FIELD: engines and pumps.
SUBSTANCE: liquid-propellant engine chamber includes mixing head containing the housing, oxidiser supply unit, fuel supply unit and flame bottom. Coaxial spray injectors include hollow tip attaching the oxidiser cavity to combustion zone, sleeve enclosing the tip with a gap and attaching the fuel cavities to combustion zone. In outlet part of the tip there located are pylons interacting with inner sleeve surface and aligning the tip relative to the sleeve, and located in mixing head along concentric circles and forming central and peripheral zones. Chamber also includes regeneratively cooled combustion chamber with critical section and a nozzle. In pylons of injector tips there made are channels one end of which opens to the tip cavity and the other one - to the combustion chamber cavity; discharge nozzle is installed in the outlet part of hollow tip with the possibility of being replaced.
EFFECT: improving combustion efficiency of fuel components.
2 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
LIQUID-PROPELLANT ROCKET ENGINE MIXING HEAD | 2011 |
|
RU2451200C1 |
LIQUID-PROPELLANT ENGINE | 2011 |
|
RU2445498C1 |
LIQUID-PROPELLANT ENGINE | 2011 |
|
RU2445500C1 |
LIQUID-PROPELLANT ENGINE MIXING HEAD | 2012 |
|
RU2496022C1 |
METHOD OF FEEDING THREE-COMPONENT FUEL INTO LIQUID-PROPELLANT ROCKET ENGINE CHAMBER | 2012 |
|
RU2495272C1 |
METHOD OF FUEL COMPONENTS FEED IN THREE-COMPONENT LIQUID PROPELLANT ROCKET ENGINE COMBUSTION CHAMBER | 2012 |
|
RU2502886C1 |
METHOD OF FEEDING THREE-COMPONENT FUEL INTO LIQUID-PROPELLANT ROCKET ENGINE CHAMBER | 2012 |
|
RU2495271C1 |
METHOD TO SUPPLY FUEL COMPONENTS IN CHAMBER OF THREE-COMPONENT LIQUID PROPELLANT ROCKET ENGINE AND COAXIAL JET NOZZLE FOR IMPLEMENTATION OF SPECIFIED METHOD | 2012 |
|
RU2501967C1 |
MIXING HEAD OF LIQUID PROPELLANT ROCKET ENGINE CHAMBER | 2012 |
|
RU2493408C1 |
MIXING HEAD OF LIQUID PROPELLANT ROCKET ENGINE CHAMBER | 2012 |
|
RU2493407C1 |
Authors
Dates
2012-03-20—Published
2011-03-24—Filed