FIELD: compressor engineering. SUBSTANCE: surface of chute 4 and back 5 of blades 3 in the region of inlet edge 6 have straight generatrix. Generatrix surfaces of chute 4 and back 5 are smoothly transformed into surfaces of at least second order in the region of outlet edge 7. Convexities of the generatrices face each other. EFFECT: improved design. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
DIFFUSER OF CENTRIFUGAL OR DIAGONAL-FLOW COMPRESSOR | 2002 |
|
RU2234623C2 |
DIFFUSER OF CENTRIFUGAL OR DIAGONAL-FLOW COMPRESSOR | 2002 |
|
RU2234622C2 |
RADIAL BLADE DIFFUSER OF CENTRIFUGAL COMPRESSOR | 2016 |
|
RU2631846C1 |
VANED DIFFUSER OF CENTRIFUGAL COMPRESSOR | 2008 |
|
RU2353818C1 |
VANED DIFFUSER FOR CENTRIFUGAL COMPRESSOR | 2001 |
|
RU2194195C1 |
CENTRIFUGAL COMPRESSOR | 2004 |
|
RU2273771C1 |
GAS TURBINE ENGINE LOW PRESSURE COMPRESSOR ROTOR IMPELLER (VERSIONS) | 2015 |
|
RU2603380C1 |
TURBOJET ENGINE LOW-PRESSURE COMPRESSOR SECOND STAGE ROTOR IMPELLER (VERSIONS) | 2015 |
|
RU2603383C1 |
TURBOJET LOW-PRESSURE COMPRESSOR ROTOR FOURTH-STAGE IMPELLER | 2015 |
|
RU2612282C1 |
GAS TURBINE ENGINE LOW-PRESSURE COMPRESSOR ROTOR IMPELLER (VERSIONS) | 2015 |
|
RU2611497C1 |
Authors
Dates
1995-02-27—Published
1991-03-05—Filed