FIELD: manufacturing technology.
SUBSTANCE: in order to reduce erosion of impeller (120, 130) due to liquid droplets in an incoming flow of gas, impeller (120, 130) comprises converging-diverging bottlenecks, wherein the incoming flow passes through the bottlenecks so that the speed of the gas at inlet (122) of the impeller first suddenly and substantially increases and then suddenly and substantially decreases, wherein the impeller is configured so that, internally after its inlet, the incoming flow is deviated gradually in the meridional plane.
EFFECT: fluid tolerant impeller for centrifugal compressors is disclosed.
14 cl, 10 dwg
Title | Year | Author | Number |
---|---|---|---|
WET GAS COMPRESSOR AND METHOD | 2013 |
|
RU2614309C2 |
CENTRIFUGAL COMPRESSOR IMPELLER WITH NON-LINEAR BLADE LEADING EDGE AND ASSOCIATED DESIGN METHOD | 2015 |
|
RU2682211C2 |
METHOD OF TURBO MACHINE COMPONENT PROTECTION AGAINST EROSION UNDER ACTION OF LIQUID DROPS, COMPONENT AND TURBOMACHINE | 2015 |
|
RU2695245C2 |
COMPRESSOR UNIT (VERSIONS) AND METHOD OF IMPARTING PARAMETERS TO GAS FLOW | 2012 |
|
RU2584395C2 |
DROP CATCHER FOR CENTRIFUGAL COMPRESSOR | 2009 |
|
RU2522015C2 |
WET GAS COMPRESSION SYSTEM WITH THERMOACOUSTIC RESONATOR | 2012 |
|
RU2607576C2 |
DEVICE AND METHOD OF CONDITIONING FLOW OF FATTY GAS | 2015 |
|
RU2703858C2 |
IMPELLER WITH HIGH RIGIDITY FOR TURBOMACHINE, TURBOMACHINE COMPRISING SAID IMPELLER, AND METHOD OF MANUFACTURING | 2016 |
|
RU2702579C1 |
IMPELLER WITH PROTECTION ELEMENTS AND CENTRIFUGAL COMPRESSOR | 2014 |
|
RU2682212C1 |
CENTRIFUGAL COMPRESSOR IMPELLER WITH BLADES HAVING S-SHAPED TRAILING EDGE | 2014 |
|
RU2669425C2 |
Authors
Dates
2019-02-14—Published
2014-09-11—Filed