FIELD: mechanical engineering; gas-turbine engines.
SUBSTANCE: proposed gas-turbine engine with electric starter contains axial-flow compressor, electric stater with rotor, installed on rotor shaft of axial-flow compressor and stator arranged in housing of axial-flow compressor. Electric starter is made in form of thyristor reactive motor with rotor in form of laminated pack with salient poles enclosed by coils of connected winding of stator, with rotor position pickup, power electronic unit and control unit.
EFFECT: improved reliability and economy of gas-turbine engine.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GAS TURBINE ENGINE CONTROL SYSTEM | 2000 |
|
RU2184258C2 |
| ELECTRIC MOTOR | 2019 |
|
RU2727956C1 |
| CONTROL VALVE | 2021 |
|
RU2781138C1 |
| SYSTEM TO DELIVER STARTING GAS INTO TURBO-EXPANDER OF GAS-TURBINE ENGINE | 2004 |
|
RU2270927C2 |
| GAS-TURBINE ENGINE CONTROL AND PROTECTIVE SYSTEM | 2002 |
|
RU2209989C1 |
| LOCKING AND REGULATING VALVE | 1999 |
|
RU2172885C2 |
| SEAL CONTROL SYSTEM OF GAS TURBOSUPERCHARGER PLANT | 2001 |
|
RU2191929C1 |
| COMPRESSOR SURGE PROTECTION METHOD | 2004 |
|
RU2266431C1 |
| GAS TURBINE ENGINE START-UP METHOD | 2018 |
|
RU2680287C1 |
| NON-CONTACT ELECTRIC REDUCTION MACHINE WITH SALIENT-POLE ARMATURE | 2010 |
|
RU2416859C1 |
