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
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT | 2008 |
|
RU2466907C1 |
| AIRCRAFT WING | 1998 |
|
RU2148526C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2742496C2 |
| MULTI-FUNCTION SHIP STATIONING AIRCRAFT, ITS CONTROLLING AND INDICATING SYSTEM ACCORDING TO AIRCRAFT INCIDENCE ANGLE | 2010 |
|
RU2442724C1 |
| SHORT TAKE-OFF AND LANDING AIRCRAFT | 2020 |
|
RU2752104C1 |
| METHOD OF IMPROVING AIRCRAFT MANOEUVRING CHARACTERISTICS DURING FINAL STAGE OF RUNWAY APPROACH BEFORE LANDING AND SUBSEQUENT FLAREOUT (VERSIONS) | 2005 |
|
RU2384874C2 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2021 |
|
RU2805888C2 |
| SUPERSONIC CONVERTIPLANE WITH X-SHAPED WING | 2015 |
|
RU2621762C1 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| TWIN-FUSELAGE ROTORCRAFT DRONE | 2012 |
|
RU2502641C1 |
