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    • 3. 发明申请
    • ACTIVE VIBRATION CONTROL DEVICES, SYSTEMS, AND METHODS
    • 主动振动控制装置,系统和方法
    • US20150375857A1
    • 2015-12-31
    • US14759132
    • 2014-01-17
    • Doug A. SWANSONPaul R. BLACKJihan RYUSteve C. SOUTHWARDDoug G. PEDERSENLORD CORPORATION
    • Doug A. SWANSONPaul R. BLACKJihan RYUSteve C. SOUTHWARDDoug G. PEDERSEN
    • B64C27/00
    • B64C27/001B64C2027/004
    • Improved active vibration control (AVC) devices (20), systems, and related methods are provided herein. An AVC device (20) includes a controller (24) adapted to receive real-time aircraft information and adjust at least one control parameter as a function of the real-time aircraft information is provided. An AVC device is adapted to detect changes in real-time aircraft information, as the aircraft moves from a steady state to transient performance, low and high air speeds, or vice versa. An AVC system (e.g., AVCS) includes one or more sensors (22), one or more actuators (26), and a controller (24) adapted to receive real-time aircraft information and adjust at least one control parameter. In some aspects, a method of controlling vibration within an aircraft includes receiving vibration information from at least one sensor (22), receiving real-time aircraft information from an avionics system (40), adjusting at least one control parameter used in a control algorithm, and generating a force command.
    • 本文提供了改进的主动振动控制(AVC)装置(20),系统和相关方法。 AVC设备(20)包括适于接收实时飞行器信息并根据提供的实时飞行器信息调整至少一个控制参数的控制器(24)。 AVC设备适用于当飞机从稳定状态转移到瞬时性能,低和高的空气速度时反过来检测实时飞机信息的变化,反之亦然。 AVC系统(例如,AVCS)包括一个或多个传感器(22),一个或多个致动器(26)和适于接收实时飞行器信息并调整至少一个控制参数的控制器(24)。 在一些方面,一种控制飞行器内的振动的方法包括从至少一个传感器接收振动信息,从航空电子系统(40)接收实时飞机信息,调整控制算法中使用的至少一个控制参数 ,并产生强制命令。