FIELD: jet engine plants of flying vehicles. SUBSTANCE: plant comprises envelope 2 whose from immovable portion is arranged about screw 1 provided with rotating blades 3 for reversing direction of air flow. Rear tail section forming nozzle 4 may be movably located in cavity 8 of envelope 2. EFFECT: enhanced efficiency. 7 cl, 11 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBOJET ENGINE | 1992 |
|
RU2101535C1 |
| AIR INTAKE FOR TURBO-JET AIRCRAFT ENGINE | 1991 |
|
RU2039880C1 |
| BRUSH SEAL | 1997 |
|
RU2158864C2 |
| GAS OUTLET PIPELINE | 1994 |
|
RU2104398C1 |
| INTERNAL-COMBUSTION ENGINE EXHAUST PIPE | 0 |
|
SU1766274A3 |
| SUCKING PLANT FOR INTERNAL COMBUSTION ENGINE | 1991 |
|
RU2065526C1 |
| PISTON INTERNAL COMBUSTION ENGINE WITH SUPERCHARGING | 1990 |
|
RU2011863C1 |
| MULTICYLINDER DIESEL LOW COMPRESSION RATIO ENGINE | 0 |
|
SU1806281A3 |
| INTERNAL-COMBUSTION ENGINE OIL CHANNEL | 0 |
|
SU1766273A3 |
| HIGH-PRESSURE PUMP CONTROL DEVICE | 0 |
|
SU1709922A3 |
