FIELD: machine building.
SUBSTANCE: air-jet engine includes a fuel supply pump, an igniter, a combustion chamber and a nozzle. Housing, flow accelerators and combustion chamber form air chambers which are connected to atmosphere.
EFFECT: invention is aimed at reduction of engine weight and reduction of fuel consumption.
1 cl, 1 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| TRANSPORT SYSTEM | 2018 | 
									
  | 
                RU2698650C1 | 
| WINDMILL-ELECTRIC GENERATOR | 2000 | 
									
  | 
                RU2197640C2 | 
| ELECTRICALLY HEATED BOILER | 1994 | 
									
  | 
                RU2079797C1 | 
| CURRENT GENERATOR | 1993 | 
									
  | 
                RU2069419C1 | 
| PUMP | 1994 | 
									
  | 
                RU2074984C1 | 
| WATER SYSTEM MAGNETIZER | 1997 | 
									
  | 
                RU2132822C1 | 
| COMPRESSED AIR OR GAS COOLING METHOD AND COMPRESSOR PLANT FOR IMPLEMENTING THIS METHOD | 1999 | 
									
  | 
                RU2172854C2 | 
| METHOD OF AND DEVICE FOR OPERATION OF RAMJET ENGINE | 2003 | 
									
  | 
                RU2264554C2 | 
| METHOD TO RECOVER SMALL-SIZE SOLID-PROPELLANT ROCKET ENGINES | 2010 | 
									
  | 
                RU2429415C1 | 
| HYBRID AIR-JET MAGNETOGASDYNAMIC ENGINE | 1998 | 
									
  | 
                RU2138668C1 | 
Authors
Dates
2020-01-28—Published
2018-10-15—Filed