FIELD: manufacturing technology.
SUBSTANCE: compressor (1) comprises flow part (13, 17, 19) and outer casing (3). Thermal shield (25) is made between the outer casing and the flow part of the compressor to reduce thermal stress and viscoplastic deformation of the casing under severe operating conditions. Outlet pipe is equipped with a heat-insulating device to reduce heat transfer from the gas flow to the inner surface of the outlet pipe.
EFFECT: compressor is disclosed.
19 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CERMET GAS LINE FOR HIGH-TEMPERATURE GAS TURBINE | 1999 |
|
RU2174617C2 |
| CENTRIFUGAL COMPRESSORS WITH INTEGRATED INTERCOOLING | 2015 |
|
RU2683063C2 |
| IMPROVED SCROLL FOR TURBOMACHINE, TURBOMACHINE COMPRISING SUCH SCROLL AND METHOD OF OPERATION | 2015 |
|
RU2699860C2 |
| FUEL NOZZLE, END FUEL NOZZLE UNIT, AND GAS TURBINE | 2013 |
|
RU2618801C2 |
| 0 |
|
SU1776885A1 | |
| GAS TURBINE PLANT | 2011 |
|
RU2493374C1 |
| GAS TURBINE ENGINE COMPRISING A CASING WITH COOLING RIBS | 2016 |
|
RU2724378C2 |
| MULTI-SECTION CENTRIFUGAL COMPRESSOR | 2014 |
|
RU2680180C1 |
| MOTOR-COMPRESSOR WITH STAGE IMPELLERS INTEGRATED IN MOTOR-ROTORS | 2014 |
|
RU2669122C1 |
| HIGH-EFFICIENCY THERMAL ENGINE | 2006 |
|
RU2380557C2 |
