FIELD: flying vehicle control systems. SUBSTANCE: mechanical linkage connecting the electric drive with trimmer contains bell crank whose one end is articulated on fixed surface of wing or tail unit and other end is made in form of adjusting mechanism engageable with trimmer rod which is adjustable in length. EFFECT: extended functional capabilities of aircraft manual control system; change of loading characteristics of control levers. 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MANUAL CONTROL SYSTEM OF TRAINER AEROPLANE | 1993 |
|
RU2093419C1 |
| LANDING GEAR FRONT LEG WHEEL TURN CONTROL SYSTEM | 1992 |
|
RU2042575C1 |
| AIRCRAFT STEERING COLUMN | 2007 |
|
RU2356793C1 |
| AEROBATIC PLANE | 1992 |
|
RU2005662C1 |
| AIRPLANE CONTROL SYSTEM | 0 |
|
SU1762751A3 |
| THREE-DIMENSIONAL BOTTOM STATION FOR MANUAL CONTROL OF AIRCRAFT | 2014 |
|
RU2579250C2 |
| THREE-CORDINATE MANUAL AIRCRAFT CONTROL STATION | 2016 |
|
RU2647220C2 |
| LANDING GEAR UP LOCAL | 1992 |
|
RU2076827C1 |
| ULTRA LOW MASS AIRPLANE | 2005 |
|
RU2336200C2 |
| THREE-COORDINATE POST FOR DOUBLED MANUAL AIRCRAFT CONTROL | 2014 |
|
RU2579417C2 |
