FIELD: power engineering; pumps, fans, gas compressors and turbines. SUBSTANCE: method involves displacement of working medium through entire length of interblade channel to ensure continuous flow of working medium on condition that absolute acceleration and its relative speed vectors are collinear. EFFECT: facilitated procedure. 4 dwg
Title | Year | Author | Number |
---|---|---|---|
MARINE PROPELLER | 1995 |
|
RU2106283C1 |
INTERNAL COMBUSTION ENGINE | 2016 |
|
RU2667828C2 |
HEAT CAVITATION GENERATOR | 2010 |
|
RU2422733C1 |
RADIAL IMPELLER GRATE OF CENTRIFUGAL WHEEL | 2017 |
|
RU2646984C1 |
VANED DIFFUSER OF CENTRIFUGAL COMPRESSOR | 2008 |
|
RU2353818C1 |
HIGHER-EFFICIENCY TURBINE BLADING (VERSIONS) | 2011 |
|
RU2457336C1 |
TOROIDAL TURBINE | 1997 |
|
RU2126485C1 |
BLADE DIFFUSER OF CENTRIFUGAL MACHINE | 2009 |
|
RU2406880C2 |
CENTRIFUGAL COMPRESSOR STAGE | 2007 |
|
RU2334901C1 |
RADIAL WHEEL ROTOR | 2010 |
|
RU2429385C1 |
Authors
Dates
1997-12-27—Published
1995-03-22—Filed