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    Health Management of Rechargeable Batteries
    3.
    发明申请
    Health Management of Rechargeable Batteries 有权
    充电电池的健康管理

    公开(公告)号：US20100121587A1

    公开(公告)日：2010-05-13

    申请号：US11565574

    申请日：2006-11-30

    申请人： John L. Vian ,  Ali R. Mansouri ,  Rangasamy Elangovan ,  Mori M. Borumand ,  Khaled Abdel-Motagaly

    发明人： John L. Vian ,  Ali R. Mansouri ,  Rangasamy Elangovan ,  Mori M. Borumand ,  Khaled Abdel-Motagaly

    IPC分类号： G01R31/36

    CPC分类号： G01R31/3624 ,  B64D45/00 ,  G01R31/008 ,  G01R31/3651 ,  G01R31/3679 ,  G01R31/3693 ,  H01M10/425 ,  H01M10/48 ,  H02J7/0022 ,  H02J7/0026 ,  H02J7/0029 ,  Y02E60/12 ,  Y02T10/7055

    摘要： Systems and methods for health management of rechargeable batteries are disclosed. In one embodiment, a rechargeable battery system includes a rechargeable battery, and a battery health management unit operatively coupled to the rechargeable battery and including a state of health module configured to estimate a battery health by receiving battery-related data and predicting one or more failure modes. The state of health module may further include a prognostic failure mode component configured to combine at least one flight data variable with at least one model-based prognostic. In alternate embodiments, the battery health management unit may further include a state of life module and a state of charge module.

    摘要翻译： 公开了用于可再充电电池的健康管理的系统和方法。 在一个实施例中，可再充电电池系统包括可再充电电池和可操作地耦合到可再充电电池的电池健康管理单元，并且包括健康状态模块，其配置为通过接收电池相关数据并预测一个或多个故障来估计电池健康状况 模式。 健康状态模块还可以包括被配置为将至少一个飞行数据变量与至少一个基于模型的预后组合的预后故障模式组件。 在替代实施例中，电池健康管理单元还可以包括生活状态模块和充电状态模块。

    Fitting and associated grommet for supporting a conduit penetrating a panel
    4.
    发明授权
    Fitting and associated grommet for supporting a conduit penetrating a panel 有权
    用于支撑穿透面板的导管的配件和相关索环

    公开(公告)号：US07681923B2

    公开(公告)日：2010-03-23

    申请号：US11561088

    申请日：2006-11-17

    申请人： Mark A. Negley ,  Rangasamy Elangovan ,  Yuri Tian ,  Eric H. Nelson ,  Paul S. Gregg ,  Michael A. Ross

    发明人： Mark A. Negley ,  Rangasamy Elangovan ,  Yuri Tian ,  Eric H. Nelson ,  Paul S. Gregg ,  Michael A. Ross

    IPC分类号： F16L3/04

    CPC分类号： F16L5/06 ,  B64C1/06 ,  F16L5/12

    摘要： A fitting and an associated grommet are provided for supporting a conduit penetrating a panel and limiting energy transfer between the conduit and panel. The fitting may include a grommet having annular first and second sections spaced apart from one another and an annular wall extending between the first and second sections such that the wall and first and second sections define a bore. A plurality of ribs protrude from the annular wall, the ribs being distributed circumferentially around the annular wall and spanning between the first and second sections. A tubular liner extends through the bore of the grommet and contacts the first and second sections. The plurality of ribs extend into the bore, and at least some of the ribs contact the liner.

    摘要翻译： 提供了一种配件和相关的索环，用于支撑穿过面板的导管并限制导管和面板之间的能量传递。 配件可以包括具有彼此间隔开的环形第一和第二部分的垫圈以及在第一和第二部分之间延伸的环形壁，使得壁和第一和第二部分限定孔。 多个肋从环形壁突出，肋围绕环形壁周向分布并跨越第一和第二部分。 管状衬套延伸穿过索环的孔并接触第一和第二部分。 多个肋延伸到孔中，并且至少一些肋与衬垫接触。

    Ice protection system and method
    5.
    发明授权
    Ice protection system and method 有权
    防冰系统和方法

    公开(公告)号：US08777163B2

    公开(公告)日：2014-07-15

    申请号：US12553481

    申请日：2009-09-03

    申请人： Morteza Safai ,  Rangasamy Elangovan ,  Vyacheslav Khozikov

    发明人： Morteza Safai ,  Rangasamy Elangovan ,  Vyacheslav Khozikov

    IPC分类号： B64D15/12

    CPC分类号： B64D15/12 ,  B64D2033/0233

    摘要： An ice protection system and method are provided that facilitate the prevention or reduction in ice formation upon an aerodynamic surface. The ice protection system may include at least one induction coil spaced apart from an electrically conductive layer of an aerodynamic surface and disposed interior of an exterior surface of the aerodynamic surface. For example, the ice protection system may include a plurality of induction coils with each induction coil being spaced apart from the other induction coils such that the respective induction coils are associated with different portions of the aerodynamic surface. The ice protection system may also include a signal source configured to provide alternating current to the induction coil(s) to thereby generate an electromagnetic field that creates an eddy current in the electrically conductive layer so as to heat the electrically conductive layer.

    摘要翻译： 提供了一种防冰系统和方法，其有助于防止或减少空气动力学表面上的冰层形成。 防冰系统可以包括与气动表面的导电层间隔开的至少一个感应线圈，并且设置在空气动力学表面的外表面的内部。 例如，冰保护系统可以包括多个感应线圈，每个感应线圈与其它感应线圈间隔开，使得相应的感应线圈与空气动力学表面的不同部分相关联。 防冰系统还可以包括被配置为向感应线圈提供交流电流从而产生在导电层中产生涡流以便加热导电层的电磁场的信号源。

    Ice Protection System And Method
    6.
    发明申请
    Ice Protection System And Method 有权
    防冰系统和方法

    公开(公告)号：US20110049300A1

    公开(公告)日：2011-03-03

    申请号：US12553481

    申请日：2009-09-03

    申请人： Morteza Safai ,  Rangasamy Elangovan ,  Vyacheslav Khozikov

    发明人： Morteza Safai ,  Rangasamy Elangovan ,  Vyacheslav Khozikov

    IPC分类号： B64D15/12

    CPC分类号： B64D15/12 ,  B64D2033/0233

    摘要： An ice protection system and method are provided that facilitate the prevention or reduction in ice formation upon an aerodynamic surface. The ice protection system may include at least one induction coil spaced apart from an electrically conductive layer of an aerodynamic surface and disposed interior of an exterior surface of the aerodynamic surface. For example, the ice protection system may include a plurality of induction coils with each induction coil being spaced apart from the other induction coils such that the respective induction coils are associated with different portions of the aerodynamic surface. The ice protection system may also include a signal source configured to provide alternating current to the induction coil(s) to thereby generate an electromagnetic field that creates an eddy current in the electrically conductive layer so as to heat the electrically conductive layer.

    摘要翻译： 提供了一种防冰系统和方法，其有助于防止或减少空气动力学表面上的冰层形成。 防冰系统可以包括与气动表面的导电层间隔开的至少一个感应线圈，并且设置在空气动力学表面的外表面的内部。 例如，冰保护系统可以包括多个感应线圈，每个感应线圈与其它感应线圈间隔开，使得相应的感应线圈与空气动力学表面的不同部分相关联。 防冰系统还可以包括被配置为向感应线圈提供交流电流从而产生在导电层中产生涡流以便加热导电层的电磁场的信号源。

    Fitting And Associated Grommet For Supporting A Conduit Penetrating A Panel
    7.
    发明申请
    Fitting And Associated Grommet For Supporting A Conduit Penetrating A Panel 有权
    配套和相关的垫圈支持管道渗透面板

    公开(公告)号：US20080116319A1

    公开(公告)日：2008-05-22

    申请号：US11561088

    申请日：2006-11-17

    申请人： Mark A. Negley ,  Rangasamy Elangovan ,  Yuri Tian ,  Eric H. Nelson ,  Paul S. Gregg ,  Michael A. Ross

    发明人： Mark A. Negley ,  Rangasamy Elangovan ,  Yuri Tian ,  Eric H. Nelson ,  Paul S. Gregg ,  Michael A. Ross

    IPC分类号： F16L55/02 ,  B64C1/00

    CPC分类号： F16L5/06 ,  B64C1/06 ,  F16L5/12

    摘要： A fitting and an associated grommet are provided for supporting a conduit penetrating a panel and limiting energy transfer between the conduit and panel. The fitting may include a grommet having annular first and second sections spaced apart from one another and an annular wall extending between the first and second sections such that the wall and first and second sections define a bore. A plurality of ribs protrude from the annular wall, the ribs being distributed circumferentially around the annular wall and spanning between the first and second sections. A tubular liner extends through the bore of the grommet and contacts the first and second sections. The plurality of ribs extend into the bore, and at least some of the ribs contact the liner.

    摘要翻译： 提供了一种配件和相关的索环，用于支撑穿过面板的导管并限制导管和面板之间的能量传递。 配件可以包括具有彼此间隔开的环形第一和第二部分的垫圈以及在第一和第二部分之间延伸的环形壁，使得壁和第一和第二部分限定孔。 多个肋从环形壁突出，肋围绕环形壁周向分布并跨越第一和第二部分。 管状衬套延伸穿过索环的孔并接触第一和第二部分。 多个肋延伸到孔中，并且至少一些肋与衬垫接触。