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21. 发明授权

US09935539B2 System and method for controlling at least one switching device, especially for use in aircraft 有权
公开(公告)号：US09935539B2
公开(公告)日：2018-04-03
申请号：US14827098
申请日：2015-08-14
申请人： Zodiac Aero Electric
发明人： Jean-Clair Pradier , Stéphane Guenot
IPC分类号： B60L1/00 , B60L3/00 , H02G3/00 , H02M3/04 , B64D47/00 , H02J3/00 , G06F11/16 , H03K17/18 , H03K17/691 , G06F11/18 , H02H1/00 , H02H3/08 , H02H5/04
CPC分类号： H02M3/04 , B64D47/00 , G06F11/1641 , G06F11/182 , H02H1/0015 , H02H1/0092 , H02H3/08 , H02H5/04 , H02J3/00 , H03K17/18 , H03K17/691
摘要： System, especially for use in aircraft, for controlling at least one switching device (5, 5b, 5n) able to open or close the connection between at least one power source and at least one supplied device, and means for measuring the state of the power supply channel. The system comprises: at least two microcontrollers (1a, 1b) each able to emit a command intended for each switching device (5, 5b, 5n), said microcontrollers (1a, 1b) being connected to at least one portion of the means for measuring the state of the power supply channel; and a means (14, 14b, 14n) for determining the command to be transmitted, able to determine the command to be transmitted to each switching device (5, 5b, 5n) from the commands emitted by each microcontroller (1a, 1b) and intended for said control switch.

22. 发明申请

US20180062358A1 DEVICE FOR ELECTRICALLY CONNECTING POWER DISTRIBUTION PLATES AND ELECTRICAL POWER DISTRIBUTION SYSTEM PROVIDED WITH SUCH A CONNECTION DEVICE 审中-公开
公开(公告)号：US20180062358A1
公开(公告)日：2018-03-01
申请号：US15638079
申请日：2017-06-29
申请人： Zodiac Aero Electric
发明人： Olivier Deshayes
IPC分类号： H02B1/20 , H05K7/14 , H02B1/48 , H02J4/00 , H02J1/10
CPC分类号： H02B1/20 , B64D41/00 , B64D2221/00 , F16B39/10 , H01R12/7088 , H01R12/732 , H01R25/164 , H01R2201/26 , H02B1/48 , H02J1/10 , H02J4/00 , H05K7/1457
摘要： A device for electrically connecting power distribution plates, comprises a connector fastened to one end of a first plate and comprising power contacts for a second plate. The connector comprises a pair of separate electrical connection parts which together electrically connect two power busbars of the first plate to two power busbars of the second plate and each includes a base for electrically connecting and mechanically fastening the part to a power busbar of the first plate and a power contact branch extending from the base and intended to interact with a power busbar of the second plate.

23. 发明授权

US09854675B2 Electronic circuit laid flat and corresponding three-dimensional electronic circuit 有权
公开(公告)号：US09854675B2
公开(公告)日：2017-12-26
申请号：US14539035
申请日：2014-11-12
申请人： ZODIAC AERO ELECfRIC
发明人： Vianney Pouget , Antonio Simao
IPC分类号： H05K1/00 , H05K1/14 , H05K1/02 , H05K1/11 , H05K1/18 , H05K3/36
CPC分类号： H05K1/148 , H05K1/028 , H05K1/11 , H05K1/189 , H05K3/361 , H05K2201/047 , H05K2201/05 , H05K2201/058 , H05K2201/10106 , H05K2201/10151
摘要： This electronic circuit, includes a set of electronic boards intended to support components and linked together by joining elements. The joining elements include curved flexible printed circuits linking two opposing ends of two electronic boards running side by side, the said curved flexible printed circuits being foldable for erecting the electronic circuit into a volume so that the electronic circuit comprises electronic boards placed opposite one another.

24. 发明授权

US09804653B2 Electrical distribution system for an aircraft 有权
公开(公告)号：US09804653B2
公开(公告)日：2017-10-31
申请号：US14826741
申请日：2015-08-14
申请人： Zodiac Aero Electric
发明人： Jean-Clair Pradier
IPC分类号： G06F11/00 , G06F1/28 , G06F13/36 , H02J1/00 , H02J4/00 , H02J9/00 , H02J13/00
CPC分类号： G06F1/28 , G06F13/36 , H02J1/00 , H02J4/00 , H02J9/00 , H02J13/00
摘要： Electrical distribution system for an aircraft comprising at least one electrical supply path comprising at least one power unit capable of opening or closing the connection between at least one electrical energy source and at least one device of the aircraft. The system comprises protection cards (2b, 2n) each comprising at least two microcontrollers each capable of sending a command to each power unit of the electrical supply paths protected by each protection card and, among the set of microcontrollers of the protection cards, at least two microcontrollers are provided with a communication and computation function with all of the microcontrollers of the protection cards (2b, 2n).

25. 发明申请

US20160069529A1 EXTERIOR SIGNALING AND/OR ILLUMINATING LIGHT AND CORRESPONDING SIGNALING AND/OR ILLUMINATING SYSTEM 有权
标题翻译：外部信号和/或照明灯和相应的信号和/或照明系统
公开(公告)号：US20160069529A1
公开(公告)日：2016-03-10
申请号：US14844854
申请日：2015-09-03
申请人： Zodiac Aero Electric
发明人： Christian Tsao , Maxime De Truchis
IPC分类号： F21S8/10 , F21V5/02
CPC分类号： F21S43/26 , B64D47/04 , B64D2203/00 , F21V5/02 , F21W2107/30 , F21Y2105/10 , F21Y2115/10
摘要： This exterior signaling and/or illuminating light, especially for an aircraft, comprises an array of exterior illuminating optical modules (7) ensuring the execution of at least one exterior signaling and/or illuminating function and an array of at least one deviating optical device (14), the illuminating optical modules being selectively activatable in groups of at least one illuminating optical module in order to selectively execute an exterior signaling and/or illuminating function conjointly with said deviating optical device.
摘要翻译：这种外部信号和/或照明光，特别是对于飞行器，包括一组外部照明光学模块（7），确保至少一个外部信号和/或照明功能的执行和至少一个偏离的光学装置如图14所示，照明光学模块可以选择性地激活至少一个照明光学模块的组，以便选择性地执行与所述偏离光学装置的外部信号和/或照明功能。

26. 发明申请

US20160068276A1 OPTICAL DEVICE FOR LIGHTING AND/OR SIGNALING LIGHT FOR AIRCRAFT AND LIGHT COMPRISING SUCH AN OPTICAL DEVICE 审中-公开
标题翻译：用于飞机照明和/或信号灯的光学装置和包含这种光学装置的光
公开(公告)号：US20160068276A1
公开(公告)日：2016-03-10
申请号：US14844987
申请日：2015-09-03
申请人： Zodiac Aero Electric
发明人： Christian Tsao , Maxime De Truchis
IPC分类号： B64D47/02
CPC分类号： B64D47/02 , B64D47/04 , F21V5/04 , F21V7/0091 , F21V13/04 , G02B19/0028 , G02B19/0061
摘要： This optical device for lighting and/or signaling system comprises a set of at least one collimator (10) each comprising a light ray input surface (13) refracting the light, a collimated light beam output surface (17) and a reflecting surface (16) intended to reflect light beams refracted by the input surface and suitable for reflecting the rays in parallel directions. The input surface (13) comprises a set of surfaces (S1, S2, S3) refracting the light that are juxtaposed and suitable for directing the rays from the source towards the reflecting surface.
摘要翻译：用于照明和/或信号系统的该光学装置包括一组至少一个准直仪（10），每个准直仪包括折射光的光线输入表面（13），准直光束输出表面（17）和反射表面（16））旨在反射由输入表面折射的光束并且适于在平行方向上反射光线。输入表面（13）包括一组折射与并置的光并适于将来自源的光线引向反射表面的表面（S1，S2，S3）。

27. 发明申请

US20160049760A1 CONNECTION SYSTEM FOR PROTECTION BOARDS OF A DISTRIBUTION SYSTEM AND RACK INCORPORATING SAID SYSTEM 审中-公开
标题翻译：配电系统保护板连接系统和机架配电系统
公开(公告)号：US20160049760A1
公开(公告)日：2016-02-18
申请号：US14827032
申请日：2015-08-14
申请人： Zodiac Aero Electric
发明人： Jean-Clair Pradier , Frédéric Pinard
IPC分类号： H01R27/02
摘要： Connection system arranged in a rack, for connecting at least one protection board (13a, 13b) of an electrical distribution system of an aircraft with a primary power supply, to at least one powered device (8a, 8b) and to a motherboard arranged in the rack.The connection system includes at least one modular connector on each protection board and, for each protection board capable of being inserted in the rack, at least one additional modular connector attached at least partly on the rack and at least one additional connector connected to the motherboard.
摘要翻译：布置在机架中的连接系统，用于将飞机的配电系统的至少一个保护板（13a，13b）与主电源连接到至少一个动力装置（8a，8b）和布置在其中的主板机架。连接系统包括在每个保护板上的至少一个模块化连接器，并且对于能够插入到机架中的每个保护板，至少一个附加的模块化连接器至少部分地连接在机架上，以及至少一个附加连接器连接到主板。

28. 发明申请

US20160048186A1 ELECTRICAL DISTRIBUTION SYSTEM FOR AN AIRCRAFT 有权
标题翻译：用于飞机的电气分配系统
公开(公告)号：US20160048186A1
公开(公告)日：2016-02-18
申请号：US14826741
申请日：2015-08-14
申请人： ZODIAC AERO ELECTRIC
发明人： Jean-Clair Pradier
IPC分类号： G06F1/28 , G06F13/36
CPC分类号： G06F1/28 , G06F13/36 , H02J1/00 , H02J4/00 , H02J9/00 , H02J13/00
摘要： Electrical distribution system for an aircraft comprising at least one electrical supply path comprising at least one power unit capable of opening or closing the connection between at least one electrical energy source and at least one device of the aircraft. The system comprises protection cards (2b, 2n) each comprising at least two microcontrollers each capable of sending a command to each power unit of the electrical supply paths protected by each protection card and, among the set of microcontrollers of the protection cards, at least two microcontrollers are provided with a communication and computation function with all of the microcontrollers of the protection cards (2b, 2n).
摘要翻译：一种用于飞行器的配电系统，包括至少一个供电路径，该至少一个供电路径包括能够打开或关闭至少一个电能源与飞行器的至少一个装置之间的连接的至少一个功率单元。该系统包括每个包括至少两个微控制器的保护卡（2b，2n），每个微控制器能够向每个保护卡保护的电源路径的每个电源单元发送命令，并且在保护卡的微控制器组中至少两个微控制器具有与保护卡（2b，2n）的所有微控制器的通信和计算功能。

29. 发明授权

US10926889B2 Hybrid headlight for aircraft 有权
公开(公告)号：US10926889B2
公开(公告)日：2021-02-23
申请号：US15469056
申请日：2017-03-24
申请人： Zodiac Aero Electric
发明人： Christian Tsao
IPC分类号： B64D47/04 , G02B19/00 , B64D47/02 , B64D47/06 , G02B5/02 , G02B27/09
摘要： This beam shaper for an aircraft headlight comprises a light input surface (3) and a light output surface (6), the output surface comprises prism-shaped areas so as to deflect a light beam transmitted between the light input surface and output surface by guiding the beam in two directions (D1, D2) which are oblique relative to an optical axis (A) of the beam shaper.

30. 发明授权

US10693281B2 Device for electrically connecting power distribution plates and electrical power distribution system provided with such a connection device 有权
公开(公告)号：US10693281B2
公开(公告)日：2020-06-23
申请号：US15638079
申请日：2017-06-29
申请人： Zodiac Aero Electric
发明人： Olivier Deshayes
IPC分类号： H02B1/20 , F16B39/10 , H02B1/48 , H01R12/70 , H01R12/73 , H02J1/10 , H02J4/00 , H05K7/14 , B64D41/00 , H01R25/16
摘要： A device for electrically connecting power distribution plates, comprises a connector fastened to one end of a first plate and comprising power contacts for a second plate. The connector comprises a pair of separate electrical connection parts which together electrically connect two power busbars of the first plate to two power busbars of the second plate and each includes a base for electrically connecting and mechanically fastening the part to a power busbar of the first plate and a power contact branch extending from the base and intended to interact with a power busbar of the second plate.

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