FIELD: aviation.
SUBSTANCE: method of changing characteristics of an aerodynamic control element of an unmanned aerial vehicle consists in the fact that the lower nose part of the surface of the aerodynamic control element is shaded from the incoming air flow by deflecting the flap located in front of the aerodynamic control element on the lower surface of the wing, in the direction from the lower surface of the wing.
EFFECT: invention can be used to reduce the value of the hinge moment of the aerodynamic control element on the wing of an unmanned aerial vehicle.
1 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AERODYNAMIC CONTROL OF AIRCRAFT | 2022 |
|
RU2792369C1 |
| CONTROL SURFACE | 2018 |
|
RU2702480C2 |
| WING WITH AERODYNAMIC CURTAIN | 2016 |
|
RU2646686C2 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| UNMANNED FLYING VEHICLE | 2005 |
|
RU2288140C1 |
| UNMANNED AERIAL VEHICLE | 2023 |
|
RU2812164C1 |
| 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 |
| AERODYNAMIC HANDLEBAR | 2022 |
|
RU2789424C1 |
| SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL | 2018 |
|
RU2711760C2 |
| DRONE | 2011 |
|
RU2493050C2 |
