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    • 2. 发明申请
    • ACTIVE VIBRATION CONTROL SYSTEMS AND METHODS FOR VEHICLES
    • 主动振动控制系统和车辆方法
    • US20150307186A1
    • 2015-10-29
    • US14441876
    • 2013-11-12
    • Doug A. SWANSONDavid W. EDEALDouglas G. PEDERSENDavid CLARKLORD CORPORATION
    • Doug A. SWANSONDavid W. EDEALDouglas G. PEDERSENDavid CLARK
    • B64C27/00F16F15/00
    • B64C27/001B64C2027/004F16F15/002G05D19/02
    • Active vibration control systems (100) and methods are provided herein. Systems (100) are expandable and include a plurality of vibration control devices (110) and at least a first controller (102) digitally linked with a second controller (104) via an interface (108). The first and the second controllers exchange information for generation of a force control command (FCC) either the first or second controller. The FCC is then executed at a first vibration control device (110) of the plurality of vibration control devices (FG) for providing active vibration control within a vehicle. A method of providing vibration control in a vehicle includes providing a plurality of active vibration control devices (100) and providing at least a first controller (102) digitally linked with a second controller (104). The method further includes generating a FCC using information exchanged between the first and the second controllers. The method further includes sending the FCC to a first vibration control device (110) of the plurality of devices (FG).
    • 本文提供了主动振动控制系统(100)和方法。 系统(100)是可扩展的并且包括多个振动控制装置(110)和至少第一控制器(102),其经由接口(108)与第二控制器(104)数字联接。 第一和第二控制器交换用于产生第一或第二控制器的力控制命令(FCC)的信息。 然后,在多个振动控制装置(FG)的第一振动控制装置(110)处执行FCC,以在车辆内提供主动振动控制。 一种在车辆中提供振动控制的方法包括提供多个主动振动控制装置(100)并且提供至少与第二控制器(104)数字连接的第一控制器(102)。 该方法还包括使用在第一和第二控制器之间交换的信息来生成FCC。 该方法还包括将FCC发送到多个设备(FG)的第一振动控制设备(110)。
    • 7. 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。