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84 条记录 (耗时 0.019 秒)

    Device for monitoring tiltable flaps on aircraft wings
    2.
    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

    申请人： Martin Richter ,  Dieter Lang

    发明人： Martin Richter ,  Dieter Lang

    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
    3.
    发明授权
    Arrangement for generating control commands for actuating flaps and slats of an aircraft 有权

    公开(公告)号：US06804586B2

    公开(公告)日：2004-10-12

    申请号：US10695618

    申请日：2003-10-27

    申请人： Martin Richter ,  Dieter Lang

    发明人： Martin Richter ,  Dieter Lang

    IPC分类号： G06F700

    CPC分类号： G05G1/04 ,  B64C13/04 ,  B64C13/503 ,  G05G9/00

    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

    申请人： Martin Richter ,  Dieter Lang

    发明人： Martin Richter ,  Dieter Lang

    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。

    Device and method for determining at least one flow parameter
    7.
    发明授权
    Device and method for determining at least one flow parameter 有权
    用于确定至少一个流量参数的装置和方法

    公开(公告)号：US08448523B2

    公开(公告)日：2013-05-28

    申请号：US13052452

    申请日：2011-03-21

    申请人： Martin Richter

    发明人： Martin Richter

    IPC分类号： G01F1/00

    CPC分类号： A61M5/16854 ,  A61M5/168 ,  G01F1/363 ,  G01F1/383 ,  G01F1/40 ,  G01F1/50

    摘要： A device for detecting at least one flow parameter includes a fluidic series connection of a first flow restriction, a first measurement area, a second flow restriction, and a second measurement area. A first sensor is provided for detecting a quantitative first measure of a pressure existing in the first measurement area. A second sensor is provided for detecting a quantitative second measure of a pressure existing in the second measurement area. An evaluator is provided which is configured to determine, while using the measures detected by the first and second sensors, a flow rate of a fluid flowing through the series connection, and/or to determine whether there is an occlusion of the first flow restriction, of the second flow restriction, or of a fluid area adjoining the second measurement area.

    摘要翻译： 用于检测至少一个流量参数的装置包括第一流量限制，第一测量区域，第二流量限制和第二测量区域的流体串联连接。 提供第一传感器用于检测存在于第一测量区域中的压力的​​定量第一测量。 提供第二传感器用于检测存在于第二测量区域中的压力的​​定量第二测量。 提供了一种评估器，其被配置为在使用由第一和第二传感器检测到的措施的同时确定流过串联连接的流体的流量和/或确定是否存在第一流量限制的阻塞， 的第二流量限制，或与第二测量区域相邻的流体区域。

    Apparatus and method for reducing motion blur in a video signal
    9.
    发明授权
    Apparatus and method for reducing motion blur in a video signal 失效
    用于减少视频信号中的运动模糊的装置和方法

    公开(公告)号：US08369644B2

    公开(公告)日：2013-02-05

    申请号：US12403657

    申请日：2009-03-13

    申请人： Oliver Erdler ,  Piergiorgio Sartor ,  Carsten Dolar ,  Martin Richter

    发明人： Oliver Erdler ,  Piergiorgio Sartor ,  Carsten Dolar ,  Martin Richter

    IPC分类号： G06K9/40

    CPC分类号： G06T5/003 ,  G06T5/20 ,  G06T2207/10016 ,  G06T2207/20201

    摘要： The present invention relates to an apparatus for reducing motion blur in a video signal, comprising an analysing means for determining edge characteristics of an input video signal and for providing motion estimation of an edge within said input video signal, generation means for generating a synthetic detail signal dependent on said edge characteristics and said motion estimation, and an adding means for adding the detail signal to the edge within the input video signal and outputting an output video signal.The present invention further relates to a method for reducing motion blur in a video signal.

    摘要翻译： 本发明涉及一种用于减少视频信号中的运动模糊的装置，包括用于确定输入视频信号的边缘特性并用于提供所述输入视频信号内的边缘的运动估计的分析装置，用于产生合成细节的产生装置 信号取决于所述边缘特性和所述运动估计，以及加法装置，用于将细节信号加到输入视频信号内的边缘并输出输出视频信号。 本发明还涉及一种用于减少视频信号中的运动模糊的方法。

    AIRCRAFT HAVING A VERTICAL LIFT SYSTEM
    10.
    发明申请
    AIRCRAFT HAVING A VERTICAL LIFT SYSTEM 有权
    具有垂直升降系统的飞机

    公开(公告)号：US20120138751A1

    公开(公告)日：2012-06-07

    申请号：US13322486

    申请日：2010-05-26

    申请人： Martin Richter ,  Peter Lücken

    发明人： Martin Richter ,  Peter Lücken

    IPC分类号： B64C3/58 ,  B64C13/16

    CPC分类号： B64C13/503 ,  B64D45/0005 ,  B64D2045/001

    摘要： An aircraft having a high lift system, including a control computer, high lift bodies on each wing, a drive coupled to these, an activation device connected to the drive via an analog connection, an input device, and sensors detecting a state of the high lift bodies connected via analog lines to the activation device. The input device connects via a digital connection to the activation device for transmitting commands for adjusting the high lift bodies. The activation device is installed in the payload area of the fuselage and in an area extending from a location spaced from the front of the wingbox by a distance of one third of the fuselage length extending from there to the aircraft's tip, as far as a location spaced from the rear of the wingbox by a distance of one third of the fuselage length extending from there to the aircraft's tail end.

    摘要翻译： 具有高升力系统的飞行器，包括控制计算机，每个机翼上的高升降体，连接到其上的驱动装置，通过模拟连接连接到驱动器的启动装置，输入装置和检测高位状态的传感器 电梯通过模拟线连接到激活装置。 输入设备通过数字连接连接到激活装置，用于发送用于调节高升降体的命令。 激活装置安装在机身的有效载荷区域中，并且在从与翼箱的前部间隔开的位置延伸距离从机身长度延伸到飞机尖端的距离的距离的距离为止， 与机翼后部间隔距离从机身长度延伸到飞机尾端的机身长度的三分之一。