FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to control over aircraft airfoils. The flap is driven by, at least, two devices 11, 12, 13, 14 that allow actuation by, at least, one actuator 30. Brake is arranged at, at least, one actuator 30 for every driven flap. Brake actuation allows fixing set state of appropriate actuator 30 at following steps: separate actuation of every brake, activation of every actuator by engine drive, termination of flap actuation on changing controlled flap set state by predefined amount.
EFFECT: higher reliability and better controllability.
17 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT WITH LIFT INCREASING SYSTEM | 2010 |
|
RU2494931C2 |
| AIRCRAFT LANDING FLAP WITH FLAP ERROR DETECTOR | 2006 |
|
RU2423295C2 |
| AIRCRAFT WING TRAILING EDGE CONTROL SURFACE | 2006 |
|
RU2405715C2 |
| AIRCRAFT CONTROL SYSTEM | 2003 |
|
RU2235043C1 |
| AIRCRAFT WING AND WING STRUCTURE WITH FLOW INFLUENCING MEANS | 2010 |
|
RU2488521C2 |
| STREAMLINED BODY AND SYSTEM TO CREATE INCREASED LIFT WITH SAID STREAMLINED BODY | 2009 |
|
RU2494923C2 |
| SET OF FLAPS ON WING OF FIXED-WING AIRCRAFT | 2004 |
|
RU2346851C2 |
| AEROSTAT TRAJECTORY CONTROL SYSTEM | 1999 |
|
RU2238217C2 |
| LANDING FLAP DRIVE SYSTEM | 2006 |
|
RU2399554C2 |
| AIRCRAFT FLAPS MOVEMENT CONTROL SYSTEM AND METHOD | 2017 |
|
RU2728236C2 |
