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    A communication system for managing a flying operation involving two or more aircraft
    21.
    发明公开
    A communication system for managing a flying operation involving two or more aircraft 审中-公开
    社区系统zwwwwungung einer Flugoperation mit zwei oder mehr Flugzeugen

    公开(公告)号：EP2879312A1

    公开(公告)日：2015-06-03

    申请号：EP13382483.9

    申请日：2013-11-29

    申请人： EADS Construcciones Aeronauticas S.A.

    发明人： Minguez Rascon, Fernado Manuel ,  Arribas Huerta Ángel ,  Jimenez Duro, Antonio ,  Gutierrez Perez, César

    IPC分类号： H04B10/112 ,  B64D39/00

    CPC分类号： H04B10/1129 ,  B64D39/00 ,  H04B10/1125

    摘要： The invention provides a communication system of voice and data messages between two or more aircraft for managing a flying operation, such as a tanker aircraft (11) and a receiver aircraft (13) during a refueling operation, that can be used in adverse environmental and/or operational conditions.
    The communication system is implemented by a free space optical data link between both aircraft which is compatible with radio silence conditions since it is not based on radio frequency transmissions and comprises first and a second segments (21, 41) in the first and second aircraft with communication control modules (25, 45) adapted for converting the messages of voice and/or data in electrical signals and vice versa and optical modules (23, 43) adapted for emitting beams of light modulated by said electrical signals and for converting received beams of modulated light in electrical signals.

    摘要翻译： 本发明提供了一种用于在加油操作期间用于管理飞行操作的两个或多个飞行器之间的语音和数据消息的通信系统，例如油罐飞机（11）和接收机（13），其可以用于不利的环境和 /或操作条件。 通信系统由两个飞机之间的自由空间光学数据链路实现，其与无线电静音条件兼容，因为它不基于射频传输，并且包括第一和第二飞行器中的第一和第二段（21,41） 通信控制模块（25,45），其适于转换电信号中的语音和/或数据的消息，反之亦然;以及适于发射由所述电信号调制的光束的光学模块（23,43），并且用于将 在电信号中调制光。

    A digital audio system of an aircraft
    26.
    发明公开
    A digital audio system of an aircraft 有权
    数字音响系统

    公开(公告)号：EP2723045A1

    公开(公告)日：2014-04-23

    申请号：EP12382410.4

    申请日：2012-10-22

    申请人： EADS Construcciones Aeronauticas, S.A.

    发明人： De las Heras Iglesias, Marcos ,  Camacho Almendros, Francisco Javier ,  Saldaña Sage, Daniel ,  Málaga Cobollo, Pedro Luis ,  Fernandez Román, Eladio ,  Mendoza Rodríguez-Borlado, Jose Luis

    IPC分类号： H04M1/58

    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 audio equipment (11) and one or more radio equipment (47) providing a reliable side tone to the operators. The audio equipment (11) and the radio equipment (47) have installed in the proximity, respectively, an audio-terminal (27) and a radio-terminal (45) connected to a digital network (15) including digital messages management units (37, 57) and digital signal processors (39, 59). The digital messages management unit (37) of the audio equipment (11) is provided with a computer program adapted to generate a side tone of an analog audio message issued by the microphone (21) of the audio equipment (11) and to activate/deactivate its sending to the headset (25) of the audio equipment (11) when the audio-terminal (27) receives from the radio-terminal (45) 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（11）和一个或多个无线电设备（47）的飞行器的数字音频系统，其向操作者提供可靠的侧音。 音频设备（11）和无线电设备（47）分别安装在连接到包括数字消息管理单元（15）的数字网络（15）的音频终端（27）和无线电终端（45） 37,57）和数字信号处理器（39,59）。 音频设备（11）的数字消息管理单元（37）设置有用于产生由音频设备（11）的麦克风（21）发出的模拟音频消息的侧音的计算机程序，并激活/ 当音频终端（27）从无线终端（45）接收到用于所述侧音的激活/去激活命令时，将其发送到音频设备（11）的耳机（25）。

    A guidance apparatus of a tanker aircraft
    27.
    发明公开
    A guidance apparatus of a tanker aircraft 有权
    Führungsvorrichtungfürein Tankflugzeug

    公开(公告)号：EP2636600A1

    公开(公告)日：2013-09-11

    申请号：EP12382085.4

    申请日：2012-03-07

    申请人： EADS Construcciones Aeronauticas S.A.

    发明人： Yagüe Martín, Ignacio

    IPC分类号： B64D39/00 ,  H05B33/08 ,  B64D47/06

    CPC分类号： B64D39/00 ,  B64D47/06 ,  G01R31/00 ,  H05B37/02

    摘要： A guidance apparatus mounted on the belly of a tanker aircraft for providing visual indications to the pilot of the receptor aircraft with respect to the approaching operation to carry out the refueling by means of a refueling boom is provided. The guidance apparatus comprises light emitting devices (11) including modules of light emitting diodes (LEDs) and control devices (41, 61) for supplying current to them that include dimming control units (45, 65) for controlling the intensity of the light emitted by said light emitting devices (11) by means of a dimming signal depending on a dimming voltage ( Vdim ). The dimming control units (45, 65) are adapted to provide to the light emitting devices (11) a pulse-exponential amplitude modulated dimming signal ( Vref2 ) so that the light intensity can be properly controlled in all visibility conditions.

    摘要翻译： 提供了一种安装在油罐飞机腹部上的引导装置，用于相对于通过加油臂执行加油的接近操作向受试飞机的飞行员提供视觉指示。 引导装置包括包括发光二极管（LED）的模块的发光装置（11）和用于向它们提供电流的控制装置（41,61），所述控制装置包括用于控制发射的光的强度的调光控制单元（45,65） 通过所述发光装置（11）通过取决于调光电压（Vdim）的调光信号。 调光控制单元（45,65）适于向发光装置（11）提供脉冲指数幅度调制调光信号（Vref2），使得可以在所有可见度条件下适当地控制光强度。

    Electro mechanical actuator
    28.
    发明公开
    Electro mechanical actuator 有权
    Elektromechanischer Aktuator

    公开(公告)号：EP2626593A1

    公开(公告)日：2013-08-14

    申请号：EP12382047.4

    申请日：2012-02-10

    申请人： EADS Construcciones Aeronauticas, S.A.

    发明人： Flores Giraldo, Santiago ,  Fernández García, Francisco Javier

    IPC分类号： F16H19/00 ,  F16H1/16 ,  B64C13/50 ,  F16H61/12

    CPC分类号： F16H19/04 ,  B64C13/42 ,  B64C13/50 ,  F16H2057/0081 ,  F16H2057/018 ,  Y02T50/44 ,  Y02T50/54 ,  Y10T74/18096

    摘要： A linear actuator (10) comprising:
    - a rotatory input shaft (13) driven by an electric motor having a helical threaded zone (15) in its external surface at its inner end:
    - an output shaft (29) having a helical threaded zone (18) in its external surface at its inner end;
    - a plurality of first helical roller gears (21,21',21") configured to engage with the rotatory input shaft (13) in its helical threaded zone (15) so that they rotate with respect to their axis (22,22',22") when the input shaft (13) rotates;
    - a plurality of second helical roller gears (23,23',23") configured to engage with the first helical roller gears (21,21',21") and with the output shaft (29) in its helical threaded zone (18) so that the rotation of the first helical roller gears (21,21',21") is firstly transmitted to the second helical roller gears (23,23',23"), which rotate with respect to their axis (24,24',24"), and secondly converted in a linear movement of the output shaft (29).

    摘要翻译： 1.一种线性致动器（10），包括：旋转输入轴（13），其由其内端在其外表面具有螺旋螺纹区域（15）的电动机驱动; - 输出轴（29），其具有螺旋形螺纹区 （18）在其外表面的内端; - 多个第一螺旋滚子齿轮（21,21'，21“），其构造成在其螺旋螺纹区域（15）中与旋转输入轴（13）接合，使得它们相对于它们的轴线（22,22' ，22“）; - 多个第二螺旋滚子齿轮（23,23'，23“），其构造成与所述第一螺旋滚子齿轮（21,21'，21”）接合并且所述输出轴（29）处于其螺旋螺纹区域（18 ），使得第一螺旋滚子齿轮（21,21'，21“）的旋转首先被传递到相对于它们的轴线（24,24）旋转的第二螺旋滚子齿轮（23,23'，23”） '，24“），并且二次转换成输出轴（29）的线性运动。

    Latching detection and indication system for aerial refueling couplings
    29.
    发明公开
    Latching detection and indication system for aerial refueling couplings 有权
    Verugelungserkennungs- und -anzeigesystemfürKupplungen zur Luftbetankung

    公开(公告)号：EP2607237A1

    公开(公告)日：2013-06-26

    申请号：EP11382398.3

    申请日：2011-12-23

    申请人： EADS Construcciones Aeronauticas, S.A.

    发明人： Marcos Montes, José Luis ,  Espinosa Sánchez, Martín ,  Terrón Blanco, Jorge ,  De la Fuente López, Samuel

    IPC分类号： B64D39/06

    CPC分类号： B64D39/06

    摘要： Reception coupling unit (31) of a hose and drogue device (19, 21) of a tanker aircraft (13) with the probe (25) of a receiver aircraft (11) for in-flight refueling, comprising, respectively, first and second cooperating latching means (39, 29) that can be positioned in one or more latching states in a refueling operation, in which the reception coupling unit (31) comprises at least a detector (51, 71) of said latching states and at least a first indication means (55, 75) and/or a second indication means (65) for providing, respectively, to the pilot of the receiver aircraft (11) and/or to the crew of the tanker aircraft (13) indications that said cooperating latching means (39, 29) are positioned in one or more of said latching states, said detector (51, 71) being operatively connected, respectively, to a first indication means (55, 75) and/or to a second indication means (65).

    摘要翻译： 具有用于飞行中加油的接收机（11）的探头（25）的油船飞机（13）的软管和锥形装置（19,21）的接收联接单元（31）分别包括第一和第二 配合的锁定装置（39,29），其可以在加油操作中被定位在一个或多个闭锁状态，其中所述接收耦合单元（31）至少包括所述锁定状态的检测器（51,71），并且至少一个 第一指示装置（55,75）和/或第二指示装置（65），用于分别提供接收机飞机（11）和/或油船飞机（13）的飞行员的飞行员，指示所述协作 锁定装置（39,29）被定位在所述锁定状态中的一个或多个中，所述检测器（51,71）分别可操作地连接到第一指示装置（55,75）和/或第二指示装置 65）。

    Air to air refueling system with an autonomous electrical system
    30.
    发明公开
    Air to air refueling system with an autonomous electrical system 有权
    空中加油系统具有独立的电系统

    公开(公告)号：EP2543599A3

    公开(公告)日：2013-05-29

    申请号：EP12174656.4

    申请日：2012-07-02

    申请人： EADS Construcciones Aeronauticas, S.A.

    发明人： Fernández García, Francisco Javier

    IPC分类号： B64D39/02

    CPC分类号： B64D39/02

    摘要： A system for air to air refueling with an autonomous electrical system, comprising at least two hose and drogue devices (3, 5) housed in gondolas located underneath the wings of the aircraft, each refueling device comprising a plurality of components actuated by electrical actuators and its electrical system that is formed by two subsystems, each one of them comprising: a) Electric generator (11) actuated by a wind turbine (25) located in one of said gondolas; b) Energy storage device (19); c) Connection to the aircraft electrical system (15, 17); d) administrating device (21) equipped with means for ensuring the generation and storage of the energy required for responding to the electrical needs of the refueling system without recurring to the electrical system of the aircraft except in the event that the energy stared in said accumulation device (19) falls below a preset value.