FIELD: engines and pumps.
SUBSTANCE: proposed compressor comprises first case (28a) that makes the holder of injector, second case (28b) arranged there around to make a circular chamber (40) and multiple air injectors (38, 38') fitted in their appropriate seats. Every said injector comprises at least one air feed channel (48) extending on one side to gas-air circuit (26) and, on opposite side, to said circular chamber between said cases. Injector inlet has collar (52) with inner side (52a) resting radially on inlet collar (44) of the first case appropriate seat and outer side (52b) radially resting on inner side of second case. Clamps of air injector inlet collar between said cases retain air injectors in the first case seats. All air injectors are retained in their seats by simple mechanical means.
EFFECT: ease of replacements, hence, of servicing.
7 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR TURBOPROP FAN BLADE ORIENTATION CONTROL | 2010 |
|
RU2525101C2 |
AIR INJECTION INTO GAS TURBINE ENGINE COMPRESSOR PATH | 2009 |
|
RU2482339C2 |
SYSTEM TO COOL REAR CAVITY OF CENTRIFUGAL COMPRESSOR IMPELLER | 2007 |
|
RU2433309C2 |
GAS TURBINE ENGINE COMPRESSOR COMPRISING BLADES WITH VARIABLE INSTALLATION ANGLE | 2015 |
|
RU2687474C2 |
GAS TURBINE PLANT AND ITS DISMANTLING METHOD | 2015 |
|
RU2689258C2 |
CONTROL SYSTEM OF BLADES WITH VARIABLE ANGLE OF INSTALLATION FOR GAS TURBINE ENGINE | 2016 |
|
RU2700113C2 |
TURBINE CRANKCASE, CONTAINING RING SECTIONS FASTENERS | 2012 |
|
RU2615867C2 |
DOUBLE-CIRCUIT GAS TURBINE ENGINE | 2019 |
|
RU2799997C2 |
GAS TURBINE ENGINE ROTOR, TURBOJET AND PLUG FOR GAS TURBINE ENGINE ROTOR | 2009 |
|
RU2496988C2 |
CONTROL RING OF STAGE OF BLADES WITH VARIABLE ANGLE OF INSTALLATION FOR GAS TURBINE ENGINE | 2015 |
|
RU2705128C2 |
Authors
Dates
2015-09-10—Published
2010-08-20—Filed