发明名称 ACTIVE VIBRATION CONTROL DEVICES, SYSTEMS, AND METHODS
摘要 Improved active vibration control (AVC) devices, systems, and related methods are provided herein. An AVC device includes a controller 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, one or more actuators, and a controller 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, receiving real-time aircraft information from an avionics system, adjusting at least one control parameter used in a control algorithm, and generating a force command.
申请公布号 US2017008620(A1) 申请公布日期 2017.01.12
申请号 US201615163026 申请日期 2016.05.24
申请人 LORD Corporation 发明人 SWANSON Doug A.;BLACK Paul R.;RYU Jihan;SOUTHWARD Steve C.;PEDERSEN Doug G.
分类号 B64C27/00 主分类号 B64C27/00
代理机构 代理人
主权项 1. An active vibration control (AVC) device for use in aircraft, the AVC device comprising: a controller comprising: a first signaling interface for receiving real-time aircraft information communicated directly from an avionics system;a force command generating module configured to process the real-time aircraft information, adjust at least one control parameter as a function of the real-time aircraft information, and generate a force command using the adjusted control parameter; anda second signaling interface for outputting the electronic force command to one or more actuators.
地址 Cary NC US