FIELD: motors and pumps.
SUBSTANCE: extensible casing surrounds internal high pressure compressor housing and contains flange to be fixed to the upstream flange of combustion chamber housing. At least, one hollow is provided between flanges and around circle where gas flow bled from combustion chamber inlet circulates inside. Besides, natural circulation resulting from pressure drops is used. Owing to control device application in accordance with the invention, thermal flange expansion is passively adjusted and stresses resulting from different expansions of housing casing and attached flange are reduced.
EFFECT: reduction of stresses resulting from different expansions of housing casing and attached flange.
10 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
GAS TURBINE ENGINE HIGH-PRESSURE TURBINE VENTILATION | 2009 |
|
RU2504662C2 |
DESIGN OF LABYRINTH SEAL FOR GAS-TURBINE ENGINE | 2004 |
|
RU2357090C2 |
TURBO MACHINE WITH DIFFUSER | 2008 |
|
RU2470169C2 |
TIGHTNESS BETWEEN COMBUSTION CHAMBER AND NOZZLE GUIDE VANES OF TURBINE IN GAS-TURBINE ENGINE | 2009 |
|
RU2503821C2 |
TURBOJET ENGINE COMPRISING IMPROVED FACILITIES OF REGULATION OF FLOW RATE OF COOLING AIR FLOW TAKEN AT OUTLET OF HIGH PRESSURE COMPRESSOR | 2010 |
|
RU2532479C2 |
COMBUSTION CHAMBER FOR TURBOMACHINE | 2020 |
|
RU2773412C1 |
ANNULAR COMBUSTION CHAMBER IN TURBINE MACHINE | 2012 |
|
RU2608513C2 |
ANNULAR COMBUSTION CHAMBER OF TURBO-MACHINE | 2012 |
|
RU2606460C2 |
FIXED UNIT OF BLADES FOR GAS TURBINE ENGINE OF REDUCED WEIGHT AND GAS TURBINE ENGINE CONTAINING AT LEAST ONE SUCH FIXED UNIT OF BLADES | 2009 |
|
RU2511857C2 |
ASSEMBLY FOR GAS-TURBINE ENGINE | 2019 |
|
RU2787833C2 |
Authors
Dates
2009-01-10—Published
2004-07-09—Filed