FIELD: power engineering industry. SUBSTANCE: turbomachine has diaphragm with guide blades 2 and diaphragm labyrinth seal 3, drum-type rotor 4 with working blades 5 and tail intermediate parts 6 provided with through bypass passages 7 whose total passage area is equal to 0.005 to 0.075 of area of passages of working blades 5; cross-section of bypass passages 7 corresponds to shape of cross section of passages of working blades 5. EFFECT: enhanced reliability. 7 dwg
Title | Year | Author | Number |
---|---|---|---|
STAGE OF AXIAL-FLOW TURBINE | 1991 |
|
RU2024770C1 |
STAGE OF AXIAL-FLOW TURBINE | 1991 |
|
RU2024769C1 |
TURBOMACHINE END SEAL | 1994 |
|
RU2086777C1 |
STEAM TURBINE | 1987 |
|
RU1554479C |
SEAL | 1991 |
|
RU2050493C1 |
STEAM TURBINE LOW-PRESSURE CYLINDER END SEAL | 1996 |
|
RU2107824C1 |
HIGH-TEMPERATURE MULTISTAGE STEAM TURBINE | 2005 |
|
RU2279551C1 |
VERTICAL ROTARY PUMP | 1991 |
|
RU2011012C1 |
END-SEAL ASSEMBLY FOR STEAM-TURBINE CYLINDER | 1999 |
|
RU2174606C2 |
END FACE SEAL OF HYDRAULIC MACHINE VANES | 0 |
|
SU618569A2 |
Authors
Dates
1995-08-27—Published
1992-12-02—Filed