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公开(公告)号：EP2343240A3
公开(公告)日：2015-02-18
申请号：EP11150056.7
申请日：2011-01-04
IPC分类号： B64D39/06
CPC分类号： B64D39/06 , Y10T137/598
摘要： System (10) for disconnecting the nozzle (1) of a boom from a receptacle (2) to which the nozzle (1) is connected for fuel transfer, comprising latches (3) which are situated in the nozzle (1) and engage with latch-pins (5) arranged in the said receptacle (2), characterized in that the system (10) comprises a receptacle disconnection system (20) which operates the latch-pins (5) of the receptacle (2) and a nozzle disconnection system (30) which operates the latches (3) of the nozzle (1) such that, when an operator performs normal disconnection of the nozzle (1), the system (10) sends a first signal (21) to the receptacle (2) so that its latch-pins (5) are retracted in order to release the latches (3) of the nozzle (1) and, in parallel, sends a second signal (31) to the nozzle (1) so that the latches (3) of the nozzle (1) are retracted and release the said nozzle (1).
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公开(公告)号：EP2636600B1
公开(公告)日：2014-10-29
申请号：EP12382085.4
申请日：2012-03-07
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43.发明公开An improved monolithic fan cowl of an aircraft engine and a manufacturing method thereof 有权Triebwerksverkleidung und dessen Herstellungsverfahren
公开(公告)号：EP2774854A1
公开(公告)日：2014-09-10
申请号：EP13382070.4
申请日：2013-03-04
CPC分类号： F01D9/02 , B29C70/44 , B29D99/0014 , B64D29/00
摘要： The invention provides a fan cowl (11) of an aircraft engine made of a composite material having an optimized structure for withstanding the expected loads and for being able to be manufactured as a monolithic ensemble. The structure comprise a skin (13), frames (15) of a closed cross-section arranged in a transverse direction to the longitudinal axis of the aircraft and longitudinal beams (17, 19) comprising first parts (21) of a closed cross-section to be superimposed to the transverse frames (15) in their crossing zones and second parts (23) of an open cross-section in zones not crossing transverse frames (15) having their webs (41) arranged in a same plane. The invention also refers to a manufacturing method of said fan cowl (11).
摘要翻译： 本发明提供了一种由具有优化结构的复合材料制成的飞机发动机的风扇罩（11），用于承受预期的载荷并且能够被制造为单体组合。 所述结构包括皮肤（13），所述框架（15）具有沿着所述飞行器的纵向轴线的横向方向布置的封闭横截面，并且所述纵向梁（17,19）包括封闭横截面的第一部分（21） 其横截面和横向框架的横截面的第二部分（23）在未穿过横向框架（15）的区域中叠置，横向框架（15）具有布置在同一平面内的横向框架（15）。 本发明还涉及所述风扇罩（11）的制造方法。
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44.发明公开
公开(公告)号：EP2664896A1
公开(公告)日：2013-11-20
申请号：EP12708877.1
申请日：2012-01-13
发明人： LORENZO PEÑA, Eladio
IPC分类号： G01D3/036
摘要： Device for providing electrical signals with high immunity to noise. The invention develops a device for processing electrical signals (100) coming from a measurement sensor (60), said sensor (60) being subjected to noise disturbances caused by radio interference and lightning effects, such that said device uses a single current-loop cable (70), through which passes the electrical signal (100) encoded according to the signal time (Ta) and repetition time (Tr) of the current wave of said signal (100), such that said signal (100) contains an upper current state (10) and a lower current state (20) whose values are outside the decision window that activates a reading device (4) in the device, which reads the electrical signal (100) coming from the sensor.
摘要翻译： 装置，用于提供电信号具有高抗噪声。 本发明开发出了一种用于处理从一个测量传感器（60），所述传感器（60）来的电信号（100）经受由无线电干扰和雷电的影响引起的噪音干扰，检查所述装置使用单个电流回路电缆 （70），通过该传递编码雅丁到信号的时间（Ta）和所述信号（100）的电流波的重复时间（TR）的电信号（100），求这就是说信号（100）包含在上电流 状态（10）和较低的电流状态（20），其值即激活在装置中，其读取的电信号（100）的读取装置（4）的决定窗外来自传感器。
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公开(公告)号：EP2554474A1
公开(公告)日：2013-02-06
申请号：EP11382272.0
申请日：2011-08-05
IPC分类号： B64C25/58
CPC分类号： B64C25/08 , B64C25/58 , B64C2025/008
摘要： Adjusting device (1) for an aircraft landing gear shock absorber (2), such that the length (3) of said shock absorber (2) can be varied to change the aircraft attitude for operations on ground, wherein the adjusting device (1) is directly connected to a shock absorber (2) by a supply line (16), the adjusting device (1) comprising an actuating element (13) that moves in a chamber (17) filled with a fluid (20), the actuating element (13) being displaced by means of a drive shaft (12) driven by a driving device (11), the displacement of the actuating element (13) in the chamber (17) causing the addition or removal of fluid (20) in the shock absorber (2), therefore varying the length (3) of said shock absorber (2). The invention also refers to an aircraft landing gear comprising such an adjusting device (1).
摘要翻译： 其特征在于，所述调节装置（1）包括用于飞机起落架减震器（2）的调节装置（1），使得所述减震器（2）的长度（3） 通过供应管线（16）直接连接到减震器（2），所述调节装置（1）包括在填充有流体（20）的腔室（17）中移动的致动元件（13），所述致动元件 （13）通过由驱动装置（11）驱动的驱动轴（12）移动，致动元件（13）在腔室（17）中的移位导致添加或移除流体 减震器（2），因此改变所述减震器（2）的长度（3）。 本发明还涉及包括这种调节装置（1）的飞机起落架。
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公开(公告)号：EP2543599A2
公开(公告)日：2013-01-09
申请号：EP12174656.4
申请日：2012-07-02
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.
摘要翻译： 一种用自主电气系统进行空气加油的系统，包括容纳在位于飞行器机翼下方的吊船中的至少两个软管和冷水装置（3,5），每个加油装置包括由电致动器致动的多个部件， 其电气系统由两个子系统形成，其中的每一个包括：a）由位于所述吊船之一中的风力涡轮机（25）致动的发电机（11）; b）储能装置（19）; c）连接飞机电气系统（15,17）; d）管理装置（21），其配备有用于确保响应于加油系统的电力需要所需的能量的产生和存储的装置，而不会重复飞行到飞行器的电气系统，除非在所述累积中凝视的能量 设备（19）下降到预设值以下。
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公开(公告)号：EP2535272A1
公开(公告)日：2012-12-19
申请号：EP11382195.3
申请日：2011-06-13
IPC分类号： B64D39/00
摘要： Actuation system for controlling the movement of a telescopic beam (20) with respect to a structural beam (10) in in-flight refueling operations, comprising at least two sensing devices, a first sensing device (30) and a second sensing device (40), measuring physical magnitudes of at least two different mechanical elements of the actuation system, such that there exists a kinematics relationship between said at least two different mechanical elements, the actuation system further comprising a control device (50) checking the coherence of said physical magnitudes measured with respect to the kinematics relationship. The invention also refers to an aircraft comprising such an actuation system.
摘要翻译： 用于在飞行中加油操作中控制伸缩梁（20）相对于结构梁（10）的运动的致动系统，包括至少两个感测装置，第一感测装置（30）和第二感测装置（40） ），测量所述致动系统的至少两个不同机械元件的物理量值，使得在所述至少两个不同机械元件之间存在运动学关系，所述致动系统还包括控制装置（50），其检查所述物理 相对于运动学关系测量的幅度。 本发明还涉及包括这种致动系统的飞行器。
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公开(公告)号：EP2466251A1
公开(公告)日：2012-06-20
申请号：EP10382339.9
申请日：2010-12-16
发明人： Huertos Sanz, Rafael
CPC分类号： G01B3/563 , B64D45/0005 , G01B21/042
摘要： Device (11) for measuring deflected angles between a mobile surface (3) and a fixed surface (5) to which the mobile surface (3) is connected along a hinge axis, comprising: first and second bases (13, 15) to be mounted, respectively, in said mobile and fixed surfaces (3, 5); an angular displacement transducer (29) installed on said first base (13) and connected to a measuring equipment able to provide the measurement in degrees; a cinematic mechanism (12) supported by said first and second bases (13, 15) and arranged for translating the angle (β) between the mobile surface (3) and the fixed surface (5) to said angular displacement transducer (29). The invention also refers to a calibration method of a transducer used as an in-flight measuring device of the deflection angle between an aircraft mobile surface (3) and an aircraft fixed surface (5) using said device (11).
摘要翻译： 用于测量移动表面（3）和可移动表面（3）沿着铰链轴线连接的固定表面（5）之间的偏转角度的装置（11），包括：第一和第二基座（13,15） 分别安装在所述移动和固定表面（3,5）中; 安装在所述第一基座（13）上并连接到能够以度数提供所述测量的测量设备的角位移传感器（29）; 由所述第一和第二基座（13,15）支撑并被布置成将所述移动表面（3）和所述固定表面（5）之间的角度（2）平移到所述角位移换能器（29）的电影机构（12）。 本发明还涉及使用所述装置（11）作为飞行器移动表面（3）和飞机固定表面（5）之间的偏转角度的飞行中测量装置的换能器的校准方法。
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50.发明公开Method and system for assembling components 审中-公开Verfahren und System zur Zusammenstellung von Komponenten
公开(公告)号：EP2405402A1
公开(公告)日：2012-01-11
申请号：EP10382187.2
申请日：2010-07-06
IPC分类号： G06T19/00
CPC分类号： G06T19/006
摘要： System (1) for enhancing the assembly of components in an environment (10) using augmented reality techniques the system (1) comprising: an input module (7), which obtains both virtual data and real data taken in real-time of the component (100) that is to be assembled by an operator and of the environment (10); and an augmented reality module (8), in which the position and orientation of the data is determined for the positioning of the virtual data over the real data by means of a plurality of markers, the virtual data and the real data being combined in augmented reality in real-time. The invention also refers to a method for assembling components (100) in an environment (10) using augmented reality techniques.
摘要翻译： 1.一种系统（1），用于使用增强现实技术增强环境（10）中部件的组装，所述系统（1）包括：输入模块（7），其获得实时数据和实时数据 （100），其由操作者和环境（10）组装; 以及增强现实模块（8），其中通过多个标记确定数据的位置和取向用于通过多个标记在真实数据上定位虚拟数据，虚拟数据和实际数据被组合在增强中 实时实时。 本发明还涉及使用增强现实技术在环境（10）中组装部件（100）的方法。
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