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    POWER SUPPLY SYSTEM AND METHOD ON BOARD AN AIRCRAFT
    1.
    发明申请
    POWER SUPPLY SYSTEM AND METHOD ON BOARD AN AIRCRAFT 有权
    电源系统和飞机上的方法

    公开(公告)号：US20080100136A1

    公开(公告)日：2008-05-01

    申请号：US11877278

    申请日：2007-10-23

    申请人： Olivier LANGLOIS ,  Lucien Prisse ,  Etienne Foch ,  Dominique Alejo

    发明人： Olivier LANGLOIS ,  Lucien Prisse ,  Etienne Foch ,  Dominique Alejo

    IPC分类号： B60L1/00 ,  H02J1/00

    CPC分类号： H02J3/38 ,  H02J1/10 ,  H02J4/00 ,  H02J5/00 ,  Y10T307/25 ,  Y10T307/313

    摘要： The invention relates to a system and a power supply method, on board an aircraft. The power supply system of an aircraft comprises several generators powering with 230 volts A.C. several distinct electrical cores, wherein the various loads of the aeroplane are connected to each of these cores, in which each core comprises: an input driver (40), several identical power modules (CVS1 . . . CVSn), means of placing in parallel several power modules comprising interconnection inductances (41) between power modules, and a switching matrix (42, 44) comprising a set of contactors, means (52) of piloting the contactors of the switching matrix (42, 44), so as to reconfigure all of these contactors in the case of failure of a power module, several output filters (43), contactors (44) of the switching matrix (42, 44) that may each be connected to at one load (Cij).

    摘要翻译： 本发明涉及飞机上的系统和电源方法。 飞行器的电源系统包括若干发电机，其具有230伏交流电，几个不同的电芯，其中飞机的各种负载连接到这些核心中的每一个，其中每个核心包括：输入驱动器（40），几个相同的 功率模块（CVS1 ... CVSn）是并联放置的多个功率模块，包括功率模块之间的互连电感（41）和包括一组接触器的开关矩阵（42,44），引导装置（52） 所述开关矩阵（42,44）的所述接触器在所述开关矩阵（42,44）的故障的情况下重新配置所有这些接触器，所述开关矩阵（42,44）的接触器中的多个输出滤波器（43） 每个都可以连接到一个负载（Cij）。

    Device and method for coupling two parts of a DC network, particularly in an aircraft
    2.
    发明授权
    Device and method for coupling two parts of a DC network, particularly in an aircraft 有权
    用于连接DC网络的两个部分，特别是在飞行器中的装置和方法

    公开(公告)号：US08736099B2

    公开(公告)日：2014-05-27

    申请号：US12993659

    申请日：2009-05-28

    申请人： Olivier Langlois ,  Lucien Prisse ,  Marc Aiximeno

    发明人： Olivier Langlois ,  Lucien Prisse ,  Marc Aiximeno

    IPC分类号： B60L1/00 ,  B60L3/00 ,  H02G3/00 ,  H01H83/00

    CPC分类号： H02M3/158 ,  H02M3/156 ,  Y10T307/766

    摘要： A device and method for coupling two parts of a dc network, in which at least two capacitors respectively are installed, particularly onboard an aircraft. The device includes at least one static converter including at least one electronic coupling device, including at least one transistor and one diode, associated with an inductance, arranged between these at least two capacitors.

    摘要翻译： 一种用于耦合直流网络的两部分的装置和方法，其中分别安装至少两个电容器，特别是在飞机上。 该装置包括至少一个静态转换器，其包括至少一个电子耦合装置，该电子耦合装置包括至少一个晶体管和一个与电感相关联的二极管，布置在这些至少两个电容器之间。

    Electrical emergency source device located on an aircraft
    5.
    发明授权
    Electrical emergency source device located on an aircraft 有权
    位于飞机上的电气应急源装置

    公开(公告)号：US07692331B2

    公开(公告)日：2010-04-06

    申请号：US11404077

    申请日：2006-04-14

    申请人： Olivier Langlois ,  Xavier Roboam ,  Hubert Piquet

    发明人： Olivier Langlois ,  Xavier Roboam ,  Hubert Piquet

    IPC分类号： H02J3/00 ,  H02J1/10

    CPC分类号： B64D41/007 ,  H02J7/34 ,  Y02T50/53 ,  Y02T50/54 ,  Y10T307/344 ,  Y10T307/587

    摘要： The invention relates to an electrical emergency source device fitted on an aircraft, which comprises an energy source capable of outputting the power necessary for vital electrical loads (10) to operate correctly, wherein there are two types of these loads: first loads, that absorb a constant power with time, second loads, that absorb variable power with time. Wherein this device comprises: a power source (12) sized to output the average power absorbed by all loads, a power source (15) capable of supplying power peaks absorbed by the second loads, and wherein, since the power of several loads is reversible, the power of the said device is also reversible.

    摘要翻译： 本发明涉及一种安装在飞机上的电气应急源装置，其包括能够输出重要电力负载（10）所需的功率以正常工作的能量源，其中存在两种类型的这些负载：第一负载，其吸收 具有时间的恒定功率，第二负载，随时间吸收可变功率。 其中该装置包括：尺寸设计成输出所有负载吸收的平均功率的电源（12），能够提供由第二负载吸收的功率峰值的电源（15），并且其中，由于多个负载的功率是可逆的 所述设备的功率也是可逆的。

    SYSTEM AND METHOD FOR SUPPLYING POWER FOR ACTUATORS ON BOARD AN AIRCRAFT
    6.
    发明申请
    SYSTEM AND METHOD FOR SUPPLYING POWER FOR ACTUATORS ON BOARD AN AIRCRAFT 有权
    用于为飞机上的执行机构供电的系统和方法

    公开(公告)号：US20080174177A1

    公开(公告)日：2008-07-24

    申请号：US12013082

    申请日：2008-01-11

    申请人： Olivier LANGLOIS ,  Etienne Foch ,  Lucien Prisse ,  Xavier Roboam

    发明人： Olivier LANGLOIS ,  Etienne Foch ,  Lucien Prisse ,  Xavier Roboam

    IPC分类号： B64D33/00 ,  H02J3/02 ,  H02J3/38

    CPC分类号： H02J1/14 ,  B64D2221/00 ,  H02J1/08 ,  H02J1/12 ,  Y02T50/54 ,  Y10T307/305 ,  Y10T307/344

    摘要： The invention relates to a system and a method for supplying power to an aircraft comprising several generators supplying alternating current to several different primary electrical master boxes (10, 11, 12 and 13), the various aircraft loads being connected to each of these master boxes. This system comprises conventional master boxes (10, 11, 12 and 13) which supply power loads and at least one master box (40, 41) devoted to actuator loads, this at least one devoted master box being connected to conventional master boxes.

    摘要翻译： 本发明涉及一种用于向飞行器供电的系统和方法，包括向多个不同的主电主箱（10,11,12和13）提供交流电的多个发电机，各种飞机负载连接到这些主箱中的每一个 。 该系统包括提供动力负载的常规主箱（10,11,12和13）以及致力于致动器负载的至少一个主箱（40,41），该至少一个专用主​​箱连接到常规主箱。

    Electrical emergency source device located on an aircraft
    7.
    发明申请
    Electrical emergency source device located on an aircraft 有权
    位于飞机上的电气应急源装置

    公开(公告)号：US20090121546A1

    公开(公告)日：2009-05-14

    申请号：US11404077

    申请日：2006-04-14

    申请人： Olivier Langlois ,  Xavier Roboam ,  Hubert Piquet

    发明人： Olivier Langlois ,  Xavier Roboam ,  Hubert Piquet

    IPC分类号： H02J9/00

    CPC分类号： B64D41/007 ,  H02J7/34 ,  Y02T50/53 ,  Y02T50/54 ,  Y10T307/344 ,  Y10T307/587

    摘要： The invention relates to an electrical emergency source device fitted on an aircraft, which comprises an energy source capable of outputting the power necessary for vital electrical loads (10) to operate correctly, wherein there are two types of these loads: first loads, that absorb a constant power with time, second loads, that absorb variable power with time. Wherein this device comprises: a power source (12) sized to output the average power absorbed by all loads, a power source (15) capable of supplying power peaks absorbed by the second loads, and wherein, since the power of several loads is reversible, the power of the said device is also reversible.

    摘要翻译： 本发明涉及一种安装在飞机上的电气应急源装置，其包括能够输出重要电力负载（10）所需的功率以正常工作的能量源，其中存在两种类型的这些负载：第一负载，其吸收 具有时间的恒定功率，第二负载，随时间吸收可变功率。 其中该装置包括：尺寸设计成输出所有负载吸收的平均功率的电源（12），能够提供由第二负载吸收的功率峰值的电源（15），并且其中，由于多个负载的功率是可逆的 所述设备的功率也是可逆的。

    System and method for supplying power for actuators on board an aircraft
    9.
    发明授权
    System and method for supplying power for actuators on board an aircraft 有权
    为飞机上的执行器供电的系统和方法

    公开(公告)号：US07923857B2

    公开(公告)日：2011-04-12

    申请号：US12013082

    申请日：2008-01-11

    申请人： Olivier Langlois ,  Etienne Foch ,  Lucien Prisse ,  Xavier Roboam

    发明人： Olivier Langlois ,  Etienne Foch ,  Lucien Prisse ,  Xavier Roboam

    IPC分类号： B60L1/00

    CPC分类号： H02J1/14 ,  B64D2221/00 ,  H02J1/08 ,  H02J1/12 ,  Y02T50/54 ,  Y10T307/305 ,  Y10T307/344

    摘要： The invention relates to a system and a method for supplying power to an aircraft comprising several generators supplying alternating current to several different primary electrical master boxes (10, 11, 12 and 13), the various aircraft loads being connected to each of these master boxes. This system comprises conventional master boxes (10, 11, 12 and 13) which supply power loads and at least one master box (40, 41) devoted to actuator loads, this at least one devoted master box being connected to conventional master boxes.

    摘要翻译： 本发明涉及一种用于向飞行器供电的系统和方法，包括向多个不同的主电主箱（10,11,12和13）提供交流电的多个发电机，各种飞机负载连接到这些主箱中的每一个 。 该系统包括提供动力负载的常规主箱（10,11,12和13）以及致力于致动器负载的至少一个主箱（40,41），该至少一个专用主​​箱连接到常规主箱。

    Power supply system and method on board an aircraft
    10.
    发明授权
    Power supply system and method on board an aircraft 有权
    飞机上的电源系统和方法

    公开(公告)号：US07737577B2

    公开(公告)日：2010-06-15

    申请号：US11877278

    申请日：2007-10-23

    申请人： Olivier Langlois ,  Lucien Prisse ,  Etienne Foch ,  Dominique Alejo

    发明人： Olivier Langlois ,  Lucien Prisse ,  Etienne Foch ,  Dominique Alejo

    IPC分类号： B60L1/00 ,  H02J3/38

    CPC分类号： H02J3/38 ,  H02J1/10 ,  H02J4/00 ,  H02J5/00 ,  Y10T307/25 ,  Y10T307/313

    摘要： A system and a power supply method, on board an aircraft, in which the power supply system of an aircraft includes several generators powering with 230 volts A.C. several distinct electrical cores, wherein the various loads of the aircraft are connected to each of these cores. Each core includes an input driver, several identical power modules, means of placing in parallel several power modules including interconnection inductances between power modules, and a switching matrix including a set of relays, means of piloting the relays of the switching matrix, so as to reconfigure all of these relays in the case of failure of a power module, several output filters, and relays of the switching matrix that may each be connected to at one load.

    摘要翻译： 一种飞机上的系统和电源方法，其中飞机的电源系统包括若干发电机，其具有230伏交流电供电，几个不同的电芯，其中飞行器的各种负载连接到这些磁芯中的每一个。 每个核心包括输入驱动器，几个相同的功率模块，并联放置包括功率模块之间的互连电感的多个功率模块，以及包括一组继电器的开关矩阵，用于对开关矩阵的继电器进行导频的装置，以便 在电源模块故障的情况下重新配置所有这些继电器，多个输出滤波器和可以在一个负载处连接的开关矩阵的继电器。