FIELD: engines and pumps.
SUBSTANCE: method includes supplying a powder of metal fuel to the combustion chamber, igniting it and burning it in a stream of air from the air inlet. The powder in the form of a uniformly mixed suspension in a liquefied fuel gas placed in a fuel tank is preloaded with a displacement pressure, heated and supplied to the combustion chamber through a nozzle. The maximum diameter of the powder particles, the extrusion pressure and the heating temperature of the slurry are determined from the protected ratios.
EFFECT: increased power characteristics and reliability of the direct-flow air-jet engine.
2 cl, 2 tbl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR FEEDING A NANODISPERSED COMPONENT OF A FUEL COMPOSITION INTO THE COMBUSTION CHAMBER OF A RAMJET ENGINE | 2021 |
|
RU2767583C1 |
| HYBRID AEROSPACE ROCKET RAMJET | 2014 |
|
RU2563641C2 |
| NANO-COMPONENT ENERGY SUPPLEMENT AND LIQUID HYDROCARBON FUEL | 2013 |
|
RU2529035C1 |
| AIR RAMJET ENGINE OPERATING ON POWDER METAL FLUID | 2009 |
|
RU2439358C2 |
| NANOCOMPOSITE SOLID FUEL FOR RAMJET | 2016 |
|
RU2646933C1 |
| COMPOSITION OF PASTE-LIKE ROCKET FUEL FOR RAMJET ENGINES WITH AFTERBURNER CHAMBER | 2012 |
|
RU2485081C1 |
| SOLID FUELED INTEGRATED STRAIGHT-JET ENGINE | 2016 |
|
RU2623134C1 |
| VORTEX GAS COMPRESSOR DEVICE FOR COMBINED AIR-JET ENGINE | 2019 |
|
RU2766496C2 |
| FUEL FOR HYPERSONIC ATHODYD | 2013 |
|
RU2541526C1 |
| RAMJET ENGINE RUNNING ON SOLID PROPELLANT AND METHOD OF ITS OPERATION | 2014 |
|
RU2565131C1 |
