FIELD: power engineering.
SUBSTANCE: coaxial jet nozzle comprises hollow tip that connects the space of one of the fuel components with the combustion zone and bushing that embraces the tip to define a ring space and connects the space of the other fuel component with the combustion zone. The exit section of the tip is provided with the radial grooves so that the periphery of the central jet bounded by the generatrices of the beams is no more than 3s, and the beam length is 2.3-2.5s, where s is the beam thickness.
EFFECT: enhanced completeness of combustion.
1 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COAXIAL SPRAY ATOMISER | 2012 |
|
RU2505698C1 |
| LIQUID PROPELLANT ROCKET ENGINE | 2012 |
|
RU2493406C1 |
| COAXIAL SPRAY ATOMISER | 2012 |
|
RU2497009C1 |
| LIQUID-PROPELLANT ENGINE | 2012 |
|
RU2490507C1 |
| LIQUID PROPELLANT ROCKET ENGINE | 2012 |
|
RU2493412C1 |
| MIXING HEAD OF LIQUID PROPELLANT ROCKET ENGINE CHAMBER | 2012 |
|
RU2493408C1 |
| COAXIAL SPRAY INJECTOR | 2012 |
|
RU2490504C1 |
| MIXING HEAD OF LIQUID ROCKET ENGINE CHAMBER | 2012 |
|
RU2498102C1 |
| METHOD OF FUEL COMPONENTS FEED IN THREE-COMPONENT LIQUID PROPELLANT ROCKET ENGINE COMBUSTION CHAMBER AND ALIGNED-JET NOZZLE TO THIS END | 2012 |
|
RU2502887C1 |
| LIQUID-PROPELLANT ENGINE CHAMBER MIXING HEAD | 2012 |
|
RU2490502C1 |
