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    • 63. 发明授权
    • Device for monitoring tiltable flaps on aircraft wings
    • 用于监控飞机机翼上的倾斜襟翼的装置
    • US07354022B2
    • 2008-04-08
    • US11316084
    • 2005-12-21
    • Martin RichterDieter Lang
    • Martin RichterDieter Lang
    • G05D1/00
    • B64D45/0005B64D2045/001
    • 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.
    • 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。