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    • 8. 发明授权
    • Device and method for determining at least one flow parameter
    • 用于确定至少一个流量参数的装置和方法
    • US08448523B2
    • 2013-05-28
    • US13052452
    • 2011-03-21
    • Martin Richter
    • Martin Richter
    • G01F1/00
    • A61M5/16854A61M5/168G01F1/363G01F1/383G01F1/40G01F1/50
    • 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.
    • 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。
    • 10. 发明申请
    • AIRCRAFT HAVING A VERTICAL LIFT SYSTEM
    • 具有垂直升降系统的飞机
    • US20120138751A1
    • 2012-06-07
    • US13322486
    • 2010-05-26
    • Martin RichterPeter Lücken
    • Martin RichterPeter Lücken
    • B64C3/58B64C13/16
    • B64C13/503B64D45/0005B64D2045/001
    • 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.
    • 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。