FIELD: transport.
SUBSTANCE: invention relates to gas turbine power plant control systems. Proposed system comprises thrust control computing module 1, electronic controller 2, and fuel control pump 4, cable mechanism. It incorporates also engine control lever (ECL) 5, thrust automatic device actuator 6, αecl position pickup 8, aircraft flight stage data transmission unit 10 connected with thrust control computing module 1. Electronic controller 2 represents electronic digital computer with the primary and secondary channels arranged on aircraft engine that comprises switch 12, unit 11 to reveal failure of αecl position pickup 8 and generates control signal for fuel control pump with due allowance for aircraft flight stage data. The latter represent signals "Take-off", "Climb" and "Cruising regime".
EFFECT: higher reliability, improved performances.
3 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF AUTOMATIC CONTROL OF GAS TURBINE ENGINE THRUST | 2009 |
|
RU2406849C1 |
| AIRCRAFT ENGINE CONTROL SYSTEM | 1990 |
|
RU1707896C |
| METHOD FOR CONTROLLING A GAS TURBINE ENGINE IN CASE OF SPONTANEOUS OPENING OF A REVERSING DEVICE | 2021 |
|
RU2774010C1 |
| METHOD OF AVIATION GAS TURBINE ENGINE CONTROL AT TAKEOFF IN CASE OF FIRE | 2015 |
|
RU2618171C1 |
| MONITORING METHOD OF GAS TURBINE ENGINE CONTROL SYSTEM | 2010 |
|
RU2468229C2 |
| CONTROL METHOD OF GAS TURBINE ENGINE REVERSIBLE DEVICE | 2019 |
|
RU2726491C1 |
| METHOD OF CONTROLLING THERMAL STATE OF ELECTRONIC CONTROLLER OF GAS TURBINE ENGINE | 2023 |
|
RU2817575C1 |
| METHOD FOR SWITCHING ON THE REVERSING DEVICE OF A GAS TURBINE ENGINE WHEN LANDING AN AIRCRAFT | 2021 |
|
RU2774011C1 |
| CONTROL METHOD OF GAS TURBINE ENGINE REVERSING DEVICE DURING AIRCRAFT LANDING AND INTERRUPTED TAKEOFF | 2019 |
|
RU2730731C1 |
| DEVICE FOR GAS TURBINE ENGINE CONTROL | 2012 |
|
RU2497000C1 |
