| 摘要 |
FIELD: transport.SUBSTANCE: invention relates to aircraft lift increasing ACS with slats 21, 22 to be arranged in various configurations: cruising flight, flight in holding area, takeoff and landing. Proposed system consists of slat control device 25 coupled via control linkage 25 with slat drive system 23, 24 and operational unit 7 connected with said slat device 26 to input slat control commands. Said slat device 26 is designed to compute configurations of slats 21, 22, direction of configurational variation of slat adjustment automatic components depending upon flight conditions data and/or other data essential for aircraft control. Note here that said slat control device 26 may automatically switch takeoff and landing operating conditions and is intended for automatic generation of commands to cause changing the configuration subject to flight speed.EFFECT: higher reliability, optimised takeoff and landing conditions.21 cl, 17 dwg |
