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1. 发明申请

US20150287657A1 SOLID-STATE STACKED DIE CONTACTORS 审中-公开
标题翻译：固态堆叠式电机接触器
公开(公告)号：US20150287657A1
公开(公告)日：2015-10-08
申请号：US14245620
申请日：2014-04-04
申请人： Hamilton Sundstrand Corporation
发明人： Pal Debabrata , John Horowy , Eric Karlen , Rainer J. Seidel
IPC分类号： H01L23/049 , H01L23/492 , H01L25/07
CPC分类号： H01L23/049 , H01L23/492 , H01L25/074 , H01L2924/0002 , H05K7/1412 , H05K7/1432 , H01L2924/00
摘要： A solid-state contactor includes a housing, a lead, a bus plate, and an end connector. The lead extends through the housing and into an interior of the housing. The bus plate is disposed within the housing interior and mounts a die which is electrically connected to the lead through the bus plate. The end connector extends between the bus plate and the lead, attaching to the bus plate at an angle for coupling a plurality of bus plates with die to the lead in a stacked arrangement.
摘要翻译：固体接触器包括壳体，引线，总线板和端部连接器。引线延伸穿过外壳并进入外壳的内部。总线板设置在壳体内部并且安装通过母线电连接到引线的管芯。端部连接器在总线板和引线之间延伸，以一定角度附接到总线板，用于将堆叠的多个总线板与管芯耦合到引线上。

2. 发明授权

US09077164B2 Cutting plate for joining together wiring harnesses of electrical cables on an aircraft 有权
标题翻译：用于连接在飞机上的电缆线束的切割板
公开(公告)号：US09077164B2
公开(公告)日：2015-07-07
申请号：US14084950
申请日：2013-11-20
申请人： Airbus Operations S.A.S.
发明人： Christophe Casse , Steve Fernandez , Marie Bayle
IPC分类号： H02G3/02 , B60R16/02 , H05K7/14
CPC分类号： H02G3/02 , B60R16/0207 , H05K7/1412
摘要： A cutting plate includes a planar interface able to accept electrical connectors, two ramps for supporting harnesses and two lateral walls, the dimensions of the interface and of the two ramps in a longitudinal direction being adapted to suit the number of connectors of the cutting plate and the dimensions in the directions other than the longitudinal direction and the dimensions of the lateral walls conforming to standard dimensions.
摘要翻译：切割板包括能够接纳电连接器的平面接口，用于支撑线束和两个侧壁的两个斜面，沿纵向方向的接口和两个斜面的尺寸适合于适合切割板的连接器的数量和在纵向方向以外的方向上的尺寸和符合标准尺寸的侧壁的尺寸。

3. 发明申请

US20140175964A1 ELECTRICAL AND ELECTRONICS BAY OF AN AIRCRAFT WITH AN IMPROVED ARCHITECTURE AND AIRCRAFT INCORPORATING SAID BAY 有权
标题翻译：具有改进建筑物的飞机的电子和电子舱和装有固定舱的飞机
公开(公告)号：US20140175964A1
公开(公告)日：2014-06-26
申请号：US14138543
申请日：2013-12-23
申请人： Airbus Operations (SAS)
发明人： Yves Durand , Bernard Guering
IPC分类号： H05K5/02
CPC分类号： H05K5/0217 , B64D43/00 , H05K7/1412
摘要： An electrical and electronics bay of an aircraft comprising two rows of elements, each row being separated by a single corridor and comprising at least one set of systems elements and at least one electrical power center, the systems elements being arranged in cabinets. At least one of the cabinets comprises mobile shelves for allowing access to the back of the cabinets by crossing it. This architecture makes it possible to increase the density of the elements present in the bay while observing the principles of redundancy and segregation.
摘要翻译：包括两排元件的飞机的电气和电子舱，每排由单个走廊分开，并且包括至少一组系统元件和至少一个电力中心，所述系统元件布置在机柜中。至少一个机柜包括用于允许通过穿过机柜的后部进入的移动货架。这种结构使得可以增加海湾中存在的元素的密度，同时遵守冗余和分离的原理。

4. 发明授权

US08760873B2 Modular assembly for fastening electronic modules 有权
标题翻译：用于紧固电子模块的模块化组件
公开(公告)号：US08760873B2
公开(公告)日：2014-06-24
申请号：US13085969
申请日：2011-04-13
申请人： Pierre Salles
发明人： Pierre Salles
IPC分类号： H05K5/00
CPC分类号： H05K7/1412 , H05K7/20145
摘要： The invention relates to a modular assembly for fastening electronic modules carried on board an aircraft, characterized in that it comprises: a frame (10) having a more or less planar vertical front surface, comprising several mechanical fastening interfaces each intended for mechanically fastening an electronic module, at least one electronic module (80) comprising a mechanical fastening interface and which is attached to the front surface of the frame in suspended position via cooperation of the mechanical fastening interface of the said at least one electronic module with one of the mechanical fastening interfaces of the frame.
摘要翻译：本发明涉及一种用于紧固承载在飞机上的电子模块的模块化组件，其特征在于，其包括：具有或多或少平面的垂直前表面的框架（10），其包括多个机械紧固接口，每个机械紧固接口用于机械地紧固电子模块，至少一个电子模块（80），其包括机械紧固接口，并且通过所述至少一个电子模块的机械紧固界面与所述机械紧固件之一的配合而在悬挂位置附接到所述框架的前表面框架的接口。

5. 发明申请

US20140091188A1 CONNECTION SYSTEM FOR CONNECTING AN ELECTRONIC DEVICE, IN PARTICULAR FOR AN AIRCRAFT, TO A TEST UNIT 有权
标题翻译：用于将特别用于飞机的电子设备连接到测试单元的连接系统
公开(公告)号：US20140091188A1
公开(公告)日：2014-04-03
申请号：US14039917
申请日：2013-09-27
申请人： AIRBUS OPERATIONS (S.A.S.)
发明人： Pierre-Louis Engelvin , Patrice Lafont
IPC分类号： F16M13/02
CPC分类号： F16M13/022 , G01R31/008 , H05K7/1412 , H05K7/1454
摘要： Connection system for connecting an electronic device, in particular for an aircraft, to a test unit. The connection system includes a fixed portion, which is fixable to said test unit, and a movable plate which is capable of receiving the electronic device to be tested and is displaceable linearly with respect to said fixed portion between two positions which correspond respectively to a connection position and a disconnection position of the electronic device, by manually actuated displacement.
摘要翻译：用于将电子装置，特别是飞机连接到测试装置的连接系统。连接系统包括可固定到所述测试单元的固定部分，以及能够接收待测试的电子设备的可移动板，并且可相对于所述固定部分线性移动，该两个位置分别对应于连接位置和电子设备的断开位置。

6. 发明授权

US08559183B1 Method to use empty slots in onboard aircraft servers and communication devices to install non-proprietary servers and communications interfaces 有权
标题翻译：在机载飞机服务器和通信设备上使用空槽的方法来安装非专有服务器和通信接口
公开(公告)号：US08559183B1
公开(公告)日：2013-10-15
申请号：US13733107
申请日：2013-01-02
申请人： iJet Technologies, Inc.
发明人： Terry L. Davis
IPC分类号： H05K7/00
CPC分类号： H05K7/00 , G06F13/409 , H05K7/1412 , H05K7/1459 , Y02D10/14 , Y02D10/151 , Y10T307/359
摘要： The power supply and cooling provided by existing aircraft system line replaceable units (LRUs) or other devices supports new cards that are installed in previously empty slots or which replace existing original cards and which are not limited in functionality and do not require licensing of any proprietary technology included in the LRU. These new cards can include components such as processors, memory, and/or storage that significantly improve the performance of the LRU, and/or add new functionality—all without exceeding the power supply and cooling capability of the LRU. A network and avionics bus interface can be added to a portion of the new card and electrically coupled to the circuitry and electronic components on the new card, so that one or more cables connected to the interface can be connected to externally accessible standard avionics buses and network connectors added to a chassis of the LRU.
摘要翻译：现有飞机系统线路可更换单元（LRU）或其他设备提供的电源和冷却支持安装在以前空槽中的新卡，或更换现有原始卡，而不限制功能，不需要任何专有权技术包括在LRU中。这些新卡可以包括显着提高LRU性能的组件，例如处理器，存储器和/或存储器，和/或添加新功能，而不会超过LRU的电源和冷却能力。网络和航空电子总线接口可以添加到新卡的一部分并且电耦合到新卡上的电路和电子部件，使得连接到接口的一个或多个电缆可以连接到外部可访问的标准航空电子总线，网络连接器添加到LRU的机箱。

7. 发明申请

US20130214105A1 RETENTION MECHANISM AND METHOD FOR REMOVEABLY SUPPORTING A PORTABLE FLIGHT CONTROLLER 有权
标题翻译：保持机械和方法，支持便携式飞行控制器
公开(公告)号：US20130214105A1
公开(公告)日：2013-08-22
申请号：US13770126
申请日：2013-02-19
申请人： L-3 COMMUNICATION AVIONICS SYSTEMS, INC
发明人： Andrew J. Herder , Jadranko NMI Soc
IPC分类号： F16M13/02
CPC分类号： F16M13/02 , B64D2045/0075 , H05K5/0204 , H05K7/1412
摘要： An aircraft electronic device retention mechanism and method of removeably supporting an aircraft electronic device having first electrical contacts within a cockpit having compatible second electrical contacts includes a base that is generally configured to the size and shape of a surface of the electronic device and at least one lever that is mounted by a pivot to the base. The lever(s) has an engaging portion that is adapted to engage an engaged portion of the electronic device and an actuation portion. The actuation portion is adapted to rotate the lever(s) about said pivot between a first orientation in which the engaging portion retains the engaged portion and a second orientation in which the engaging portion does not retain said engaged portion. A manual actuator is connected with the actuation portion of the pivot. The manual actuator is configured to move between a first position, which rotates the lever(s) to the second orientation and a first position which rotates the lever(s) to the first orientation to retain the electronic device.
摘要翻译：一种飞行器电子设备保持机构和方法，其可拆卸地支撑飞行器电子设备，该飞行器电子设备在具有兼容的第二电触点的驾驶舱内具有第一电触头，其包括通常配置为电子设备的表面的尺寸和形状的基座，以及至少一个杠杆由枢轴安装到底座。杠杆具有接合部分，该接合部分适于接合电子设备的接合部分和致动部分。所述致动部分适于在所述接合部分保持所述被接合部分的第一方向和所述接合部分不保持所述被接合部分的第二方位之间围绕所述枢轴旋转所述杆。手动致动器与枢轴的致动部分连接。手动致动器构造成在将杠杆转动到第二方向的第一位置和使杠杆旋转到第一取向以保持电子装置的第一位置之间移动。

8. 发明授权

US08369069B2 Avionics equipment carrier system with quick-mount housing and quick-mount modules 有权
标题翻译：具有快速安装外壳和快速安装模块的航空电子设备载体系统
公开(公告)号：US08369069B2
公开(公告)日：2013-02-05
申请号：US11992148
申请日：2006-09-19
申请人： Stefan Osternack , Oliver Schalke , Sven Rehmeier , Jörg Bradtke
发明人： Stefan Osternack , Oliver Schalke , Sven Rehmeier , Jörg Bradtke
IPC分类号： H05K5/00 , H05K7/00 , B64D45/00 , B64D47/00 , B64F1/00 , B64C1/00
CPC分类号： H05K7/1412 , H05K7/1424
摘要： An avionics equipment carrier system for slide-in modules with data processing, data transmitting, data storage or data displaying devices, such as for example electronics printed circuit boards, network components, storage devices, display devices and the like, or power supply devices, includes a housing, at least one module rack for accommodating the slide-in modules and at least one backplane board with Ethernet connection architecture. When the dimensions of the housing comply with ARINC standards, and the housing is arranged for installation in an avionics module rack as a quick-mount housing, and any desired circuit boards of a specific standard format can be used in the slide-in modules which are designed as quick-mount modules.
摘要翻译：一种用于具有数据处理，数据传输，数据存储或数据显示设备（例如电子印刷电路板，网络组件，存储设备，显示设备等）或电源设备的滑入式模块的航空电子设备载体系统，包括壳体，用于容纳滑入模块的至少一个模块架和具有以太网连接架构的至少一个底板。当壳体的尺寸符合ARINC标准时，并且外壳被布置为安装在作为快速安装壳体的航空电子模块机架中，并且可以在滑入模块中使用具有特定标准格式的任何期望的电路板，被设计为快速安装模块。

9. 发明申请

US20120320512A1 Avionics instrument and mounting bracket 审中-公开
公开(公告)号：US20120320512A1
公开(公告)日：2012-12-20
申请号：US13573131
申请日：2012-08-25
申请人： Joseph Polizzotto , Marc Polizzotto , Lawrence E. Elbert
发明人： Joseph Polizzotto , Marc Polizzotto , Lawrence E. Elbert
IPC分类号： H05K7/00 , G06F1/16
CPC分类号： H05K5/0017 , B64D43/00 , G06F1/1626 , G06F2200/1614 , H05K7/1412
摘要： The present invention is an avionics instrument and mounting bracket. In particular, the present invention is directed to an avionics instrument that can be mounted in a variety of positions on an aircraft instrument panel. The mounting bracket preferably comprises a cylindrical interior and an exterior with squared sides and rounded corners. The bracket has an adjustment gap with first and second ports on opposing sides and an adjustment screw spanning the adjustment gap to adjust the tightness of the bracket. The front of the bracket preferably has four panel screw ports. The avionics instrument has a display panel mounted to a cylindrical electronics housing where the diameter of the housing is less than the length of the display panel. The display panel preferably has four positional modes of display and a control button for switching between the display modes. The cylindrical electronics housing is inserted into the bracket.

10. 发明申请

US20120244740A1 ELECTRICAL AND MECHANICAL CONNECTION DEVICE FOR AN ELECTRONIC MODULE IN A RACK 有权
标题翻译：用于机架中的电子模块的电气和机械连接装置
公开(公告)号：US20120244740A1
公开(公告)日：2012-09-27
申请号：US13429290
申请日：2012-03-23
申请人： Jean-Noël Klaver , Eric Rauscent , Christian Cavailles , Stéphane Fabre
发明人： Jean-Noël Klaver , Eric Rauscent , Christian Cavailles , Stéphane Fabre
IPC分类号： H01R13/62
CPC分类号： H05K7/1412
摘要： The general field of the invention is that of electrical and mechanical connection devices for an electronic module in a rack, the electronic module comprising a first connector and the rack comprising a second connector complementing the first connector. In the connection device according to the invention, the first connector is mounted in a lateral recess on the side of the module, the second connector is mounted with free rotation in the rack on supports which also include a locking handle for ensuring the electrical and mechanical connection of the module in the rack. This device applies particularly to the display devices mounted on aircraft instrument panels.
摘要翻译：本发明的一般领域是用于机架中的电子模块的电气和机械连接装置的电子模块，该电子模块包括第一连接器，并且该机架包括补充第一连接器的第二连接器。在根据本发明的连接装置中，第一连接器安装在模块侧面的横向凹槽中，第二连接器在支架上自由旋转安装在机架上，该支撑件还包括用于确保电和机械的锁定手柄模块在机架中的连接。该装置特别适用于安装在飞机仪表板上的显示装置。

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