SATELLITE TRANSPONDER WITH A SYSTEM AND A METHOD FOR PROCESSING COMMUNICATION DATA BY ANALOG DIGITAL CONVERSION OF THE SIGNALS, FORMATION OF FREQUENCY CHANNELS AND COMBINATION OF THEM BY A SWITCH WITH A PLURALITY OF STAGES
    1.
    发明公开
    SATELLITE TRANSPONDER WITH A SYSTEM AND A METHOD FOR PROCESSING COMMUNICATION DATA BY ANALOG DIGITAL CONVERSION OF THE SIGNALS, FORMATION OF FREQUENCY CHANNELS AND COMBINATION OF THEM BY A SWITCH WITH A PLURALITY OF STAGES 审中-公开
    用于通过信号的模拟数字转换处理通信数据的系统和方法的卫星应答器,频率信道的形成及其通过具有多个阶段的开关的组合

    公开(公告)号:EP3297181A1

    公开(公告)日:2018-03-21

    申请号:EP17200881.5

    申请日:2013-10-31

    IPC分类号: H04B7/185

    CPC分类号: H04B7/18515

    摘要: An apparatus comprising a backplane and a number of transponder slices connected to the backplane to form a transponder. The number of transponder slices comprise an analog front end configured to receive an analog input comprising a first plurality of bandwidths and a first plurality of interface frequencies, analog to digital converters configured to convert the analog input to digital signals, a digital channelizer configured to process the digital signals to generate a plurality of frequency slices, a digital combiner configured to assemble the plurality of frequency slices to form output sub-bands, a digital switch configured to route the plurality of frequency slices from the digital channelizer to the digital combiner, digital to analog converters configured to convert the output sub-bands to an analog output, and an analog back end configured to transmit the analog output comprising a second plurality of bandwidths and a second plurality of interface frequencies.

    摘要翻译: 一种装置,包括背板和连接到背板的多个转发器片以形成转发器。 应答器片的数量包括被配置为接收包括第一多个带宽和第一多个接口频率的模拟输入的模拟前端,被配置为将模拟输入转换为数字信号的模数转换器,被配置为处理 数字信号以产生多个频率片段,数字组合器,被配置为组合多个频率片段以形成输出子带,数字开关,被配置为将多个频率片段从数字信道器路由到数字组合器,数字 被配置为将输出子带转换为模拟输出的模拟转换器以及被配置为传送包括第二多个带宽和第二多个接口频率的模拟输出的模拟后端。

    SYSTEMS AND METHODS FOR INTERFACING WITH AN AIRCRAFT CABIN CONTROL SYSTEM
    2.
    发明公开
    SYSTEMS AND METHODS FOR INTERFACING WITH AN AIRCRAFT CABIN CONTROL SYSTEM 审中-公开
    用于与飞机机舱控制系统接口的系统和方法

    公开(公告)号:EP3296205A1

    公开(公告)日:2018-03-21

    申请号:EP17185146.2

    申请日:2017-08-07

    摘要: Systems 100 and methods 500 for interfacing with an aircraft cabin control system are provided. One system includes a controller 102 configured to control cabin services 104 associated with one or more passengers 106, a portable electronic device 108 configured to wirelessly connect to the controller 102 and a seat location identifier 112 associated with a seat 114 of one passenger of the passengers 106. The system further includes an application 116 on the portable electronic device 108 that interfaces with the controller 102 when the portable electronic device 108 is wirelessly connected to the controller 102, wherein the application 116 controls the cabin services 104 associated with the seat 114 of the one passenger.

    摘要翻译: 提供了用于与飞机机舱控制系统接口的系统100和方法500。 一个系统包括配置成控制与一个或多个乘客106相关联的机舱服务104的控制器102,配置成无线连接到控制器102的便携式电子设备108以及与乘客的一位乘客的座位114相关联的座位位置标识符112 该系统还包括便携式电子装置108上的应用程序116,当便携式电子装置108无线连接到控制器102时,该应用程序116与控制器102连接,其中应用程序116控制与座椅114相关联的座舱服务104 一位乘客。

    TOROIDAL SUPPORT STRUCTURES
    4.
    发明公开
    TOROIDAL SUPPORT STRUCTURES 审中-公开
    TOROIDAL支撑结构

    公开(公告)号:EP3290344A1

    公开(公告)日:2018-03-07

    申请号:EP17188308.5

    申请日:2017-08-29

    IPC分类号: B64G1/64 B64G1/40

    摘要: Provided are toroidal support structures and assemblies comprising these structures. A toroidal support structure comprises one or more side panels forming a tubular ring and one or more floor panels forming a planar ring. These rings define the toroidal shape of the structure. The structure also comprises multiple isolating linear support components connected to a top edge of the tubular ring. During installation of the structure, the isolating linear support components are attached to a mounting base for supporting the structure relative to the base, while providing thermal isolation to the rings and preventing their mechanical distortion. As such, a toroidal support structure can be attached to various types of mounting bases, such as a cryogenic tank of a spacecraft. Both rings provide supporting and mounting surfaces for equipment, cables, and pipes, while the toroidal opening allows external components to protrude through the support structure.

    摘要翻译: 提供了包括这些结构的环形支撑结构和组件。 环形支撑结构包括形成管状环的一个或多个侧面板和形成平面环的一个或多个地板面板。 这些环限定了结构的环形形状。 该结构还包括连接到管状环的顶部边缘的多个隔离线性支撑部件。 在安装结构时,隔离线性支撑部件连接到安装基座上,以便相对于基座支撑该结构,同时为环提供热绝缘并防止它们的机械变形。 这样,环形支撑结构可以连接到各种类型的安装基座上,例如航天器的低温罐。 两个环为设备,电缆和管道提供支撑和安装表面,而环形开口允许外部组件穿过支撑结构。

    Heat exchanger and associated method employing a stirling engine
    5.
    发明公开
    Heat exchanger and associated method employing a stirling engine 审中-公开
    采用斯特林发动机的换热器和相关方法

    公开(公告)号:EP2503133A3

    公开(公告)日:2018-02-28

    申请号:EP12160818.6

    申请日:2012-03-22

    IPC分类号: F02G1/043

    摘要: A heat exchanger and associated method are provided that may eliminate or reduce the need for an external mechanical or electrical power source to drive the fan by utilization, instead, of a Stirling engine. A heat exchanger (10) includes a plurality of coils (12) configured to carry a primary fluid. The heat exchanger (10) also includes a fan (18) including a plurality of fan blades configured to force a secondary fluid across the plurality of coils to facilitate heat transfer between the primary and secondary fluids. The heat exchanger also includes a Stirling engine (20) operably connected to the fan (18) and configured to cause rotation of the fan blades. A corresponding method is also provided.

    摘要翻译: 提供了一种热交换器和相关的方法,其可以通过替代斯特林发动机来消除或减少对外部机械或电源来驱动风扇的需要。 热交换器(10)包括构造成承载主流体的多个线圈(12)。 热交换器(10)还包括风扇(18),风扇(18)包括多个风扇叶片,所述风扇叶片构造成迫使次级流体流过多个线圈以促进主流体和次级流体之间的热传递。 热交换器还包括斯特林发动机(20),该斯特林发动机(20)可操作地连接到风扇(18)并且被配置为引起风扇叶片的旋转。 还提供了相应的方法。

    SYSTEM AND METHOD FOR HIGH SPEED SURFACE AND SUBSURFACE FOREIGN OBJECT DEBRIS AND DEFECT DETECTION
    6.
    发明公开
    SYSTEM AND METHOD FOR HIGH SPEED SURFACE AND SUBSURFACE FOREIGN OBJECT DEBRIS AND DEFECT DETECTION 审中-公开
    用于高速表面和次表面异物清除和缺陷检测的系统和方法

    公开(公告)号:EP3279648A1

    公开(公告)日:2018-02-07

    申请号:EP17183232.2

    申请日:2017-07-26

    IPC分类号: G01N25/72 B29C70/38

    摘要: A system and method for the detection of foreign object debris materials or defects on and/or under a surface (e.g., outer ply) of a composite part being formed by a composite layup machine. A gantry (203, 205, 215, 220, 305) moves over the composite part (140, 201) along a predetermined length thereof. A thermal excitation source (110) fixed to the gantry (203, 205, 215, 220, 305) directs infrared radiation across the width of the surface of the composite part (140, 201). An infrared camera (120, 206, 210, 211, 212, 216, 221, 310, 320, 330) fixed to the gantry (203, 205, 215, 220, 305) a predetermined distance away from the thermal excitation source (110) scans the surface as the gantry (203, 205, 215, 220, 305) moves to detect and output scan information thereof. A controller (170) is coupled to the thermal excitation source (110) and to the infrared camera (120, 206, 210, 211, 212, 216, 221, 310, 320, 330). The controller (170) processes the sequence of infrared images to identify a foreign object debris material or defect located on and/or under the surface.

    摘要翻译: 一种用于检测由复合叠层机器形成的复合部件的表面(例如,外层)上和/或下面的外来物体碎片材料或缺陷的系统和方法。 门架(203,205,215,220,305)沿其预定长度在复合部件(140,201)上移动。 固定到机架(203,205,215,220,305)的热激发源(110)引导红外辐射穿过复合部件(140,201)的表面的宽度。 一个红外摄像机(120,206,210,211,212,216,221,310,320,330)固定在机架(203,205,215,220,305)上,离开热激励源(110 )在台架(203,205,215,220,305)移动以检测并输出其扫描信息时扫描表面。 控制器(170)耦合到热激发源(110)和红外摄像机(120,206,210,211,212,216,221,310,320,330)。 控制器(170)处理红外图像序列以识别位于表面上和/或表面下的异物碎片材料或缺陷。

    RETRACTABLE INDEX PINS AND METHODS OF OPERATING THEREOF
    7.
    发明公开
    RETRACTABLE INDEX PINS AND METHODS OF OPERATING THEREOF 审中-公开
    可伸缩指针引脚及其操作方法

    公开(公告)号:EP3275587A1

    公开(公告)日:2018-01-31

    申请号:EP17182517.7

    申请日:2017-07-21

    IPC分类号: B23P19/10 F16B19/02

    摘要: Provided are self-retractable centering assemblies and methods of using these assemblies for alignment of parts having determinant assembly alignment holes. An assembly includes a center pin having a threaded portion threadably engaging a drive component. The assembly also includes a puller bushing rotatably coupled to the drive component. The center pin protrudes through the puller bushing and can slide with respect to the puller bushing when the drive component is rotated relative to the center pin. The sliding distance is controlled by a limiter disposed within the cavity of the puller bushing. During operation, a portion of the center pin extends from the puller bushing and is inserted into alignment holes of parts being aligned. The drive component is rotated relative to the center pin resulting in the center pin being pulled out of the alignment holes while the puller bushing is being pressed against the parts.

    摘要翻译: 提供了自我缩回定心组件以及使用这些组件对具有行列式组件对准孔的部件进行对准的方法。 一种组件包括中心销,该中心销具有螺纹啮合驱动部件的螺纹部分。 该组件还包括可旋转地联接到驱动部件的牵拉套。 当驱动部件相对于中心销旋转时,中心销突出穿过拉拔套管并可相对于拉拔套管滑动。 滑动距离由设置在拉拔套管的空腔内的限制器控制。 在操作过程中,中心销的一部分从拉拔套筒延伸并插入对齐的部件的对准孔中。 驱动部件相对于中心销旋转,导致中心销从对准孔中拉出,同时拉动套管被压靠在部件上。

    METHOD FOR DETECTING A FAILING RECTIFIER OR RECTIFIER SOURCE IN A UPS
    8.
    发明公开
    METHOD FOR DETECTING A FAILING RECTIFIER OR RECTIFIER SOURCE IN A UPS 审中-公开
    用于检测UPS中的失效整流器或整流器源的方法

    公开(公告)号:EP3254366A1

    公开(公告)日:2017-12-13

    申请号:EP16714061.5

    申请日:2016-02-04

    发明人: HEBER, Brian P.

    摘要: A method is provided for detecting a failure of a rectifier or a rectifier source in context of an uninterruptible power supply. The method includes: measuring an input current into the rectifier from a primary power source; determining a rate of change in the measured current; determining a current difference between a reference current and the measured current; measuring voltage output by the rectifier; determining a voltage difference between a reference voltage and the measured voltage; and detecting a failure condition of the rectifier as a function of the measured input current, the rate of change in the measured current, the current difference, the measured voltage and the voltage difference. More specifically, a failure condition of the rectifier is identified when the input current is decreasing and the rate of change in the measured current is decreasing and the current difference is increasing and the voltage difference is increasing.

    COMMUNICATION PACKET CONVERSION
    10.
    发明授权
    COMMUNICATION PACKET CONVERSION 有权
    通信分组转换

    公开(公告)号:EP2642725B1

    公开(公告)日:2017-11-22

    申请号:EP12161054.7

    申请日:2012-03-23

    申请人: Itron Global SARL

    发明人: Van Wyk, Hartman

    IPC分类号: H04L29/08 H04L29/06

    CPC分类号: H04W28/065 H04W84/18

    摘要: Techniques for converting communication packets in a network having multiple nodes are described herein. A node may receive communication packets from one or more neighboring nodes. Each communication packet may include control data and payload data. The node may extract the payload data and store the payload data for a time period. The node may determine whether to concatenate the extracted payload data of the communication packets (e.g., based on destinations to where each of the extracted payload data are to be sent, a supported data rate, an application type associated with the extracted payload data, etc.). The node may concatenate the extracted payload data of the communication packets and send the concatenated payload data to another node in a communication packet.