FIELD: aviation.
SUBSTANCE: proposed wing tip includes wing tip proper with vortex generator mounted on it for forming flow of opposite direction relative to tip vortex; vortex generator is provided with bacelle and nozzle. Wing tip is provided with cylindrical casing forming longitudinal cut with upper and lower edges on outer surface. In front portion, inner surface of casing is engageable with outer surface of nozzle and in tail portion it is engageable with open end face of nozzle.
EFFECT: enhanced lifting and aerodynamic properties.
4 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT WING TIP AND ITS VORTEX GENERATOR | 2008 |
|
RU2389649C1 |
| AIRCRAFT WING TIP | 2008 |
|
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RU2667410C1 |
| VORTEX FLOW GENERATOR | 2010 |
|
RU2453736C1 |
| MULTI-MEMBER TIP | 1997 |
|
RU2118270C1 |
| GROOVE-TYPE GENERATOR OF VORTEX FLOW | 2011 |
|
RU2453737C1 |
