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1. 发明申请

US20150251769A1 IN-FLIGHT REFUELING METHOD AND SYSTEM FOR CONTORLLING MOTION OF THE HOSE AND DROGUE 有权
标题翻译：用于管理软管和驱动器的运动的飞行补救方法和系统
公开(公告)号：US20150251769A1
公开(公告)日：2015-09-10
申请号：US14640652
申请日：2015-03-06
申请人： EADS Construcciones Aeronauticas S.A.
发明人： Samuel De la Fuente Lopez , Bruno Martinez Vazquez
IPC分类号： B64D39/06 , B64D39/02
CPC分类号： B64D39/06 , B64D39/00 , B64D39/02
摘要： A method for in-flight refueling of a receiver aircraft from a tanker aircraft including: measuring continuously a tension at an end of a hose extending from the tanker aircraft towards the receiver aircraft, and using the measured tension to control a torque applied to a drum device deploying the hose from the tanker aircraft such that the tension at the end of the hose conforms to target tensions during each phase of the refueling operation.
摘要翻译：一种用于从油罐飞机进行飞行中加油的方法，包括：连续地测量从油罐飞机向接收机飞行器延伸的软管的端部处的张力，并使用测量的张力来控制施加到滚筒的扭矩装置从油罐飞行器部署软管，使得软管末端的张力在加油操作的每个阶段期间符合目标张力。

2. 发明申请

US20150003556A1 COMMUNICATION METHODS BETWEEN A TANKER AIRCRAFT AND A RECEIVER AIRCRAFT IN AN IN-FLIGHT REFUELING OPERATION 有权
标题翻译：航空器飞行员与航空器中的接收机之间的通信方法
公开(公告)号：US20150003556A1
公开(公告)日：2015-01-01
申请号：US14318849
申请日：2014-06-30
申请人： EADS CONSTRUCCIONES AERONAUTICAS, S.A.,
发明人： Javier FERNANDEZ GARCíA , Luis Fernando GIMENEZ ABAD
IPC分类号： H04L27/14 , B64D39/00 , H04L27/12
CPC分类号： H04L27/14 , B64D39/00 , H04L27/12
摘要： The invention provides transmission methods of messages between a tanker aircraft and receiver aircraft that facilitate air refueling operations using a boom device in, particularly, radio silence environments. In the case of data messages, the method comprises steps for transmitting a message from the aircraft that emits the message to the target aircraft as an analog signal via the electro-magnetic connection which is used for contact detection and disconnection and audio communications between the tanker aircraft and the receiver aircraft in radio silence environments. In the case of audio and data messages it is transmitted a signal resulting from mixing analog signals corresponding to both messages in a way that allows their separation at the target aircraft.
摘要翻译：本发明提供了在油船飞机和接收机之间的消息的传输方法，该方法在特别是无线电静音环境中使用吊杆装置来促进空中加油操作。在数据消息的情况下，该方法包括以下步骤：用于经由用于接触检测和断开的电磁连接以及油罐车之间的音频通信的从发射消息的飞机的消息作为模拟信号发送到目标飞机飞机和收音机在无线电沉默环境中。在音频和数据消息的情况下，它被传输一个信号，该信号是通过混合对应于这两个消息的模拟信号产生的，这种信号允许它们在目标飞机上分离。

3. 发明申请

US20130245879A1 METHOD AND SYSTEM FOR MONITORING A STRUCTURE 有权
标题翻译：监测结构的方法和系统
公开(公告)号：US20130245879A1
公开(公告)日：2013-09-19
申请号：US13782622
申请日：2013-03-01
申请人： EADS CONSTRUCCIONES AERONAUTICAS, S.A., SOCIEDAD UNIPERSONAL
发明人： José Ignacio ARMIJO TORRES , Javier GÓMEZ-ESCALONILLA BALLESTEROS , Jaime GARCÍA ALONSO
IPC分类号： G01N19/08
CPC分类号： G01N19/08 , G01M5/0008 , G01M5/0016 , Y02B10/30
摘要： A method and system of monitoring a structure, the method including: a) synchronously acquiring data comprising a plurality of operational parameters and at least one strain data, b) building a significant points dataset from the data acquired in step a), and c) modelling a relationship between the operational parameters and the strain data using the built significant points dataset to train a non-adaptive prediction functional supervised approximation method, wherein the step of building a significant points dataset comprises deletion of redundant information from the acquired data. The resultant models may be used to process structure real operation data in order to estimate the eventual crack initiation and crack growth on a set of predefined locations of the structure.
摘要翻译：一种监测结构的方法和系统，所述方法包括：a）同步获取包括多个操作参数和至少一个应变数据的数据，b）从步骤a）中获取的数据构建有效点数据集，以及c）使用构建的有效点数据集建模操作参数和应变数据之间的关系，以训练非自适应预测功能监督近似方法，其中构建有效点数据集的步骤包括从所获取的数据中删除冗余信息。所得到的模型可以用于处理结构实际操作数据，以估计结构的一组预定义位置上的最终裂纹发生和裂纹扩展。

4. 发明申请

US20130100277A1 WORKBENCH FOR MANUFACTURING OR CHECKING ELECTRICAL WIRING HARNESSES 有权
标题翻译：制造或检查电线束的工作台
公开(公告)号：US20130100277A1
公开(公告)日：2013-04-25
申请号：US13714964
申请日：2012-12-14
申请人： EADS Construcciones Aeronauticas, S.A.
发明人： Alberto Diego Prieto Loefkrantz , Antonio De Marco Mendiela , Carlos Alejo Ramirez , Carlos Martinez Perez , Daniel Martinez Campos , Jose Carlos Diaz Cruz , Marco Antonio Escalera Castro , Raul Cano Bagaza , Raul Quesada Pegalajar
IPC分类号： H05K13/08 , G06T7/00
CPC分类号： H05K13/08 , G06F3/011 , G06T7/0004 , H01B13/01209 , H01B13/01227
摘要： A workbench and an assistance method for manufacturing or checking electrical wiring harnesses. The workbench comprises: an assembly board; image projection devices on the assembly board; optical sensors arranged on the assembly board to provide information about its position; cameras arranged to capture gestures of the technician in charge of the workbench; a computer with a set of computer programs adapted to provide, through the image projection devices images in 1:1 scale of templates of the electrical wiring harness being manufactured or checked projected onto the assembly board and, superimposed on them, complementary images of aid requested by the technician, acting on virtual menus and/or buttons projected onto the assembly board.
摘要翻译：一种用于制造或检查电气线束的工作台和辅助方法。工作台包括：组装板; 组装板上的图像投影设备; 布置在组装板上的光学传感器提供关于其位置的信息; 相机布置成捕获负责工作台的技术人员的手势; 具有一组计算机程序的计算机，其适于通过图像投影设备提供投影到组装板上的正在制造或检查的电线束的1：1标度的图像，并且叠加在其上的辅助图像由技术人员对投影到组装板上的虚拟菜单和/或按钮进行操作。

5. 发明授权

US09407356B2 Digital audio system of an aircraft 有权
标题翻译：数字音响系统的飞机
公开(公告)号：US09407356B2
公开(公告)日：2016-08-02
申请号：US14437557
申请日：2013-10-17
申请人： EADS Construcciones Aeronauticas S.A.
发明人： Marcos De Las Heras Iglesias , Francisco Javier Camacho Almendros , Daniel Saldana Sage , Pedro Luis Malaga Cobollo , Eladio Fernandez Roman , Jose Luis Mendoza Rodriguez-Borlado
IPC分类号： H04B1/38 , H04B7/24 , H04M1/58 , H04R1/08 , H04R1/10
CPC分类号： H04B7/24 , H04M1/58 , H04R1/08 , H04R1/1008
摘要： A digital audio system of an aircraft comprising one or more pieces of audio equipment and one or more pieces of radio equipment providing a reliable side tone to the operators. The audio equipment and the radio equipment have installed in the proximity, respectively, an audio-terminal and a radio-terminal connected to a digital network including digital messages management units and digital signal processors. The digital messages management unit of the audio equipment is provided with a computer program adapted to generate a side tone of an analog audio message issued by the microphone of the audio equipment and to activate/deactivate its sending to the headset of the audio equipment when the audio-terminal receives from the radio-terminal an activation/deactivation command for said side tone.
摘要翻译：一种包括一个或多个音频设备和一个或多个无线电设备的飞行器的数字音频系统，为操作者提供可靠的侧音。音频设备和无线电设备分别安装在连接到包括数字消息管理单元和数字信号处理器的数字网络的音频终端和无线电终端。音频设备的数字消息管理单元设置有适于产生由音频设备的麦克风发出的模拟音频消息的侧音的计算机程序，并且当音频设备的麦克风发送到耳机时，激活/去激活音频设备的耳机音频终端从无线电终端接收用于所述侧音的激活/去激活命令。

6. 发明申请

US20150270892A1 DIGITAL AUDIO SYSTEM OF AN AIRCRAFT 有权
标题翻译：飞机的数字音频系统
公开(公告)号：US20150270892A1
公开(公告)日：2015-09-24
申请号：US14437557
申请日：2013-10-17
申请人： EADS CONSTRUCCIONES AERONAUTICAS, S.A.
发明人： Marcos De Las Heras Iglesias , Francisco Javier Camacho Almendros , Daniel Saldana Sage , Pedro Luis Malaga Cobollo , Eladio Fernandez Roman , Jose Luis Mendoza Rodriguez-Borlado
IPC分类号： H04B7/24 , H04R1/10 , H04R1/08
CPC分类号： H04B7/24 , H04M1/58 , H04R1/08 , H04R1/1008
摘要： A digital audio system of an aircraft comprising one or more pieces of audio equipment and one or more pieces of radio equipment providing a reliable side tone to the operators. The audio equipment and the radio equipment have installed in the proximity, respectively, an audio-terminal and a radio-terminal connected to a digital network including digital messages management units and digital signal processors. The digital messages management unit of the audio equipment is provided with a computer program adapted to generate a side tone of an analog audio message issued by the microphone of the audio equipment and to activate/deactivate its sending to the headset of the audio equipment when the audio-terminal receives from the radio-terminal an activation/deactivation command for said side tone.
摘要翻译：一种包括一个或多个音频设备和一个或多个无线电设备的飞行器的数字音频系统，为操作者提供可靠的侧音。音频设备和无线电设备分别安装在连接到包括数字消息管理单元和数字信号处理器的数字网络的音频终端和无线电终端。音频设备的数字消息管理单元设置有适于产生由音频设备的麦克风发出的模拟音频消息的侧音的计算机程序，并且当音频设备的麦克风发送到耳机时，激活/去激活音频设备的耳机音频终端从无线电终端接收用于所述侧音的激活/去激活命令。

7. 发明申请

US20140158829A1 IN-FLIGHT REFUELING SYSTEMS WITH A DIGITAL COMMUNICATION SUB-SYSTEM 有权
标题翻译：具有数字通信子系统的飞行补救系统
公开(公告)号：US20140158829A1
公开(公告)日：2014-06-12
申请号：US14092271
申请日：2013-11-27
申请人： Eads Construcciones Aeronauticas, S.A.
发明人： Luis Fernando GIMÉNEZ ABAD
IPC分类号： B64D39/00
CPC分类号： B64D39/00
摘要： The invention provides in-flight refueling systems with a communication sub-system available in radio silence operations including at least a first digital wireless data link comprising a first RF transceiver and a second RF transceiver coupled, respectively, to first and second antennas located in two points inside the boom or the hose of the refueling system or in RF communication with them and connected, respectively, to refueling control units in the tanker aircraft and in the free end of the refueling device by data buses allowing a digital communication between them.
摘要翻译：本发明提供飞行中加油系统，其具有在无线电静音操作中可用的通信子系统，包括至少第一数字无线数据链路，第一数字无线数据链路包括分别耦合到第二和第二天线的第一RF收发器和第二RF收发器分配在加油系统的悬臂或软管内，或者与它们进行射频通信，分别连接到加油机中的加油控制单元和加油装置的自由端，通过允许它们之间的数字通信的数据总线。

8. 发明授权

US08610481B2 Discrete signal consolidation device and method and aircraft with said device 失效
标题翻译：离散信号整合装置和方法与飞机与所述装置
公开(公告)号：US08610481B2
公开(公告)日：2013-12-17
申请号：US13671655
申请日：2012-11-08
申请人： Eads Construcciones Aeronauticas, S.A.
发明人： Eladio Lorenzo Pena
IPC分类号： G06F1/04
CPC分类号： H03K5/1252 , G01D5/24
摘要： A device and a method for eliminating transitions in discrete signals. The working of the device and method is based on allowing the charge of a capacitor with one state when the state opposite the state to which it has been assigned is produced and allowing their discharge through a corresponding capacitor when their state is active. The signal is advantageously consolidated without needing processors or programs, is very simple, there is increased reliability, and the device can very easily be integrated in any sensor, such as those used in aircraft.
摘要翻译：一种消除离散信号转换的装置和方法。器件和方法的工作基于在产生与其分配的状态相反的状态下产生具有一个状态的电容器的充电，并且当它们的状态有效时允许它们通过相应的电容器放电。该信号有利地在不需要处理器或程序的情况下被整合，非常简单，增加了可靠性，并且该装置可以非常容易地集成在任何传感器中，例如在飞行器中使用的传感器。

9. 发明申请

US20130299639A1 Communication System 审中-公开
标题翻译：通讯系统
公开(公告)号：US20130299639A1
公开(公告)日：2013-11-14
申请号：US13891748
申请日：2013-05-10
申请人： EADS CONSTRUCCIONES AERONAUTICAS, S.A.
发明人： Bruno Martinez Vazquez
IPC分类号： B64D39/00
CPC分类号： B64D39/00 , B64D39/06
摘要： A communications system between a receiving aircraft and a tanker aircraft. The system includes a retractable tube with a nozzle which connects to a receiving aircraft receptacle, wherein the system comprises a primary device for sending/receiving data on the nozzle and a secondary device for sending/receiving data on the receptacle. The tanker and receiving aircraft transmit data by means of the devices only when the devices are both active and positioned opposite each other. In this way an indication is enabled to at least one of the two aircraft that the nozzle is correctly connected in the receptacle.
摘要翻译：接收飞机和油轮飞机之间的通信系统。该系统包括具有连接到接收飞行器插座的喷嘴的可伸缩管，其中该系统包括用于在喷嘴上发送/接收数据的主要装置以及用于在容器上发送/接收数据的辅助装置。油罐车和接收飞机只有当设备处于活动状态并且彼此相对定位时才通过设备传输数据。以这种方式，能够使两个飞行器中的至少一个喷嘴正确地连接在容器中。

10. 发明授权

US09429459B2 System and method for measuring a mass of fuel within a variable geometry container 有权
标题翻译：用于测量可变几何容器内的燃料质量的系统和方法
公开(公告)号：US09429459B2
公开(公告)日：2016-08-30
申请号：US14524794
申请日：2014-10-27
申请人： EADS Construcciones Aeronauticas, S.A.
发明人： Jose Luis Marcos Montes , Guillaume Angibaud , Samuel De La Fuente Lopez , Martin Espinosa Sanchez
IPC分类号： G01F23/00 , G01F22/00 , G01F23/20
CPC分类号： G01F23/0061 , G01F22/00 , G01F23/20
摘要： A system and method for measuring a mass of fuel contained in a variable geometry container. The container comprises a container assembly, formed by a variable geometry container disposed on a rigid support, a three-axis load cell coupled with the rigid support and providing a first set of three signals with a magnitude proportional to the force exerted by the container assembly, a three-axis accelerometer coupled with the rigid support and providing a second set of three signals with a magnitude proportional to the acceleration to which the container assembly is subjected, and a signal processing device configured to convert the first and the second set of signals into force and acceleration data, for three perpendicular directions of the space, and configured to calculate a measure relative to the mass of fuel contained in the variable geometry container.
摘要翻译：一种用于测量容纳在可变几何容器中的燃料质量的系统和方法。容器包括容器组件，其由设置在刚性支撑件上的可变几何容器形成，与刚性支撑件联接的三轴称重传感器，并提供具有与由容器组件施加的力成比例的大小的第一组三个信号耦合有刚性支撑件的三轴加速度计，并且提供具有与容器组件所承受的加速度成比例的大小的第三组三个信号;以及信号处理装置，被配置为转换第一和第二组信号对于空间的三个垂直方向施加和加速数据，并被配置为计算相对于包含在可变几何容器中的燃料质量的测量。

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