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31. 发明授权

US09800025B2 Power supply controller for an electrical energy distribution network and method for manufacturing this controller 有权
公开(公告)号：US09800025B2
公开(公告)日：2017-10-24
申请号：US14975398
申请日：2015-12-18
申请人： Zodiac Aero Electric
发明人： Olivier Deshayes , Jérôme Jean-Louis Corneil Valire
IPC分类号： H02B1/04 , B60R16/03 , H05K7/14 , H02M7/00
CPC分类号： H02B1/04 , B60R16/03 , H02M7/003 , H05K7/1457
摘要： This power supply controller for an electrical energy distribution network comprises an electronic power card on which power modules are fitted and on which a set of at least one control module is fitted to control the power modules.The electronic card comprises control buses positioned between the control modules and power module fitting locations on which power modules are fitted according to the use of the controller, to form an electronic power card specific to a use of the power supply controller.

32. 发明申请

US20170275021A1 HYBRID HEADLIGHT FOR AIRCRAFT 审中-公开
公开(公告)号：US20170275021A1
公开(公告)日：2017-09-28
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 , G02B27/09 , G02B19/00
CPC分类号： B64D47/04 , B64D47/02 , B64D47/06 , G02B5/0231 , G02B19/0028 , G02B19/0066 , G02B27/0955 , G02B27/0972
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.

33. 发明申请

US20170242564A1 INTERFACE FOR AIRCRAFT AND METHOD OF CONTROL OF SUCH AN INTERFACE 审中-公开
公开(公告)号：US20170242564A1
公开(公告)日：2017-08-24
申请号：US15438465
申请日：2017-02-21
申请人： Zodiac Aero Electric
发明人： Romain De Bossoreille
IPC分类号： G06F3/0488
CPC分类号： G06F3/0488 , G01C23/00 , G06F3/0416 , G06F3/1454 , G06F2203/0383 , G06F2203/04803 , G09G5/14 , G09G2340/12 , G09G2340/125 , G09G2370/16 , G09G2380/12 , G09G2380/14
摘要： This interface for aircraft comprises an assemblage of at least one display device for the display of data, at least one support (L) for portable computer equipment comprising means of power supply for the computer equipment, bidirectional means of data transfer to the computer equipment and a communication gateway (4) between the support and the onboard display device, comprising means of copying image data in order to copy the image data coming from the computer equipment onto at least a portion of the screen of at least one of the display devices and means of transfer of data representative of a command gesture between the display device and the support.

34. 发明申请

US20170031400A1 SYSTEM FOR CONTROLLING THE ELECTRICAL POWER SUPPLY OF AN AIRCRAFT 审中-公开
标题翻译：用于控制飞机电力供应的系统
公开(公告)号：US20170031400A1
公开(公告)日：2017-02-02
申请号：US15225067
申请日：2016-08-01
申请人： ZODIAC AERO ELECTRIC
发明人： Jean-Pierre BALBINOT
IPC分类号： G06F1/26
CPC分类号： G06F1/26 , B64D2221/00 , G05B9/03 , H02J4/00
摘要： A system for controlling electrical power supply of an aircraft includes at least two control boards and at least two switching members. Each switching member is connected to each control board. Each control board includes a processor. Each processor is configured to determine a command for switching states of switch contacts of each switching member and to determine information relating to validity of each switching command. Each switching member includes a transmitter to determine a command to be transmitted to a detector to detect parallelization, a power actuator configured to transmit a power signal to the switch contacts depending on the command received from the detector, and switch contacts configured to selectively open or close an electrical power supply line. The command is selected from the switching commands and the information relating to the validity of each switching command.
摘要翻译：用于控制飞行器电力供应的系统包括至少两个控制板和至少两个切换构件。每个开关构件连接到每个控制板。每个控制板包括一个处理器。每个处理器被配置为确定用于切换每个切换构件的开关触点的状态的命令，并且确定与每个切换命令的有效性有关的信息。每个切换构件包括发射机，用于确定要发送到检测器以检测并行化的命令;动力致动器，被配置为根据从检测器接收的命令向开关触点发送功率信号;以及开关触点，被配置为选择性地打开或关闭电源线。从切换命令和与每个切换命令的有效性相关的信息中选择该命令。

35. 发明申请

US20170027076A1 ELECTRICAL EQUIPMENT COMPRISING ELECTRONIC CARDS 有权
标题翻译：包含电子卡的电气设备
公开(公告)号：US20170027076A1
公开(公告)日：2017-01-26
申请号：US14392321
申请日：2014-06-26
申请人： ZODIAC AERO ELECTRIC
发明人： Olivier Deshayes
IPC分类号： H05K7/14 , H05K7/16 , H05K7/20
CPC分类号： H05K7/1418 , H05K7/1412 , H05K7/16 , H05K7/20127
摘要： Electrical equipment, in particular for aircraft, comprising: a fixed frame delimiting a storage compartment having a front opening, a pivoting frame mounted to pivot on the fixed frame to occupy a storage position in which it is placed inside the storage compartment of the fixed frame and an accessibility position in which it extends through the front opening of the fixed frame, the pivoting frame delimiting a reception space having at least one access opening, situated behind its front, for the introduction of electronic cards and their removal when the pivoting frame is in said accessibility position in which said access opening is situated in front of said front opening of the fixed frame, the pivoting frame being provided with electrical connection means that can be coupled to electrical connection means of the electronic cards.
摘要翻译：电气设备，特别是用于飞行器的电气设备包括：限定具有前开口的储藏室的固定框架，安装成在固定框架上枢转的枢转框架，以占据其被放置在固定框架的储藏室内部的存储位置以及可伸缩位置，其中其延伸穿过固定框架的前开口，枢转框架限定具有位于其前部后面的至少一个进入开口的接收空间，用于引入电子卡片，并且当枢转框架是在所述可接近位置，其中所述进入开口位于所述固定框架的所述前开口的前面，所述枢转框架设置有可连接到所述电子卡的电连接装置的电连接装置。

36. 发明申请

US20150255963A1 THREE-PHASE ELECTRICAL ENERGY DISTRIBUTION SYSTEM FURNISHED WITH A MEANS OF GUIDANCE OF ELECTRIC ARCS 有权
标题翻译：三相电气分配系统配有电气指导手段
公开(公告)号：US20150255963A1
公开(公告)日：2015-09-10
申请号：US14640305
申请日：2015-03-06
申请人： Zodiac Aero Electric
发明人： Remi Andreoletti
IPC分类号： H02B1/20 , H02B1/46
CPC分类号： H02B13/025 , H02B1/46 , H02G5/00 , H02G5/005
摘要： A three-phase electrical energy distribution system includes a set of current distribution bars extending side by side and clad with an insulator. The bars include opposing insulator-free zones. The electrical energy distribution system finds application to the three-phase electrical energy distribution systems embedded aboard an aircraft.
摘要翻译：三相电能分配系统包括一组并排延伸并用绝缘体包覆的电流分配棒。这些棒包括相对的无绝缘体区域。电能分配系统适用于飞机上嵌入的三相电能分配系统。

37. 发明申请

US20150009593A1 DEVICE AND METHOD FOR PROTECTING AGAINST LEAKAGE CURRENTS 审中-公开
标题翻译：防止泄漏电流的装置和方法
公开(公告)号：US20150009593A1
公开(公告)日：2015-01-08
申请号：US14323155
申请日：2014-07-03
申请人： Zodiac Aero Electric
发明人： Stéphane Guenot , Loic Aoustin , Jean-Clair Pradier
IPC分类号： H02H9/08 , H01H83/02
CPC分类号： H02H9/08 , H01H83/02 , H02H5/12 , H02H9/041
摘要： Device for protecting against leakage currents, the device being intended to be wired up between a first electrical connection (2) and a second electrical connection (3).The device comprises a switch (5) configured so as to at least partially divert the current flowing in the first electrical connection and controlled by the voltage of the first electrical connection.
摘要翻译：用于防止泄漏电流的装置，该装置旨在在第一电连接（2）和第二电连接（3）之间布线。该装置包括开关（5），其被配置为至少部分地转移在第一电连接中流动并由第一电连接的电压控制的电流。

38. 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.

39. 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.

40. 发明授权

US10435174B2 Optical device for lighting and/or signaling light for aircraft and light comprising such an optical device 有权
公开(公告)号：US10435174B2
公开(公告)日：2019-10-08
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 , B64D47/04 , F21V7/00 , G02B19/00 , F21V5/04 , F21V13/04
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.

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