FIELD: gas-turbine engineering. SUBSTANCE: flue tube has front ring, external and internal casings with film cooling facilities made on their surfaces with annular crosswise slits inbetween whose axes are located in same plane perpendicular to flue tube axis. Distance from internal surface of front ring to plane of axes of annular slits is 0.28 to 0.4 of flue tube length. EFFECT: reduced emission of pollutants, improved reliability in engine operation. 3 dwg
Title | Year | Author | Number |
---|---|---|---|
RING COMBUSTION CHAMBER OF GAS TURBINE ENGINE | 1989 |
|
SU1837699A1 |
RING COMBUSTION CHAMBER FOR GAS-TURBINE ENGINE | 1985 |
|
RU1325962C |
RADIAL-FACE CONTACT SEAL | 1990 |
|
RU2037704C1 |
BEARING SUPPORT | 1989 |
|
RU1646354C |
DEVICE FOR DRAINING FUEL FROM COMBUSTION CHAMBER OF GAS TURBINE ENGINE | 1983 |
|
RU1254798C |
FLAME TUBE FOR RING COMBUSTION CHAMBER OF GAS-TURBINE ENGINE HAVING CENTRIFUGAL COMPRESSOR | 1988 |
|
RU2033545C1 |
TUBULAR-ANNULAR COMBUSTION CHAMBER OF GAS-TURBINE POWER PLANT | 1995 |
|
RU2107227C1 |
GAS TURBINE CANNULAR-TYPE COMBUSTION CHAMBER | 1997 |
|
RU2138739C1 |
0 |
|
SU1777628A3 | |
MODULAR MOBILE GAS-TURBINE POWER-AND-HEAT GENERATION PLANT AND SHELL BOILER FOR PLANT | 2000 |
|
RU2171903C1 |
Authors
Dates
1995-03-27—Published
1990-07-30—Filed