FIELD: power engineering. SUBSTANCE: fuel gas goes from gasifier to turbine inlet and air is extracted from compressor and delivered over air ducts through vanes, while cooling them, to turbine flow path. Since fuel gas admitted to turbine contains combustible components and its temperature is higher than ignition point of the latter, mixing such gas with delivered air causes burning of combustible components and increase in gas temperature. Almost isothermal gas expansion within turbine can be attained by appropriate distribution of air supply. EFFECT: improved conditions fir fuel combustion. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GAS-TURBINE PLANT | 1992 |
|
RU2061888C1 |
| GAS TURBINE ENGINE OPERATING METHOD AND GAS TURBINE ENGINE | 2019 |
|
RU2726861C1 |
| AIR ACCUMULATING PLANT | 1992 |
|
RU2053398C1 |
| GAS-TURBINE PLANT | 1994 |
|
RU2078228C1 |
| METHOD OF CONVERTING HEAT INTO MECHANICAL WORK IN GAS- TURBINE ENGINE AND GAS-TURBINE ENGINE | 1993 |
|
RU2044906C1 |
| METHOD OF CONVERTING HEAT ENERGY TO MECHANICAL WORK IN GAS-TURBINE ENGINE AND GAS-TURBINE ENGINE | 1992 |
|
RU2031230C1 |
| GAS TURBINE PLANT (GTP) WITH FLUID INJECTION TO GTP CIRCUIT | 2011 |
|
RU2517995C2 |
| METHOD OF OPERATION OF JET ENGINE | 1995 |
|
RU2087735C1 |
| METHOD OF AND DEVICE FOR INCREASING TEMPERATURE DIFFERENCE IN HEAT ENGINE | 1998 |
|
RU2151310C1 |
| BURNER WITH GAS AND AIR PRE-MIXING FOR GAS TURBINES AND CONVECTORS (EMBODIMENTS) | 2018 |
|
RU2716775C2 |
