FIELD: aircraft engineering. SUBSTANCE: rims of pulley members have disks which transform into hubs, spring-lever frames coaxial to a bush and mounted on it in support bearings. The spring-lever frame is connected to the rim of the pulley members by kinematic links and has a spring mechanism stop member. The system provides particular cable tension and transfer of command forces from an engine control lever and a automatic thrust control device to the cable system. EFFECT: improved operating reliability and structure. 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ENGINE CONTROL UNIT | 1993 |
|
RU2091274C1 |
| DELTA-PLANER | 0 |
|
SU1752657A1 |
| HAND-OPERATED ONBOARD WINCH | 1991 |
|
RU2016836C1 |
| SEAPLANE BOARD FLOATER BEARING UNIT | 1992 |
|
RU2015069C1 |
| ENGINE CONTROL STICK | 1994 |
|
RU2100255C1 |
| PIPE CUTTER | 1990 |
|
RU2025226C1 |
| TWO-CHANNEL POWER SUPPLY SYSTEM | 0 |
|
SU1802898A3 |
| FIREPROOF HYDROPLANE | 1991 |
|
RU2028253C1 |
| CABLE TENSIONER FOR CONTROL SYSTEM | 2000 |
|
RU2180640C2 |
| HYDRAULIC SYSTEM FOR CONTROLLING HATCH DRIVES OF FIRE-FIGHTING VEHICLE TANK GROUP | 1991 |
|
RU2015065C1 |
