FIELD: aeronautics; aviation; cosmonautics.
SUBSTANCE: invention relates to a method for synchronising aircraft engines. Activation logic for each engine is used to synchronise engines. Activation logic sets up three states, specifically, off, standby and on. Switching between different states is carried out in a certain manner depending on security conditions. When one engine is switched off, all other engines automatically do the same.
EFFECT: higher safety when synchronising engines.
6 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF AIRCRAFT ENGINES SYNCHRONIZATION | 2012 |
|
RU2605140C2 |
| METHOD FOR PROTECTING A GAS TURBINE ENGINE WITH A THREE-STAGE GAS GENERATOR AGAINST THE PUMP WITH THE FOLLOWING DESTROY OF THE GAS AIR TRACT | 2020 |
|
RU2747113C1 |
| GAS TURBINE CONTROL METHOD AND SYSTEM, AND GAS TUBRINE CONTAINING SUCH SYSTEM | 2010 |
|
RU2509905C2 |
| LP SPOOL POWER TAKE-OFF AND DEBRIS REMOVAL SYSTEM | 2020 |
|
RU2795890C2 |
| O V TCHEREMUSHKIN'S AIRCRAFT | 2008 |
|
RU2396185C1 |
| METHOD TO PROTECT GAS-TURBINE ENGINE FROM UNSTABLE OPERATION OF COMPRESSOR | 2006 |
|
RU2310100C2 |
| CONTROL OVER TURBOMACHINE | 2011 |
|
RU2562131C2 |
| HYDRAULIC TRANSMISSION OF TRANSPORT MACHINE | 2012 |
|
RU2545245C2 |
| METHOD OF AIRCRAFT ENGINE MONITORING DURING OPERATION IN FLIGHT | 2016 |
|
RU2708905C2 |
| METHOD FOR EMERGENCY POWER SUPPLY OF AUXILIARY POWER PLANT OF AIRCRAFT LIFE SUPPORT SYSTEMS | 1992 |
|
RU2005898C1 |
