FIELD: power mechanical engineering. SUBSTANCE: at burning fuel in a combustion chamber air flow is preliminary separated into ring coaxial jets. Adjacent jets is swirled in opposite directions, and nearest parts of the swirled air jets and fuel jets is fed to semi-bounded space for forming over- rich fuel-air mixture, creating circulating burning zones, and partially burning out of fuel at air-fuel ratio of 0.6-0.8. The remainder parts of the swirled air jets enter confined space for forming poor fuel-air mixture and creating circulating burning zones. EFFECT: enhanced efficiency. 5 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF BURNING FUEL | 1991 |
|
RU2027047C1 |
FORECHAMBER OF COMBUSTION CHAMBER | 1994 |
|
RU2086857C1 |
PRECHAMBER OF COMBUSTION CHAMBER | 1993 |
|
RU2083927C1 |
COMBUSTION CHAMBER | 1994 |
|
RU2086856C1 |
METHOD OF BURNING FUEL | 1998 |
|
RU2128807C1 |
METHOD OF BURNING FUEL | 2001 |
|
RU2213296C2 |
COMBUSTION CHAMBER PREMIXING CAVITY | 1993 |
|
RU2083926C1 |
GAS-TURBINE COMBUSTION CHAMBER | 1996 |
|
RU2107229C1 |
GAS TURBINE CANNULAR-TYPE COMBUSTION CHAMBER | 1997 |
|
RU2141077C1 |
COMBUSTION CHAMBER | 1993 |
|
RU2087805C1 |
Authors
Dates
1995-01-20—Published
1991-09-02—Filed