FIELD: gas turbine engine engineering. SUBSTANCE: device has spring-loaded two- belt slide valve 3. Spring-loaded two-belt slide valve 39 has groove 40 connected with controlled space 41 of servo piston 14 and slide valve 32. Spring space 42 of the slide valve is connected with cutting off slide valve 17 and space 43 is connected with electromagnetic valve 15. EFFECT: improved design. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR CONTROL OF GAS-TURBINE ENGINE | 1991 |
|
RU2032823C1 |
CONTROL SYSTEM COMMAND DEVICE FOR GAS-TURBINE ENGINE | 1991 |
|
RU2006632C1 |
GAS-TURBINE ENGINE REACTION NOZZLE FLAP CONTROL SYSTEM | 2002 |
|
RU2289713C2 |
DEVICE FOR AUTOMATIC CONTROL OF GAS-TURBINE ENGINE | 1990 |
|
RU2028482C1 |
GAS TURBINE ENGINE FUEL RATE CONTROL SYSTEM | 2001 |
|
RU2198312C2 |
0 |
|
SU244813A1 | |
DEVICE FOR AUTOMATIC SUPPLY OF FUEL INTO COMBUSTION CHAMBER OF GAS-TURBINE ENGINE | 1992 |
|
RU2029122C1 |
METHOD AND SYSTEM FOR SUPPLYING FUEL TO COMBUSTION CHAMBER OF GAS-TURBINE ENGINE | 1992 |
|
RU2034166C1 |
TURBOJET ENGINE FUEL SUPPLY SYSTEM | 1989 |
|
SU1792127A1 |
FUEL CONTROL SYSTEM IN GAS-TURBINE ENGINE | 2006 |
|
RU2324065C2 |
Authors
Dates
1995-03-10—Published
1991-06-27—Filed