FIELD: process engineering.
SUBSTANCE: gas turbine (33) is proposed, comprising at least a compressor (43), a power turbine (47), a load junction (35) connecting said gas turbine (33) to the load (37), a load junction enclosure (65) at least partially surrounding said junction (35), and a channels system for the cooling air (51, 61, 63) configured and arranged to ensure the circulation of the cooling air flow in the load junction enclosure, sufficient for heat removal from the load junction (35).
EFFECT: invention allows to reduce the thermal and mechanical stress in the gas turbine.
16 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GAS TURBINE WITH BILATERAL DRIVE | 2013 |
|
RU2642714C2 |
| GAS TURBINE, CONTAINING PRIMARY AND SECONDARY COOLERS OF LUBE OIL | 2013 |
|
RU2625391C1 |
| GAS TURBINE SEALING-UP SYSTEM | 2001 |
|
RU2270352C2 |
| METHODS AND SYSTEMS FOR PREVENTING LUBRICATING OIL LEAKAGE IN GAS TURBINES | 2014 |
|
RU2661123C2 |
| GAS-TURBINE MARINE INSTALLATIONS | 2014 |
|
RU2697690C1 |
| GAS TURBINE ENGINE COMPRISING A CASING WITH COOLING RIBS | 2016 |
|
RU2724378C2 |
| DEVICE AND METHOD OF GAS TURBINE UNBLOCKING AFTER ITS STOP | 2013 |
|
RU2622356C2 |
| GAS TURBINE IN MECHANICAL DRIVE APPLICATIONS AND OPERATING METHODS THEREOF | 2013 |
|
RU2659603C2 |
| COMBUSTION CHAMBER OF GAS TURBINE AND GAS TURBINE | 2019 |
|
RU2727946C1 |
| AVIATION-TYPE GAS TURBINE WITH IMPROVED HEAT REGULATION | 2019 |
|
RU2777405C2 |
