FIELD: aircraft engines.
SUBSTANCE: invention relates to devices for unit connections of housings of aircraft gas-turbine engines. Proposed device for connecting mixer with housing of outer circuit of double-flow gas-turbine engine contains connecting members secured on mixer with alternating air and gas channels. Said members are made in form of ring secured on mixer by means of suspension members in form of inclined walls with shelves rigidly secured on ring and mixer. Ring is installed relative to outer circuit of engine with ring-radial expansion clearance. Ring suspension members on mixer can be connected in pairs to each other by shelves secured on ring to form U-shaped common member whose middle shelf is located opposite to air channel of mixer. Ring suspension members on mixer can be interconnected by shelves to form corrugated belt. Ring is provided with longitudinal splines. Housing of outer circuit of engine is provided with mating splines. Ring radial expansion clearance is made on pitch circle of splines.
EFFECT: improved reliability of device for connecting housing of gas-turbine engine, provision of function of support of gas generator with preservation of parameters of air flow at mixer outlet.
4 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR CONNECTING HOUSING OF GAS TURBINE ENGINE | 2001 |
|
RU2200849C2 |
AFTERBURNER OF BYPASS GAS TURBINE MIXED-FLOW ENGINET (VERSIONS) | 2008 |
|
RU2366823C1 |
ADAPTIVE AFTERCHARGE OF GAS TURBINE ENGINE | 2022 |
|
RU2786875C1 |
GAS-TURBINE ENGINE | 2013 |
|
RU2555933C2 |
DEVICE FOR MECHANICAL CONTROL OF RADIAL CLEARANCE BETWEEN ENDS OF ROTOR BLADES AND STATOR OF COMPRESSOR AND GAS TURBINE ENGINE TURBINE, METHOD OF CONTROLLING RADIAL CLEARANCE BETWEEN ENDS OF ROTOR BLADES AND STATOR OF COMPRESSOR AND GAS TURBINE ENGINE TURBINE | 2017 |
|
RU2702063C2 |
AFTERBURNER COMBUSTION CHAMBER OF A DUAL-CIRCUIT TURBOJET ENGINE AND METHOD FOR ITS OPERATION | 2021 |
|
RU2784569C1 |
METHOD OF GAS TURBINE ENGINE BATCH MANUFACTURING AND GAS TURBINE ENGINE MANUFACTURED ACCORDING TO THIS METHOD | 2013 |
|
RU2551142C1 |
METHOD OF BATCH PRODUCTION OF GAS-TURBINE ENGINE, AND GAS-TURBINE ENGINE MADE BY MEANS OF THIS METHOD | 2013 |
|
RU2544636C1 |
METHOD OF BATCH PRODUCTION OF GAS-TURBINE ENGINE, AND GAS-TURBINE ENGINE MADE BY MEANS OF THIS METHOD | 2013 |
|
RU2545111C1 |
BYPASS GAS TURBINE ENGINE | 2012 |
|
RU2499894C1 |
Authors
Dates
2005-10-27—Published
2004-01-28—Filed