FIELD: aviation.
SUBSTANCE: aviation-type gas turbine is described, containing a case, a compressor with a rotor mounted on a generator shaft supported for the rotation in the case, a high pressure turbine located in the case with a rotor mounted on the generator shaft for the joint rotation with the compressor rotor, a combustion chamber, a power turbine located in the case and containing a rotor mounted on a turbine shaft for the actuation of a load, while there is heat-insulating coating for reduction in heat dissipation through the case.
EFFECT: creation of a turbine with improved heat regulation reducing the risk of blocking a rotor, including in an operating state, is achieved.
12 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE AND METHOD OF GAS TURBINE UNBLOCKING AFTER ITS STOP | 2013 |
|
RU2622356C2 |
| SYSTEMS TO COOL COMPONENT OF STEAM PIPE | 2008 |
|
RU2498090C2 |
| POWER-GENERATING SYSTEM WITH RING COMBUSTION CHAMBER | 1997 |
|
RU2243383C2 |
| VENTILATION SYSTEM FOR BEARING OIL CAVITY | 2019 |
|
RU2753385C1 |
| HEAT SHIELD FOR GAS TURBINE ENGINE | 2020 |
|
RU2790234C1 |
| METHOD AND DEVICE FOR COOLING GAS | 2005 |
|
RU2304260C2 |
| TURBINE ASSEMBLY IN TURBINE ENGINE | 2014 |
|
RU2638114C2 |
| THERMAL CONTROL SYSTEM FOR ROTOR BEARING SUPPORTING ELEMENT, STEAM TURBINE AND POWER PLANT | 2012 |
|
RU2602320C2 |
| NOZZLE WITH BLADE PROFILE TUBE FOR GAS TURBINE | 2017 |
|
RU2729589C1 |
| GAS TURBINE DEVICE | 2016 |
|
RU2678861C1 |
