FIELD: machine building.
SUBSTANCE: invention relates to control of gas turbine engine with application of thrust reversal during aircraft braking. Control method of reversible device of gas turbine engine includes locking of control signal for activation of reverse device at position of engine control lever outside zone of gas turbine engine small gas mode or in absence of information signal or signals describing aircraft landing. In case of fire in gas turbine engine, Fire in Engine Nacelle information signal is additionally automatically generated. In case of Fire in Engine nacelle information signal generation, control signal for reversible device activation is automatically blocked before flight completion.
EFFECT: higher safety of flight at braking of aircraft due to introduction of automatic locking of reversible device activation till flight completion in case of engine fire.
6 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CONTROL METHOD OF GAS TURBINE ENGINE REVERSING DEVICE DURING AIRCRAFT LANDING AND INTERRUPTED TAKEOFF | 2019 |
|
RU2730731C1 |
| CONTROL METHOD OF AIRCRAFT ENGINE REVERSING DEVICE AT AIRCRAFT BRAKING | 2019 |
|
RU2719778C1 |
| METHOD FOR SWITCHING ON THE REVERSING DEVICE OF A GAS TURBINE ENGINE WHEN LANDING AN AIRCRAFT | 2021 |
|
RU2774011C1 |
| METHOD FOR CONTROLLING A GAS TURBINE ENGINE IN CASE OF SPONTANEOUS OPENING OF A REVERSING DEVICE | 2021 |
|
RU2774010C1 |
| METHOD AND DEVICE FOR CONTROLLING AIRCRAFT GAS TURBINE ENGINE THRUST REVERSAL | 2024 |
|
RU2828300C1 |
| METHOD FOR CONTROLLING THE REVERSER APPARATUS OF A GAS TURBINE ENGINE | 2021 |
|
RU2783048C1 |
| METHOD OF AVIATION GAS TURBINE ENGINE CONTROL AT TAKEOFF IN CASE OF FIRE | 2015 |
|
RU2618171C1 |
| ELECTROMECHANICAL SYSTEM FOR CONTROLLING THE REVERSER APPARATUS OF A GAS TURBINE ENGINE | 2020 |
|
RU2757949C1 |
| METHOD OF CONTROL OVER GAS TURBINE ENGINE | 2011 |
|
RU2488706C2 |
| METHOD OF CONTROLLING THERMAL STATE OF ELECTRONIC CONTROLLER OF GAS TURBINE ENGINE | 2023 |
|
RU2817575C1 |
