Device for monitoring tiltable flaps on aircraft wings
    1.
    发明授权
    Device for monitoring tiltable flaps on aircraft wings 有权
    用于监控飞机机翼上的倾斜襟翼的装置

    公开(公告)号:US07354022B2

    公开(公告)日:2008-04-08

    申请号:US11316084

    申请日:2005-12-21

    IPC分类号: G05D1/00

    CPC分类号: B64D45/0005 B64D2045/001

    摘要: A device for monitoring tiltable flaps on aircraft wings including rotary sensors at the rotary axis of the flap and associated with each actuating element. A rotation sensor is connected to the actuating elements by a spring band. The band is a coupled for angle transmission and the band is connected at a distance from the rotary axis. The spring band is stiff in the direction of rotation, while in the lateral direction, for the purpose of compensating for transverse movements of the actuating elements, the spring band is soft. For each flap, the signals of the rotary sensors, at decentralized monitoring devices to locate errors, are transmitted to an evaluation unit.

    摘要翻译: 一种用于监控飞机机翼上的可倾斜翼片的装置,包括在翼片的旋转轴线处的旋转传感器并与每个致动元件相关联。 旋转传感器通过弹簧带连接到致动元件。 该带是用于角度传输的连接,并且该带在与旋转轴线一定距离处连接。 弹簧带在旋转方向上是刚性的,而在横向方向上,为了补偿致动元件的横向运动,弹簧带是柔软的。 对于每个挡板,旋转传感器的信号在分散监视装置处定位错误,被传送到评估单元。

    Arrangement for generating control commands for actuating flaps and slats of an aircraft

    公开(公告)号:US06804586B2

    公开(公告)日:2004-10-12

    申请号:US10695618

    申请日:2003-10-27

    IPC分类号: G06F700

    摘要: An arrangement for generating control commands for controlling the slats and landing flaps of an aircraft includes two manually operable command input levers which are arranged directly side-by-side or as a “rod-within-rod” and are connected respectively by two linkages to two rotatable sensor disks that respectively cooperate with two sets of signal emitters that are electrically connected respectively to two control computers. The two levers and two linkages are coupled to form a single command transducer having two coupled parallel command transmission paths. Based on the signals of the signal emitters, the control computers generate actuating signals that are provided to actuators for adjusting the positions of the slats and landing flaps. A mechanical disconnect or jamming of one mechanical command transmission path or a malfunction or failure of one of the sensor arrangements will not cause a failure of the slat and flap command functions, because the other command transmission path will remain functional.

    Device for monitoring tiltable flaps on aircraft wings
    4.
    发明申请
    Device for monitoring tiltable flaps on aircraft wings 有权
    用于监控飞机机翼上的倾斜襟翼的装置

    公开(公告)号:US20060145028A1

    公开(公告)日:2006-07-06

    申请号:US11316084

    申请日:2005-12-21

    IPC分类号: B64C9/16

    CPC分类号: B64D45/0005 B64D2045/001

    摘要: In a device for monitoring tiltable flaps on aircraft wings it is proposed that rotary sensors in the rotary axis of the flap be associated with each actuating element, and a sensor rotation by way of a spring band be connected to the actuating element, as a coupler for angle transmission, at a distance to the rotary axis. The spring band is stiff in the direction of rotation, while in lateral direction, for the purpose of compensating for a transverse movements of the actuating elements, said spring band is soft. For each flap the signals of the rotary sensors, as decentralised monitoring devices to locate errors, are transmitted to an evaluation unit.

    摘要翻译: 在用于监测飞机机翼上的可倾斜襟翼的装置中,提出在翼片的旋转轴线上的旋转传感器与每个致动元件相关联,并且通过弹簧带将传感器旋转连接到致动元件,作为耦合器 用于角度传输,距离旋转轴。 弹簧带在旋转方向上是刚性的,而在横向方向上,为了补偿致动元件的横向运动,弹簧带是柔软的。 对于每个挡板,旋转传感器的信号作为分散监视装置来定位错误,被传送到评估单元。

    Pump Having a Filter Arrangement
    7.
    发明申请
    Pump Having a Filter Arrangement 有权
    具有过滤器布置的泵

    公开(公告)号:US20120063928A1

    公开(公告)日:2012-03-15

    申请号:US13228258

    申请日:2011-09-08

    IPC分类号: F04B53/00

    摘要: A pump for pumping a medium from a suction side to a pressure side includes a filter arrangement. The filter arrangement includes an inflow path, a first outflow path, and a second outflow path. A hydrophobic membrane filter is arranged between the inflow path and the first outflow path. A hydrophilic membrane filter is arranged between the inflow path and the second outflow path. At least one section of the hydrophobic membrane filter and one section of the hydrophilic membrane filter are located opposite each other at a distance of no more than 1 mm so that a gas bubble that moves along with a medium flowing in the inflow path comes into contact with the hydrophobic membrane filter during the movement. The first and second outflow paths of the filter arrangement are connected to the suction side of the pump.

    摘要翻译: 用于将介质从吸入侧泵送到压力侧的泵包括过滤器装置。 过滤器装置包括流入路径,第一流出路径和第二流出路径。 疏水膜过滤器布置在流入路径和第一流出路径之间。 亲水膜过滤器布置在流入路径和第二流出路径之间。 疏水膜过滤器的至少一个部分和亲水膜过滤器的一个部分以不大于1mm的距离彼此相对定位,使得与在流入路径中流动的介质一起移动的气泡接触 在移动期间使用疏水膜过滤器。 过滤器装置的第一和第二流出路径连接到泵的吸入侧。

    METHOD AND SYSTEM FOR REDUCING BLOCKING ARTEFACTS IN COMPRESSED IMAGES AND VIDEO SIGNALS
    8.
    发明申请
    METHOD AND SYSTEM FOR REDUCING BLOCKING ARTEFACTS IN COMPRESSED IMAGES AND VIDEO SIGNALS 审中-公开
    压缩图像和视频信号中减少阻塞特征的方法和系统

    公开(公告)号:US20110123121A1

    公开(公告)日:2011-05-26

    申请号:US12895037

    申请日:2010-09-30

    IPC分类号: G06K9/40 G06K9/48

    摘要: The present invention relates to a coding parameter independent method for reduction of blocking artefacts in a compressed image or video signal. For this purpose, the image is analysed in the vicinity of the block boundaries in order to measure the existence and strength of blocking artefacts and to detect image areas. Based on the analysis result map information for each pixel adjacent to a block boundary is generated. The filter mode for each block boundary is adaptively determined dependent on the map information and the image is filtered depending on the chosen filter mode.

    摘要翻译: 本发明涉及用于减少压缩图像或视频信号中的阻塞伪影的编码参数独立方法。 为了这个目的,在块边界附近分析图像,以便测量阻挡伪像的存在和强度并检测图像区域。 基于与块边界相邻的每个像素的分析结果映射信息被生成。 每个块边界的滤波器模式根据地图信息自适应地确定,并且根据所选择的滤波器模式对图像进行滤波。

    FAULT-TOLERANT ACTUATING SYSTEM FOR ADJUSTING FLAPS OF AN AIRCRAFT, COMPRISING ADJUSTMENT KINEMATICS WITH A FIXED PIVOT, AND A METHOD FOR MONITORING AN ACTUATING SYSTEM

    公开(公告)号:US20110062282A1

    公开(公告)日:2011-03-17

    申请号:US12991174

    申请日:2009-05-05

    IPC分类号: B64C13/24

    摘要: A fault-tolerant actuating system with at least one flap, adjustable on a respective wing of an aircraft, and with a control and monitoring device, includes: drive devices that are functionally connected to the control and monitoring device, with one of these drive devices in each case being associated with a flap, where each flap in each case is associated with a drive device, in each case including: two drive motors, two brake mechanisms, where each drive motor is associated with a brake mechanism for stopping rotation of the output of the respective drive motor, a differential that couples the outputs of the aforesaid to the aforesaid in a summing manner, an output shaft for coupling the output of the differential to drive connections, and a differential lock that is functionally connected to the control and monitoring device, which differential lock is coupled to the control and monitoring device in this manner, where each of the brake mechanisms as well as the differential lock can be operated by way of a command signal from the control and monitoring device; adjustment devices, that are coupled to the respective drive device associated with the flap, where each adjustment device in each case includes: a transmission gear unit, an adjustment mechanism and a position sensor that is functionally connected to the control and monitoring device for acquiring the adjustment state of the flap; where the control and monitoring device includes: an actuating function for generating command signals for the drive motors for adjusting the flap, a monitoring function by way of which a command signal is transmitted to both brake mechanisms and to the differential lock for operating the aforesaid when the control and monitoring device based on a comparison of sensor values of the position sensors on two different adjustment devices of a flap determines different adjustment states that exceed a predetermined extent, and a method for monitoring an actuating system.

    Plug-in connections
    10.
    发明授权
    Plug-in connections 有权
    插件连接

    公开(公告)号:US07793966B2

    公开(公告)日:2010-09-14

    申请号:US11596302

    申请日:2005-05-13

    IPC分类号: B60D1/62

    CPC分类号: B62D53/125 B60D1/64

    摘要: Disclosed is a plug-in coupling system for joining cables between a tractor and a trailer. The invention also relates to the individual components, i.e. the semitrailer coupling and the plug-in connector on which the invention is implemented. The cables between the tractor and the trailer are usually plugged into each other by hand. Automatic systems have not been successful on the market so far. The aim of the invention is therefore to create a plug-in coupling system which allows the supply cables to be connected in a comfortable and operationally safe manner when the trailer is joined to and disconnected from the tractor. Said aim is achieved, among other things, by disposing the socket in a stationary manner below the insertion hole on the semitrailer coupling while arranging the contact points of the plug below the king pin on the plug-in connector.

    摘要翻译: 公开了一种用于在拖拉机和拖车之间连接电缆的插入式联接系统。 本发明还涉及实现本发明的单个组件,即半挂车联轴器和插入式连接器。 拖拉机和拖车之间的电缆通常用手插入对方。 到目前为止,自动化系统在市场上还没有成功。 因此,本发明的目的是创建一种插入式联接系统,其允许当拖车接合到拖拉机并与拖拉机断开连接时以舒适和操作上安全的方式连接供电电缆。 所述目的通过在插塞式连接器的主销的下方将插头的接触点布置在半挂车联轴器上的插入孔的下方,以固定的方式设置插座来实现。