FIELD: aircraft engineering.
SUBSTANCE: aircraft ejector speed-up device comprises, at least, two hermetically coupled nozzles and, least, one vacuumized chamber. Note that the proposed speed-up device incorporates a plate linked to the rotary shaft and communicates with a sealed package of the first and second nozzles fitted on said plate to revolve it.
EFFECT: higher-efficiency ejector.
5 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SHESTERENKO'S AIRCRAFT (SAC) | 2006 |
|
RU2384471C2 |
| SHESTERENKO'S HEAD PIECE (VERSIONS) | 2006 |
|
RU2356637C2 |
| NOZZLE DEVICE | 2004 |
|
RU2303491C2 |
| HEAT EXCHANGER HEATING METHOD OF THE HOUSES HEATING SYSTEM AND OTHER OBJECTS AND DEVICE FOR THE METHOD IMPLEMENTATION | 2012 |
|
RU2618183C2 |
| SHESTERENKO SUPERNOZZLE (VERSIONS) | 2004 |
|
RU2361679C2 |
| PROBE | 2001 |
|
RU2206410C2 |
| NOZZLE ASSEMBLY | 2003 |
|
RU2267360C2 |
| THERMAL HEAD | 2006 |
|
RU2313403C2 |
| FLYING VEHICLE | 2003 |
|
RU2277059C2 |
| METHOD AND THE DEVICE FOR DISPERSION OF THE GAS-LIQUID MIXTURE | 2003 |
|
RU2279907C2 |
