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    HEAT TRANSFER DEVICES
    1.
    发明申请
    HEAT TRANSFER DEVICES 有权
    换热装置

    公开(公告)号：US20130112374A1

    公开(公告)日：2013-05-09

    申请号：US13289307

    申请日：2011-11-04

    申请人： Thomas M. Murray ,  Edward Zielinski

    发明人： Thomas M. Murray ,  Edward Zielinski

    IPC分类号： F28D15/04 ,  F28F1/00

    CPC分类号： B64D33/12 ,  B64G1/506

    摘要： Heat transfer devices are described. In one example, a heat transfer device for installation in a system having a heat generating element within the system away from which heat is to be transferred is described. The heat transfer device includes a heat pipe having a first portion, a second portion, and a working fluid contained within the heat pipe for transferring heat from the first portion to the second portion. The first portion is disposed in proximity with the heat generating element. The second portion is coupled to the first portion. At least part of the second portion is disposed outside the system to dissipate heat from the heat generating element and the second portion may be variably extended outside the system.

    摘要翻译： 描述了传热装置。 在一个示例中，描述了一种用于安装在系统内的传热装置，其中系统内的发热元件远离热量将被传送。 传热装置包括：热管，其具有第一部分，第二部分和包含在热管内的工作流体，用于将热量从第一部分传递到第二部分。 第一部分设置在发热元件附近。 第二部分耦合到第一部分。 第二部分的至少一部分设置在系统外部以散发来自发热元件的热​​量，并且第二部分可以可变地延伸到系统外部。

    Composite heat shield
    3.
    发明授权
    Composite heat shield 有权
    复合隔热罩

    公开(公告)号：US07927686B2

    公开(公告)日：2011-04-19

    申请号：US12170789

    申请日：2008-07-10

    申请人： Edward Zielinski ,  Thomas J. Connelly

    发明人： Edward Zielinski ,  Thomas J. Connelly

    IPC分类号： B32B3/00 ,  B32B3/12 ,  B64C1/10 ,  B64C1/00 ,  B64D7/00

    CPC分类号： B64D33/04 ,  B64C7/02 ,  B64D29/02 ,  B64G1/58 ,  Y10T428/1314 ,  Y10T428/1317 ,  Y10T428/234 ,  Y10T428/24562 ,  Y10T428/24661

    摘要： A composite heat shield includes a ceramic composite heat shield body comprising a pair of generally spaced-apart heat shield side panels, a heat shield bottom panel extending between the heat shield side panels and having a heat exposure surface, a heat shield top panel extending between the heat shield side panels in spaced-apart relationship with respect to the heat shield bottom panel and having at least one heat shield surface and at least one heat shield cavity defined between the heat shield bottom panel and the heat shield top panel.

    摘要翻译： 复合隔热罩包括陶瓷复合隔热罩体，该陶瓷复合隔热罩主体包括一对大致隔开的隔热屏侧板，在隔热屏侧面板之间延伸并具有热曝露表面的隔热罩底板， 所述隔热罩侧板相对于所述隔热罩底板间隔开，并且具有至少一个隔热表面和限定在所述隔热罩底板和所述隔热罩顶板之间的至少一个隔热罩。

    Heat exchanger systems and associated systems and methods for cooling aircraft starter/generators
    4.
    发明授权
    Heat exchanger systems and associated systems and methods for cooling aircraft starter/generators 有权
    热交换器系统及相关系统和方法，用于冷却飞机启动器/发电机

    公开(公告)号：US07883053B2

    公开(公告)日：2011-02-08

    申请号：US12244595

    申请日：2008-10-02

    申请人： Edward Zielinski ,  Thomas M. Murray

    发明人： Edward Zielinski ,  Thomas M. Murray

    IPC分类号： B64D33/10

    CPC分类号： F28D7/0066 ,  B64D13/00 ,  F28D1/0435 ,  F28D7/0083 ,  F28D2021/0021 ,  Y02T50/44 ,  Y02T50/56

    摘要： Heat exchanger systems and associated systems and methods for cooling aircraft starters/generators are disclosed. A system in accordance with one embodiment includes a first fluid flow path for a first fluid, a second fluid flow path for a second fluid, and a third fluid flow path for a third fluid. The first and second flow paths are positioned proximate to the third flow path to transfer heat between the third fluid and both the first and second fluids. The third flow path is configured to allow a transfer of heat between the second and third fluids at a first transfer rate when the first fluid carries heat at a first rate, and at a second transfer rate different than the first transfer rate when the first fluid does not carry heat, or carries heat at a second rate less than the first rate. Accordingly, when the heat to be rejected by one fluid is decreased, the heat transfer rate for the remaining fluid can be increased.

    摘要翻译： 公开了用于冷却飞机起动器/发电机的热交换器系统和相关系统和方法。 根据一个实施例的系统包括用于第一流体的第一流体流动路径，用于第二流体的第二流体流动路径和用于第三流体的第三流体流动路径。 第一和第二流动路径定位成靠近第三流动路径，以在第三流体和第一和第二流体两者之间传递热量。 第三流动路径被配置为当第一流体以第一速率承载热量时以第一流体的速率传递第二流体和第三流体之间的热量，并且当第一流体 不携带热量，或以低于第一速率的第二速率承载热量。 因此，当由一种流体排出的热量降低时，可以增加剩余流体的传热速率。

    Composite Heat Shield
    5.
    发明申请
    Composite Heat Shield 有权
    复合热盾

    公开(公告)号：US20090098321A1

    公开(公告)日：2009-04-16

    申请号：US12170789

    申请日：2008-07-10

    申请人： Edward Zielinski ,  Thomas J. Connelly

    发明人： Edward Zielinski ,  Thomas J. Connelly

    IPC分类号： B32B3/10

    CPC分类号： B64D33/04 ,  B64C7/02 ,  B64D29/02 ,  B64G1/58 ,  Y10T428/1314 ,  Y10T428/1317 ,  Y10T428/234 ,  Y10T428/24562 ,  Y10T428/24661

    摘要： A composite heat shield includes a ceramic composite heat shield body comprising a pair of generally spaced-apart heat shield side panels, a heat shield bottom panel extending between the heat shield side panels and having a heat exposure surface, a heat shield top panel extending between the heat shield side panels in spaced-apart relationship with respect to the heat shield bottom panel and having at least one heat shield surface and at least one heat shield cavity defined between the heat shield bottom panel and the heat shield top panel.

    摘要翻译： 复合隔热罩包括陶瓷复合隔热罩体，该陶瓷复合隔热罩主体包括一对大致隔开的隔热屏侧板，在隔热屏侧面板之间延伸并具有热曝露表面的隔热罩底板， 所述隔热罩侧板相对于所述隔热罩底板间隔开，并且具有至少一个隔热表面和限定在所述隔热罩底板和所述隔热罩顶板之间的至少一个隔热罩。

    Heat Exchanger Systems and Associated Systems and Methods for Cooling Aircraft Starter/Generators
    6.
    发明申请
    Heat Exchanger Systems and Associated Systems and Methods for Cooling Aircraft Starter/Generators 有权
    热交换器系统及相关系统和方法用于冷却飞机启动器/发电机

    公开(公告)号：US20090025913A1

    公开(公告)日：2009-01-29

    申请号：US12244595

    申请日：2008-10-02

    申请人： Edward Zielinski ,  Thomas M. Murray

    发明人： Edward Zielinski ,  Thomas M. Murray

    IPC分类号： F28D7/10

    CPC分类号： F28D7/0066 ,  B64D13/00 ,  F28D1/0435 ,  F28D7/0083 ,  F28D2021/0021 ,  Y02T50/44 ,  Y02T50/56

    摘要： Heat exchanger systems and associated systems and methods for cooling aircraft starters/generators are disclosed. A system in accordance with one embodiment includes a first fluid flow path for a first fluid, a second fluid flow path for a second fluid, and a third fluid flow path for a third fluid. The first and second flow paths are positioned proximate to the third flow path to transfer heat between the third fluid and both the first and second fluids. The third flow path is configured to allow a transfer of heat between the second and third fluids at a first transfer rate when the first fluid carries heat at a first rate, and at a second transfer rate different than the first transfer rate when the first fluid does not carry heat, or carries heat at a second rate less than the first rate. Accordingly, when the heat to be rejected by one fluid is decreased, the heat transfer rate for the remaining fluid can be increased.

    摘要翻译： 公开了用于冷却飞机起动器/发电机的热交换器系统和相关系统和方法。 根据一个实施例的系统包括用于第一流体的第一流体流动路径，用于第二流体的第二流体流动路径和用于第三流体的第三流体流动路径。 第一和第二流动路径靠近第三流动路径定位，以在第三流体和第一和第二流体两者之间传递热量。 第三流动路径被配置为当第一流体以第一速率承载热量时以第一流体的速率传递第二流体和第三流体之间的热量，并且当第一流体 不携带热量，或以低于第一速率的第二速率承载热量。 因此，当由一种流体排出的热量降低时，可以增加剩余流体的传热速率。

    Fireproof electrical wire housing
    10.
    发明授权
    Fireproof electrical wire housing 失效
    防火电线外壳

    公开(公告)号：US5664810A

    公开(公告)日：1997-09-09

    申请号：US533952

    申请日：1995-09-26

    申请人： Edward Zielinski

    发明人： Edward Zielinski

    IPC分类号： F16L5/02 ,  A62C3/16 ,  H02G3/04 ,  H02G3/22 ,  F16L39/00

    CPC分类号： H02G3/22 ,  A62C3/16 ,  H02G3/0412

    摘要： A fireproof electrical wire housing (9) for routing electrical wires through a barrier wall, such as an aircraft bulkhead (21), without destroying the fireproof and hermetic functions of the bulkhead (21) is disclosed. The fireproof electrical wire housing (9) includes a sleeve (13) which surrounds a wire bundle (11) and a tubular housing (19). The tubular housing (19) includes a cover plate (17) that is mounted to the bulkhead(21). Thereafter, the sleeve (13) is inserted into the tubular housing (19). Holes (35) penetrating the wall of the sleeve (13) are used to inject a sealant into a cavity (39) in the sleeve (13) to prevent vapors and flames from passing through the fireproof electrical wire housing (9).

    摘要翻译： 公开了一种用于在不破坏隔板（21）的防火和密封功能的情况下将电线穿过阻挡壁（例如飞机隔板21）的防火电线外壳（9）。 防火电线外壳（9）包括围绕电线束（11）的套管（13）和管状外壳（19）。 管状壳体（19）包括安装在舱壁（21）上的盖板（17）。 此后，套筒（13）插入管状壳体（19）中。 穿过套筒（13）的壁的孔（35）用于将密封剂注入到套筒（13）中的空腔（39）中，以防止蒸汽和火焰穿过防火电线外壳（9）。