FIELD: aeronautical engineering; manual control of flying vehicle power plants. SUBSTANCE: unit includes engine control levers and stops of intermediate modes with shift mechanisms. Engine control levers are provided with at least two program threshold members. EFFECT: enhanced reliability. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CABLE ENGINE CONTROL SYSTEM | 1991 |
|
RU2015076C1 |
| ENGINE CONTROL STICK | 1994 |
|
RU2100255C1 |
| HAND-OPERATED ONBOARD WINCH | 1991 |
|
RU2016836C1 |
| FIREPROOF HYDROPLANE | 1991 |
|
RU2028253C1 |
| SEAPLANE BOARD FLOATER BEARING UNIT | 1992 |
|
RU2015069C1 |
| TOILET ARRANGEMENT | 1994 |
|
RU2100254C1 |
| TWO-CHANNEL POWER SUPPLY SYSTEM | 0 |
|
SU1802898A3 |
| SEAPLANE | 1993 |
|
RU2104224C1 |
| SEAPLANE SPRAY DEFLECTOR | 1992 |
|
RU2015068C1 |
| SEAPLANE FUEL TANK VENTING SYSTEM | 1992 |
|
RU2054361C1 |
