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1.发明申请METHOD AND DEVICE FOR PROVIDING AUTOMATIC LOAD ALLEVIATION TO A HIGH LIFT SURFACE SYSTEM, IN PARTICULAR TO A LANDING FLAP SYSTEM, OF AN AIRCRAFT 有权用于向自动负载表示系统提供自动负载校正的方法和装置，特别是对于飞机的飞行板系统公开(公告)号：US20110084173A9
公开(公告)日：2011-04-14
申请号：US12086467
申请日：2006-12-08
IPC分类号： B64C13/16
CPC分类号： B64C13/16
摘要： A method and a device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft when a blockage occurs, wherein in response to a control signal emitted by a control device at least one high lift surface, which is actuated by means of a local mechanical final control element, is brought to a predetermined position by a central drive unit that is connected by way of a rotary shaft arrangement to the local final control element by generating a torque transmitted by the central drive unit to the rotary shaft arrangement. If a signal is registered that indicates that there is a blockage within the high lift surface system, the torque transmitted by the central drive unit to the rotary shaft arrangement is automatically reduced to a predetermined low torque value, and the position of the high lift surface system is fixed.
摘要翻译： 一种方法和装置，用于在发生堵塞时向飞行器的高升力表面系统（特别是着陆挡板系统）提供自动负载减轻，其中响应于由控制装置发射的控制信号，至少一个高升程 通过局部机械终控制元件致动的表面通过中心驱动单元被带到预定位置，该中心驱动单元通过旋转轴装置连接到局部最终控制元件，通过产生由中心传递的扭矩 驱动单元到旋转轴装置。 如果登记指示高升力面系统内存在阻塞的信号，则由中央驱动单元传递给旋转轴装置的扭矩自动降低到预定的低扭矩值，并且高升程面的位置 系统固定。
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2.发明申请METHOD AND DEVICE FOR PROVIDING AUTOMATIC LOAD ALLEVIATION TO A HIGH LIFT SURFACE SYSTEM, IN PARTICULAR TO A LANDING FLAP SYSTEM, OF AN AIRCRAFT 有权用于向自动负载表示系统提供自动负载校正的方法和装置，特别是对于飞机的飞行板系统公开(公告)号：US20100044518A1
公开(公告)日：2010-02-25
申请号：US12086467
申请日：2006-12-08
IPC分类号： B64C13/16
CPC分类号： B64C13/16
摘要： A method and a device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft when a blockage occurs, wherein in response to a control signal emitted by a control device at least one high lift surface, which is actuated by means of a local mechanical final control element, is brought to a predetermined position by a central drive unit that is connected by way of a rotary shaft arrangement to the local final control element by generating a torque transmitted by the central drive unit to the rotary shaft arrangement. If a signal is registered that indicates that there is a blockage within the high lift surface system, the torque transmitted by the central drive unit to the rotary shaft arrangement is automatically reduced to a predetermined low torque value, and the position of the high lift surface system is fixed.
摘要翻译： 一种方法和装置，用于在发生堵塞时向飞行器的高升力表面系统（特别是着陆挡板系统）提供自动负载减轻，其中响应于由控制装置发射的控制信号，至少一个高升程 通过局部机械终控制元件致动的表面通过中心驱动单元被带到预定位置，该中心驱动单元通过旋转轴装置连接到局部最终控制元件，通过产生由中心传递的扭矩 驱动单元到旋转轴装置。 如果登记指示高升力面系统内存在阻塞的信号，则由中央驱动单元传递给旋转轴装置的扭矩自动降低到预定的低扭矩值，并且高升程面的位置 系统固定。
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3.发明授权Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft 有权一种提供自动负载减轻的方法和装置，用于飞机的高升力面系统，特别是降落翼系统公开(公告)号：US08256718B2
公开(公告)日：2012-09-04
申请号：US12086467
申请日：2006-12-08
CPC分类号： B64C13/16
摘要： A method and a device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft when a blockage occurs, wherein in response to a control signal emitted by a control device at least one high lift surface, which is actuated by means of a local mechanical final control element, is brought to a predetermined position by a central drive unit that is connected by way of a rotary shaft arrangement to the local final control element by generating a torque transmitted by the central drive unit to the rotary shaft arrangement. If a signal is registered that indicates that there is a blockage within the high lift surface system, the torque transmitted by the central drive unit to the rotary shaft arrangement is automatically reduced to a predetermined low torque value, and the position of the high lift surface system is fixed.
摘要翻译： 一种方法和装置，用于在发生堵塞时向飞行器的高升力表面系统（特别是着陆翼片系统）提供自动负载减轻，其中响应于由控制装置发射的控制信号，至少一个高升程 通过局部机械终控制元件致动的表面通过中心驱动单元被带到预定位置，该中心驱动单元通过旋转轴装置连接到局部最终控制元件，通过产生由中心传递的扭矩 驱动单元到旋转轴装置。 如果登记指示高升力面系统内存在阻塞的信号，则由中央驱动单元传递给旋转轴装置的扭矩自动降低到预定的低扭矩值，并且高升程面的位置 系统固定。
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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
CPC分类号： B64D45/0005 , B64C13/42 , B64D2045/001 , Y02T50/44
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.
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公开(公告)号：US08814085B2
公开(公告)日：2014-08-26
申请号：US12991174
申请日：2009-05-05
IPC分类号： B64C3/38
CPC分类号： B64D45/0005 , B64C13/42 , B64D2045/001 , Y02T50/44
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.
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6.发明授权Method for manufacturing a bending transducer, a micro pump and a micro valve, micro pump and micro valve 有权弯曲换能器，微型泵和微型阀，微型泵和微型阀的制造方法公开(公告)号：US09410641B2
公开(公告)日：2016-08-09
申请号：US13604294
申请日：2012-09-05
申请人： Markus Herz , Martin Richter , Martin Wackerle
发明人： Markus Herz , Martin Richter , Martin Wackerle
CPC分类号： F16K99/0001 , F04B43/043 , F16K99/0015 , F16K99/0048 , F16K2099/008 , F16K2099/0094 , H01L41/0973 , Y10T29/49236
摘要： A method of manufacturing a bending transducer having a drive element and a membrane includes providing the membrane and the drive element and applying a production signal to the drive element during a bonding of the drive element to the membrane such that the drive element is pre-stressed after the bonding, wherein the production signal is of a same kind as an operation signal to operate the bending transducer.
摘要翻译： 制造具有驱动元件和膜的弯曲换能器的方法包括提供膜和驱动元件，并且在将驱动元件接合到膜时将驱动元件施加到驱动元件，使得驱动元件被预应力 在所述接合之后，其中所述生产信号与用于操作所述弯曲换能器的操作信号相同。
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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
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。
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8.发明申请METHOD FOR MANUFACTURING A BENDING TRANSDUCER, A MICRO PUMP AND A MICRO VALVE, MICRO PUMP AND MICRO VALVE 有权弯曲传感器，微型泵和微型阀门，微型泵和微型阀门的制造方法公开(公告)号：US20130055889A1
公开(公告)日：2013-03-07
申请号：US13604294
申请日：2012-09-05
申请人： Markus Herz , Martin Richter , Martin Wackerle
发明人： Markus Herz , Martin Richter , Martin Wackerle
CPC分类号： F16K99/0001 , F04B43/043 , F16K99/0015 , F16K99/0048 , F16K2099/008 , F16K2099/0094 , H01L41/0973 , Y10T29/49236
摘要： A method of manufacturing a bending transducer having a drive element and a membrane includes providing the membrane and the drive element and applying a production signal to the drive element during a bonding of the drive element to the membrane such that the drive element is pre-stressed after the bonding, wherein the production signal is of a same kind as an operation signal to operate the bending transducer.
摘要翻译： 制造具有驱动元件和膜的弯曲换能器的方法包括提供膜和驱动元件，并且在将驱动元件接合到膜时将驱动元件施加到驱动元件，使得驱动元件被预应力 在所述接合之后，其中所述生产信号与用于操作所述弯曲换能器的操作信号相同。
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公开(公告)号：US08369644B2
公开(公告)日：2013-02-05
申请号：US12403657
申请日：2009-03-13
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。
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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
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。
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