FIELD: machine building.
SUBSTANCE: invention relates to compressor building, in particular, to design of impellers. The impeller of the centrifugal compressor comprises the main disc with blades; a cover disc fixed on end surfaces of the blades, the inner surface of which is made as conical with a rectilinear generatrix, and a blade-to-blade channel formed by inner surfaces of the main and cover discs. The inner conical surface of the cover disc is made as conical with an angle near the top, which is equal to 180°-α, the inner surface of the main disc is also made as conical with an angle near the top equal to 180°-α, which provides for meridian symmetry of the gas flow and increased external diameter of the impeller from D2 to D3, which provides for development of a mobile vaneless diffuser on the impeller.
EFFECT: invention is aimed at increasing energy characteristics of an impeller: flow rate, head, efficiency, reduced pulsations and turbulence at the output of the impeller.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
CENTRIFUGAL COMPRESSOR STAGE | 2009 |
|
RU2414629C2 |
CENTRIFUGAL COMPRESSOR STAGE | 2007 |
|
RU2334901C1 |
IMPELLER OF CENTRIFUGAL COMPRESSOR | 2010 |
|
RU2450165C1 |
CENTRIFUGAL SUPERCHARGER IMPELLER | 1999 |
|
RU2182265C2 |
DEVICE FORMING PASSAGE AREA OF INTERVANE CHANNEL OF CENTRIFUGAL COMPRESSOR RADIAL DIFFUSER | 2005 |
|
RU2294462C1 |
STAGE OF CENTRIFUGAL TURBOMACHINE | 2001 |
|
RU2243417C2 |
CENTRIFUGAL COMPRESSOR | 2004 |
|
RU2273771C1 |
WORKING WHEEL OF CENTRIFUGAL COMPRESSOR | 0 |
|
SU1772428A1 |
CENTRIFUGAL SUPERCHARGER IMPELLER | 2000 |
|
RU2174196C1 |
MULTISTAGE CENTRIFUGAL COMPRESSOR | 0 |
|
SU1523737A1 |
Authors
Dates
2014-04-10—Published
2012-08-29—Filed