Shift mechanism for aircraft control system

摘要: A shift mechanism for an aircraft control system reversibly shifting the of between a power mode and manual operation. The has stick input connection, primary surface output connection secondary connection. is made to bell crank-shaped housing which pivoted structure connections are connected idler arm connecting member, respectively, that housing. member moved by actuator first position wherein its pivotal aligned with second non-alignment. During this position, disconnected from arm. As consequence, during responsive movement (power mode) while (manual mode).