的至少一个去凝结入口通道,与旁通阀和至少一个去凝固入口通道流动连通的多个冷却通道,以及至少一个去凝固 出口通道与旁通阀和至少一个去凝结入口通道流体连通。 旁通阀构造成在第一操作模式期间在至少一个去凝结入口通道和多个冷却通道之间输送流体,以有助于降低流体的温度。 旁通阀进一步构造成在第二操作模式期间在至少一个去凝结入口通道和至少一个去凝结出口通道之间输送流体。