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41. 发明申请

US20130195464A1 SYSTEM FOR OPTICAL OPEN SPACE DATA COMMUNICATION BASED ON DISCRETE OUTPUT LEVELS 有权
标题翻译：基于离散输出电平的光学开放空间数据通信系统
公开(公告)号：US20130195464A1
公开(公告)日：2013-08-01
申请号：US13749111
申请日：2013-01-24
申请人： EADS Deutschland GmbH
发明人： Thilo Fath , Christian Blumm , Josef Schalk , Nikolaus Peter Schmitt , Christoph Heller
IPC分类号： H04B10/114
CPC分类号： H04B10/114 , H04B10/1141
摘要： A system for open space data communication comprising a transmitting device and an optical receiver using multiple varying levels of emitted radiation output. The transmitting device includes multiple emitter groups that are capable of being switched on and off and each of which can be activated in parallel to emit fixed, varying radiation outputs. A total radiation output emitted by the transmitting device is defined by a sum of the emitted radiation outputs of the emitter groups, wherein to transmit a bit vector (b0 . . . bn) an emitter group assigned to a most significant bit (b0) emits a maximum radiation output Pmax and emitter groups assigned to the less significant bits (b1 . . . bn) of the bit vector emit radiation outputs: Px=Pmax/2x where x=1 . . . n.
摘要翻译：一种用于开放空间数据通信的系统，包括发射装置和使用多个发射的辐射输出的多个变化等级的光接收机。发射装置包括能够被接通和断开的多个发射极组，并且每个发射极组可以被并联激活以发射固定的，变化的辐射输出。由发射装置发射的总辐射输出由发射体组的发射辐射输出的总和来定义，其中为了传输分配给最高有效位（b0）的发射极组（b0 ... bn）发射位矢量（b0 ... bn）分配给位向量的较低有效位（b1 ... bn）的最大辐射输出Pmax和发射极组发射辐射输出：Px = Pmax / 2x，其中x = 1。。。 n。

42. 发明申请

US20020016692A1 Method and device for detection of a defect in a sensor system 失效
标题翻译：用于检测传感器系统中的缺陷的方法和装置
公开(公告)号：US20020016692A1
公开(公告)日：2002-02-07
申请号：US09907516
申请日：2001-07-17
申请人： EADS DEUTSCHLAND GMBH
发明人： Andreas Langmeier , Winfried Lohmiller
IPC分类号： G01D018/00 , G01C019/00 , G06F019/00 , G01C025/00 , G01F025/00
CPC分类号： G01D3/08
摘要： A method for implementation in a measuring system containing a sensor system and an arithmetic unit for detection of a defect in the measuring system, wherein at least one state variable of the system is derived from at least one sensor value in the measuring system, wherein a cost function value based on deviation of the measured value y from the calibration as a function of a previously calculated state x is calculated for the respective measurement and the calculated squared deviation is then compared with a corresponding threshold value. An error is identified and if necessary appropriate action is taken if the threshold value is exceeded.
摘要翻译：一种用于在包含传感器系统和用于检测测量系统中的缺陷的运算单元的测量系统中实现的方法，其中系统的至少一个状态变量从测量系统中的至少一个传感器值导出，其中，针对各测量计算出基于作为先前计算的状态x的函数的校准的测量值y的偏差的成本函数值，然后将计算的平方偏差与相应的阈值进行比较。识别错误，如果需要，如果超过阈值，则采取适当的措施。

43. 发明申请

US20010023394A1 Process for designing flight controllers 有权
标题翻译：飞行控制器设计流程
公开(公告)号：US20010023394A1
公开(公告)日：2001-09-20
申请号：US09805896
申请日：2001-03-15
申请人： EADS Deutschland GmbH
发明人： Juergen Becker
IPC分类号： G06G007/48
CPC分类号： G05B13/024
摘要： Process for designing flight controllers, in which first for the rigid airplane and then for the elastic airplane the damping and the phase delay for each excitation frequency is determined, and the flight controller is adapted in such a manner that the structural responses to each excitation frequency for both the rigid airplane and the elastic airplane in the open control circuit outside two design fields, applicable to the elastic airplane, are laid around the instability points in the data field comprising damping and phase delay, whereby for the design of the elastic airplane between the phase delays of null270 degrees and null495 degrees, a damping exceeding null6 dB is allowed.
摘要翻译：用于设计飞行控制器的过程，其中首先为刚性飞机然后为弹性飞机确定每个励磁频率的阻尼和相位延迟，并且飞行控制器被调整为使得对每个激励频率的结构响应对于适用于弹性飞机的两个设计领域外的开放式控制电路中的刚性飞机和弹性飞机都围绕包括阻尼和相位延迟的数据场中的不稳定点，由此为了设计弹性飞机在允许-270度和-495度的相位延迟，阻尼超过-6 dB。

44. 发明申请

US20010019092A1 Cable holder for attaching cables in a vehicle 失效
标题翻译：用于将电缆连接在车辆中的电缆支架
公开(公告)号：US20010019092A1
公开(公告)日：2001-09-06
申请号：US09800134
申请日：2001-03-05
申请人： EADS DEUTSCHLAND GMBH
发明人： Siegmund Koziol
IPC分类号： F16L003/22
CPC分类号： H02G3/26 , Y10S248/90 , Y10S248/909
摘要： A cable holder for attachment of cables in a vehicle structure is formed as an elongated plate provided with indicator markings at predetermined spacing along longitudinal edges of the plate so that the plate can be divided into plate segments of determined length at the markings. Two rows of retainer elements which form open loops at the upper surface of the plate are provided. The retainer elements are adapted to secure the connectors of the cables to the plate. The retainer elements in one row are longitudinally offset from the retainer elements of the other row such that a retainer element in one row extends between two retainer elements in the other row.
摘要翻译：形成用于将电缆连接在车辆结构中的缆线架作为细长板，该板沿着板的纵向边缘以预定的间隔设置指示标记，使得板可以在标记处被划分成具有确定长度的板段。提供了两排在板的上表面形成开环的保持元件。保持器元件适于将电缆的连接器固定到板上。一排中的保持器元件与另一排的保持器元件纵向偏移，使得一列中的保持器元件在另一排中的两个保持器元件之间延伸。

45. 发明申请

US20010011359A1 Reconfiguration procedure for an error-tolerant computer-supported system with at least one set of observers 审中-公开
标题翻译：具有至少一组观察者的容错计算机支持系统的重新配置程序
公开(公告)号：US20010011359A1
公开(公告)日：2001-08-02
申请号：US09768419
申请日：2001-01-24
申请人： EADS DEUTSCHLAND GMBH
发明人： Thomas Kohler , Winfried Lohmiller
IPC分类号： G06F011/00
CPC分类号： G05B9/03
摘要： Reconfiguration procedure for an error-tolerant system with at least one set of observers that are each formed from various combinations of sensors and a system model whereby the set of observers cause time-dependent operating statuses to fulfill system functions, whereby past deviations of the measured system status of this combination of one of the estimated system statuses of the assigned observers are used to determine the error status of each of these combinations of sensors for each time interval.
摘要翻译：具有至少一组观察者的容错系统的重新配置过程，每组观察者各自由传感器的各种组合和系统模型形成，由此观察者组会引起时间相关的操作状态来实现系统功能，由此过去偏差使用分配的观察者的估计系统状态之一的组合的系统状态来确定每个时间间隔的传感器的这些组合中的每一个的错误状态。

46. 发明授权

US09625145B2 High frequency-stabilized combustion in aircraft gas turbines 有权
公开(公告)号：US09625145B2
公开(公告)日：2017-04-18
申请号：US14313474
申请日：2014-06-24
申请人： EADS Deutschland GmbH
发明人： Juergen Steinwandel , Johannes Stuhlberger
IPC分类号： F02C1/00 , F23C99/00 , F23N5/00 , F23R3/28 , F02C7/00
CPC分类号： F23C99/001 , F02C7/00 , F23N5/006 , F23N2041/20 , F23R3/28 , F23R2900/00009 , Y02T50/677
摘要： A gas turbine includes a combustion chamber and a microwave source to produce microwave radiation. The gas turbine is arranged to guide the microwave radiation into a cavity of the combustion chamber. Due to the microwave radiation, in the cavity of the combustion chamber, combustion in the cavity may be supported and thus lean operation of the gas turbine is made possible.

47. 发明授权

US09558715B2 Interactive passenger cabin unit and method for controlling presentations thereon 有权
标题翻译：互动客舱单元及其上的演示控制方法
公开(公告)号：US09558715B2
公开(公告)日：2017-01-31
申请号：US14032237
申请日：2013-09-20
申请人： EADS Deutschland GmbH
发明人： Marc Velten , Daniel Meister , Rene Schubotz , Jens Gaertner
IPC分类号： G09G5/14 , G06F3/16 , G06F3/041 , G06F3/01 , B64D11/00 , B64D45/00
CPC分类号： G09G5/14 , B64D11/0015 , B64D2011/0061 , B64D2045/007 , G06F3/017 , G06F3/0412 , G06F3/16
摘要： A passenger cabin unit of a passenger transportation vehicle includes a display device configured to present visual effects, information and images. The display device is disposed so as to completely or substantially cover surfaces of the passenger cabin unit which are visible from inside the passenger cabin unit. The display device is divided into first display regions and a second display region. Each of the first display regions is assigned to a respective individual passenger or group of passengers. A plurality of passenger command input devices are each disposed in a respective one of the first display regions and are each configured to be operated by the respective individual passenger or group of passengers to control visual presentation. A crew command input device is configured to be operated by cabin crew to control visual presentation on some or all of the first display regions and on the second display region.
摘要翻译：客运车辆的客舱单元包括被配置为呈现视觉效果，信息和图像的显示装置。显示装置设置成完全或基本上覆盖从乘客舱单元内部可见的客舱单元的表面。显示装置分为第一显示区域和第二显示区域。每个第一显示区域被分配给各个乘客或乘客组。多个乘客命令输入装置分别设置在第一显示区域中的相应一个中，并且各自被配置为由各个乘客或乘客组操作以控制视觉呈现。船员命令输入装置被配置为由机组人员操作以控制在部分或全部第一显示区域和第二显示区域上的视觉呈现。

48. 发明授权

US09475148B2 Friction stir processing method for a workpiece having surface coating 有权
标题翻译：具有表面涂层的工件的摩擦搅拌处理方法
公开(公告)号：US09475148B2
公开(公告)日：2016-10-25
申请号：US15146399
申请日：2016-05-04
申请人： EADS Deutschland GmbH
发明人： Juegren Silvanus , Tommy Brunzel
IPC分类号： B23K20/22 , B23K20/12
CPC分类号： B23K20/122 , B23K20/1225 , B23K20/1255 , B23K20/22
摘要： A friction stir processing tool having a shoulder, which is implemented on a body, and which has a friction surface for pressing against at least one workpiece at least partially provided with a surface coating, and a friction reducing unit for reducing the friction resistance between the surface coating and the friction surface.
摘要翻译：一种摩擦搅拌处理工具，其具有肩部，其实施在主体上，并且具有用于按压至少一个至少部分地设置有表面涂层的工件的摩擦表面;以及摩擦减小单元，用于减小所述摩擦阻力表面涂层和摩擦表面。

49. 发明授权

US09431704B2 Antenna apparatus and method for electronically pivoting a radar beam 有权
标题翻译：用于电子地枢转雷达波束的天线装置和方法
公开(公告)号：US09431704B2
公开(公告)日：2016-08-30
申请号：US13888909
申请日：2013-05-07
申请人： EADS Deutschland GmbH
发明人： Volker Ziegler , Benedikt Schulte
IPC分类号： H01Q3/34 , H01Q1/28 , H01Q3/22 , G01S7/03 , G01S7/06 , G01S13/42 , G01S13/94 , G01S13/02
CPC分类号： H01Q3/34 , G01S7/03 , G01S7/062 , G01S13/426 , G01S13/94 , G01S2013/0245 , H01Q1/28 , H01Q3/22
摘要： An antenna apparatus for a radar sensor having a plurality of individual antenna devices that interact through interference to generate and/or receive a radar beam at a predetermined angle of transmission and/or reception. The individual antenna devices are provided with a radar signal and are arranged such that a first angle of transmission and/or reception of the radar beam is determined via an analog beam formation and a second angle of transmission and/or reception of the radar beam is determined via a digital beam formation. The antenna apparatus further includes a feed device configured to generate the radar signal. In addition, the radar beam can be electronically pivoted. Also, an aircraft can include the antenna apparatus.
摘要翻译：一种用于雷达传感器的天线装置，具有多个单独的天线装置，其通过干扰相互作用，以在预定的发射和/或接收角度产生和/或接收雷达波束。各个天线装置设置有雷达信号，并且被布置成使得经由模拟波束形成确定雷达波束的第一发射角度和/或接收角度，并且雷达波束的发射和/或接收的第二角度是通过数字波束形成确定。天线装置还包括配置成产生雷达信号的馈送装置。此外，雷达波束可以电子枢转。此外，飞机可以包括天线装置。

50. 发明申请

US20160185459A1 Auxiliary Device for High-Flying Aircraft 审中-公开
标题翻译：高飞机辅助装置
公开(公告)号：US20160185459A1
公开(公告)日：2016-06-30
申请号：US14654181
申请日：2013-12-18
申请人： ASTRIUM GMBH , EADS DEUTSCHLAND GMBH
发明人： Andreas KIEFER , Jens FEDERHEN , Dieter DRAGON , Werner SCHOLZ
IPC分类号： B64D27/26 , B64D5/00 , B64D27/24 , B64D41/00
CPC分类号： B64D27/26 , B64C39/024 , B64C2201/042 , B64C2201/082 , B64C2201/122 , B64D5/00 , B64D27/02 , B64D27/24 , B64D41/00 , B64D2211/00 , Y02T50/44 , Y02T50/55 , Y02T50/62
摘要： An auxiliary device is provided for a high-altitude airplane. The auxiliary device includes a drive, which is independent of the airplane, for the ascent of the airplane into the stratosphere. The airplane is releasably coupled to the auxiliary device. The auxiliary drive is releasable from the airplane altitude on the latest on reaching a predetermined mission.
摘要翻译：为高空飞机提供辅助装置。辅助装置包括独立于飞机的驱动器，用于使飞机上升到平流层。飞机可释放地联接到辅助装置。辅助驱动器在达到预定任务时可从最近的飞机高度释放。

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