FIELD: aircraft engineering.
SUBSTANCE: method and device for increase in aircraft lift, aircraft engine being provided with the nozzle located nearby the wing trailing edge. Aircraft lift is increased by exploiting the nozzle lower outer surface with at least one aerodynamic shutter arranged thereat to deflect the airflow all around the aircraft.
EFFECT: reduced drag caused by turbulence.
5 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL | 2018 |
|
RU2711760C2 |
| AIRCRAFT-MONOPLANE WITH ADDITIONAL WING | 2003 |
|
RU2249542C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT - DISK-TYPE FLYING VEHICLE | 1999 |
|
RU2174484C2 |
| METHOD OF CONTROL OF FLYING VEHICLE AND DEVICE FOR REALIZATION OF THIS METHOD (VERSIONS) | 2005 |
|
RU2299834C2 |
| SHORT TAKEOFF AND LANDING UNMANNED AERIAL VEHICLE | 2015 |
|
RU2606216C1 |
| ALL-TERRAIN AIR-CUSHION LIGHT AIRPLANE | 2000 |
|
RU2226470C2 |
| SEAPLANE | 2001 |
|
RU2223200C2 |
| METHOD OF CREATING AIRCRAFT LIFT (VERSIONS), METHOD OF FLIGHT, NON-AERODYNAMIC ALL-WEATHER VTOL AIRCRAFT "MAXINIO" (VERSIONS), METHODS OF TAKE-OFF AND LANDING, AICRAFT CONTROL METHOD AND SYSTEM, FUSELAGE, WING (VERSIONS), THRUST REVERSE AND METHOD OF ITS OPERATION, LANDING GEAR SYSTEM, GAS SEPARATION AND DISTRIBUTION SYSTEM | 2007 |
|
RU2349505C1 |
| GROUND-EFFECT VEHICLE | 2019 |
|
RU2716303C1 |
