FIELD: propulsion machinery. SUBSTANCE: metal profile shell that is not force-cooled is mounted freely without fixing and is put on hollow fin-rod which houses baffle plate. Shell is flown about by working medium. Clearance housing at least one screen having protrusions on its both surfaces is formed between shell and rod. Protective and thermal barrier coats may be deposited on surfaces of shell, screen and rod. EFFECT: diminished consumption of cooling air without disturbance of aerodynamics of blade grid. 1 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
ENVELOPED BLADE FOR TURBO-MACHINE | 1997 |
|
RU2131977C1 |
TURBOMACHINE ROTATING BLADE | 1995 |
|
RU2118462C1 |
ENVELOPE TURBINE BLADE FEATHER | 1998 |
|
RU2154169C2 |
GAS TURBINE COOLED CERAMET BLADES | 1999 |
|
RU2204020C2 |
COMPLEX BLADE OF AXIAL TURBO-MACHINE | 2009 |
|
RU2416029C2 |
WORKING BLADE OF THE GAS TURBINE | 2017 |
|
RU2656052C1 |
COMPOSITE WORKING BLADE OF TURBOMACHINE | 2023 |
|
RU2822437C1 |
GAS TURBINE CERMET BLADE | 2012 |
|
RU2510463C2 |
GAS TURBINE CERMET COOLED NOZZLE VANE | 1995 |
|
RU2097574C1 |
QUASIADIABATIC CERAMIC NOZZLE ASSEMBLY OF HIGH- TEMPERATURE GAS TURBINE (VERSIONS) | 1999 |
|
RU2204021C2 |
Authors
Dates
1998-10-27—Published
1995-10-26—Filed