公开(公告)号：US20070118254A1

公开(公告)日：2007-05-24

申请号：US11536128

申请日：2006-09-28

申请人： Greg Barnes ,  Eileen Horbury ,  Eric Jacobs ,  Kenneth Buckman

发明人： Greg Barnes ,  Eileen Horbury ,  Eric Jacobs ,  Kenneth Buckman

IPC分类号： G06F17/00

CPC分类号： G05D1/0858 ,  B64C27/57

摘要： A flight control system for a helicopter having a main rotor and a tail rotor is provided. The flight control system includes an automatic rotor speed control being configured to transition the main rotor and the tail rotor between a high speed and a low speed based upon a plurality of received information without requiring any pilot action, the plurality of received information comprising height above ground level, knot indicated air speed, outside air temperature, barometric altitude, pressure altitude, density altitude, and an engine operational status.

摘要翻译： 提供了一种具有主转子和尾转子的直升机飞行控制系统。 飞行控制系统包括自动转子速度控制，其被配置为基于多个接收到的信息在高速和低速之间转换主转子和尾部转子，而不需要任何导向动作，所述多个接收信息包括高度 地面水平，结指示空气速度，外部空气温度，气压高度，压力高度，密度高度和发动机运行状态。