FIELD: engines and pumps.
SUBSTANCE: gas turbine engine combustion chamber comprises outer casing and detachable case. The latter is made up of at least three parts with longitudinal joints. Said joints are arranged uniformly along the circumference. At least one of two annular flanges of the case features tapered mating surface.
EFFECT: reduction in case strain irregularity, higher tightness of flange joints.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| REMOTE COMBUSTION CHAMBER | 2015 |
|
RU2626180C2 |
| SMALL-SIZE GAS TURBINE PLANT | 2024 |
|
RU2819326C1 |
| ANNULAR COMBUSTION CHAMBER OF GAS-TURBINE ENGINE | 0 |
|
SU1726917A1 |
| NOZZLE ASSEMBLY OF LOW-PRESSURE TURBINE (LPT) OF GAS TURBINE ENGINE (GTE) (VERSIONS) AND BLADE OF LPT NOZZLE ASSEMBLY (VERSIONS) | 2018 |
|
RU2691203C1 |
| TUBULAR-ANNULAR COMBUSTION CHAMBER OF GAS TURBINE ENGINE | 1998 |
|
RU2151961C1 |
| ADJUSTABLE ANNULAR COMBUSTION CHAMBER | 2020 |
|
RU2749472C1 |
| GAS-TURBINE ENGINE ANNULAR COMBUSTION CHAMBER | 2002 |
|
RU2212591C1 |
| DEVICE FOR ATTACHMENT OF FLAME TUBE IN BODY OF COMBUSTION CHAMBER | 2001 |
|
RU2223448C2 |
| SEAL OF INNER JOINT BETWEEN GAS TURBINE DISTRIBUTOR AND COMBUSTION CHAMBER | 2012 |
|
RU2496017C1 |
| COMBUSTION CHAMBER WITH CIRCULAR ULTRASONIC SELF-EXCITED OSCILLATOR FOR FUEL ATOMIZING | 2000 |
|
RU2170884C1 |
