FIELD: centrifugal compressors with air flow rate control systems; gas-turbine engines for transport facilities and gas-turbine power plants.
SUBSTANCE: proposed method is used for centrifugal compressor having impeller, radial open diffuser and radial vaned diffuser. Proposed method includes change of flow area at impeller outlet before inlet of radial vaned impeller. Besides that, flow area behind radial vaned diffuser is changed additionally; control of flow section before radial vaned diffuser and behind radial vaned diffuser is effected in turn.
EFFECT: extended field of steady operation of compressor.
3 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
CENTRIFUGAL COMPRESSOR | 2006 |
|
RU2327060C1 |
DEVICE FORMING PASSAGE AREA OF INTERVANE CHANNEL OF CENTRIFUGAL COMPRESSOR RADIAL DIFFUSER | 2005 |
|
RU2294462C1 |
CENTRIFUGAL COMPRESSOR | 2004 |
|
RU2273771C1 |
CENTRIFUGAL COMPRESSOR STAGE | 2007 |
|
RU2334901C1 |
VANED DIFFUSER OF CENTRIFUGAL COMPRESSOR | 2008 |
|
RU2353818C1 |
CENTRIFUGAL COMPRESSOR REGULATING METHOD | 0 |
|
SU667691A1 |
VANED DIFFUSER FOR CENTRIFUGAL COMPRESSOR | 2001 |
|
RU2194195C1 |
RADIAL-FLOW COMPRESSOR STAGE | 2011 |
|
RU2452876C1 |
METHOD OF SEALING AIR CHANNELS | 2014 |
|
RU2582725C2 |
COMPRESSOR | 2004 |
|
RU2253758C1 |
Authors
Dates
2005-02-10—Published
2003-06-18—Filed