FIELD: control of autonomous aerodynamic control surfaces of transport facility not interconnected by LH and RH pedals. SUBSTANCE: device has housing, levers of LH and RH pedals articulated on axles, link gears rigidly secured on respective axles and connected with spring-loaded rods. Output bell-crank connected with control rods of aerodynamic control surfaces is provided with quadrant with two bearing revolving rollers. Each roller is mounted for engagement with one of spring-loaded rods when respective pedal is depressed. Ends of rods directed to rollers are bevelled. Device is provided with mechanism for return of output bell-crank to neutral position when pedal is released. EFFECT: enhance reliability. 4 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT ENGINE CONTROL HANDLE | 1995 |
|
RU2089464C1 |
| AIRCRAFT ENGINE CONTROL UNIT | 2000 |
|
RU2188780C2 |
| AIRCRAFT FUEL SYSTEM | 1996 |
|
RU2134216C1 |
| TARGET SIMULATOR | 1997 |
|
RU2125275C1 |
| HELICOPTER CONTROL SYSTEM | 2023 |
|
RU2819837C1 |
| DEVICE WITH DIFFERENT-STROKE PEDALS FOR CONTROL OF AIRCRAFT RUDDERS | 2000 |
|
RU2178371C1 |
| AIRCRAFT NOSE UNDERCARRIAGE CONTROL SYSTEM | 1992 |
|
RU2070140C1 |
| CABLE CLAMP | 1994 |
|
RU2086830C1 |
| METHOD OF LOADING AIRCRAFT BRAKE CONTROL SYSTEM FOOT STATION PEDALS AND FOOT STATION PEDAL ASSEMBLY TO THIS END | 2012 |
|
RU2524808C1 |
| DEVICE FOR CHANGE OF GEAR RATIO IN FLYING VEHICLE CONTROL SYSTEM | 1991 |
|
RU2065825C1 |
