FIELD: power mechanical engineering. SUBSTANCE: air flow is preliminary separated into coaxial ring jets and adjacent air jets are swirled toward each other. The nearest parts of the jets are then directed radially toward each other. The fuel jets enter a space between these parts of swirled air jets. In so doing the fuel jets are in high turbulent shear layer of air and intensive mixing of fuel with air occurs. EFFECT: enhanced efficiency. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
PRECHAMBER OF COMBUSTION CHAMBER | 1993 |
|
RU2083927C1 |
METHOD OF BURNING FUEL | 1991 |
|
RU2027048C1 |
FUEL COMBUSTION METHOD | 2011 |
|
RU2511980C2 |
FORECHAMBER OF COMBUSTION CHAMBER | 1994 |
|
RU2086857C1 |
COMBUSTION CHAMBER | 1993 |
|
RU2087805C1 |
COMBUSTION CHAMBER PREMIXING CAVITY | 1993 |
|
RU2083926C1 |
COMBUSTION CHAMBER | 1994 |
|
RU2086856C1 |
COMBUSTION CHAMBER | 1992 |
|
RU2027112C1 |
FRONTAL ARRANGEMENT OF COMBUSTION CHAMBER | 1990 |
|
RU2013708C1 |
COMBUSTIBLE CHAMBER | 1991 |
|
RU2027111C1 |
Authors
Dates
1995-01-20—Published
1991-09-02—Filed