FIELD: cooling systems. SUBSTANCE: perforated member is made in the form of a plate, a rib and pins which edges are engageable with the plate. The cooling circuit height reduces down the cooling medium flow. EFFECT: improved structure. 3 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD AND DEVICE FOR TURBINE BLADE COOLING | 1993 |
|
RU2098638C1 |
METHOD FOR COOLING OF NOZZLE ASSEMBLY OF A LOW-PRESSURE TURBINE (LPT) OF A GAS TURBINE ENGINE AND A LPT NOZZLE ASSEMBLY WHICH IS COOLED BY THIS METHOD, A METHOD FOR COOLING A BLADE OF LPT NOZZLE ASSEMBLY AND A NOZZLE ASSEMBLY BLADE, COOLED BY THIS METHOD | 2018 |
|
RU2691202C1 |
METHOD OF REPLACING ASSEMBLY OF WORKING VANES OF TURBINE STAGE OF GAS-TURBINE ENGINE | 1995 |
|
RU2099541C1 |
AIR COOLING PATH OF BLADE OF NOZZLE APPARATUS OF HIGH PRESSURE TURBINE OF A GAS TURBINE ENGINE (VERSIONS) | 2018 |
|
RU2686430C1 |
GAS TURBINE COOLED WORKING BLADE | 2012 |
|
RU2506429C1 |
GAS TURBINE COOLED NOZZLE GUIDE VANE | 2003 |
|
RU2237811C1 |
NOZZLE ASSEMBLY OF LOW-PRESSURE TURBINE (LPT) OF GAS TURBINE ENGINE (GTE) (VERSIONS) AND BLADE OF LPT NOZZLE ASSEMBLY (VERSIONS) | 2018 |
|
RU2691203C1 |
GAS-TURBINE COOLED BLADE | 0 |
|
SU1815334A1 |
HIGH-PRESSURE TURBINE ROTOR OF A GAS TURBINE ENGINE (VERSIONS) | 2018 |
|
RU2691868C1 |
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 |
Authors
Dates
1994-03-15—Published
1990-09-27—Filed