FIELD: compressors.
SUBSTANCE: example of a centrifugal compressor comprises a housing forming an inlet chamber and comprising first and second holes defining a recirculation channel which is hydraulically connected to the inlet chamber. Impeller is located inside the housing and can rotate about the longitudinal axis for suction of liquid into the inlet chamber. First and second holes are located in different axial positions along longitudinal axis. Plurality of inlet guide vanes are rotatable and located in inlet chamber. Centrifugal compressor comprises a ring and a controller designed to move the ring along the longitudinal axis between the first position and the second position at rotation of the inlet guide vanes. Ring closes at least one of the first and second holes, and is stronger in the second position than in the first position.
EFFECT: disclosed is centrifugal compressor with recirculation channel.
23 cl, 17 dwg
Title | Year | Author | Number |
---|---|---|---|
GAS COMPRESSOR GUIDE VANES SYSTEM TO BE FITTED IN THROAT | 2010 |
|
RU2508476C2 |
HIGHLY EFFICIENT CENTRIFUGAL IMPELLER | 2019 |
|
RU2719415C1 |
REDUCED LOAD FROM AXIAL FORCE IN TURBOCOMPRESSOR | 2016 |
|
RU2718397C2 |
CENTRIFUGAL COMPRESSOR WITH FLOW STABILIZING CASE | 1994 |
|
RU2117825C1 |
TURBOFAN ENGINE WITH COMPACT SYSTEM OF AIR TAKEOFF FROM BOOSTER COMPRESSOR | 2006 |
|
RU2433312C2 |
MOTOR-COMPRESSOR WITH STAGE IMPELLERS INTEGRATED IN MOTOR-ROTORS | 2014 |
|
RU2669122C1 |
GAS TURBINE ENGINE, FOR EXAMPLE AIRCRAFT TURBOJET ENGINE | 2005 |
|
RU2373402C2 |
INLET GUIDE VANE DEVICE | 2015 |
|
RU2699863C2 |
SYSTEMS AND METHODS FOR CONTROLLING FLOW OF EXHAUST GAS IN GAS TURBINE SYSTEMS WITH RECIRCULATION OF EXHAUST GAS | 2014 |
|
RU2645392C2 |
TURBOCOMPRESSOR RECIRCULATING DEVICE | 2003 |
|
RU2296247C2 |
Authors
Dates
2020-03-17—Published
2019-01-18—Filed