FIELD: heat power engineering. SUBSTANCE: ring converging-diverging passageway connects the flowing part of the turbine with the take-off chamber. The average ellipticity of the diverging part is equal to or greater than 1.15 but no less than 1.25, the divergence angle being equal to 2-7°. The ratio of the minimum to maximum cross-section is equal to 0.03-0.35. The outlet diameter of the diffuser has an eccentricity with respect to the inlet diameter. The ratio of the eccentricities is 0.04-0.075. The minimum inlet diameter of the diffuser is located from the side of the take-off branch pipes. EFFECT: improved design. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
STEAM TURBINE EXTRACTION CHAMBER | 0 |
|
SU1082974A1 |
STEAM TURBINE BLEED-OFF BELT | 0 |
|
SU1325171A1 |
EXHAUST SECTION OF STEAM TURBINE | 1989 |
|
RU2053373C1 |
METHOD OF COOLING THE ROTOR OF A HIGH PRESSURE TURBINE (HPT) OF GAS TURBINE ENGINE (GTE), HPT ROTOR AND HPT ROTOR BLADE COOLED BY THIS METHOD, KNOT OF THE DEVICE OF TWISTING OF AIR OF HPT ROTOR | 2018 |
|
RU2684298C1 |
STAGE OF CENTRIFUGAL TURBOMACHINE | 2001 |
|
RU2243417C2 |
HIGH-PRESSURE TURBINE ROTOR OF A GAS TURBINE ENGINE (VERSIONS) | 2018 |
|
RU2691868C1 |
METHOD TO COOL BY-PASS GAS TURBINE ENGINE VANES AND DEVICE TO THIS END | 2008 |
|
RU2387846C1 |
DEVICE FOR COOLING OF STEAM TURBINE FLOW PASSAGE MEMBERS | 1992 |
|
RU2037051C1 |
EXHAUST BRANCH PIPE OF STEAM TURBINE | 1992 |
|
RU2040697C1 |
TURBOMACHINE | 1992 |
|
RU2042835C1 |
Authors
Dates
1995-10-27—Published
1991-04-03—Filed