FIELD: mechanical engineering; gas-turbine engines. SUBSTANCE: device to deliver fuel into main combustion chamber of gas-turbine engine has small fuel nozzle and nozzle made in form of outer housing (sleeve) of small nozzle, and outer and inner air swirlers. Nozzle (sleeve), being of high flow- rate design, is held stationarily by spring, while blades of outer swirler are made turnable. EFFECT: enlarged range of steady burning, provision of stability of combustion process at increase of fuel consumption. 7 dwg
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BLADE TURN REGULATOR OF PRE-CHAMBER SWIRLER | 1996 |
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RU2175097C2 |
COMBUSTION CHAMBER OF ADAPTIVE GAS-TURBINE ENGINE | 1998 |
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COMBUSTION CHAMBER FRONT SYSTEM FOR HIGH- TEMPERATURE GAS-TURBINE ENGINE | 1996 |
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GAS-TURBINE ENGINE COMBUSTION CHAMBER | 1994 |
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OPTOELECTRONIC ANGLE GAGE | 1996 |
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MAIN COMBUSTION CHAMBER DIFFUSER FOR AIRCRAFT GAS- TURBINE ENGINE | 1996 |
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AIR INTAKE | 1992 |
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ANTI-G DEVICE FOR FLYING VEHICLE CREW MEMBER | 1992 |
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Authors
Dates
2001-07-27—Published
1998-09-08—Filed