FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed drone has fuselage, wing, V-like tail unit and engine with tractor propeller. Fuselage 1 consists of nose part 9 and conical tail part 10 attached to central part 8. Wing 2 comprises centre section 5 connected with outer wings 6 with ailerons 7. Tail unit 3 incorporates cradle 12 connecting cantilever 11 and connected with tail part 10. Centre section 5 has buildup 13 and payload fasteners. Outer wings 6 are arranged at transverse angle and feature geometrical warp with reduction of pitch angle at end cross-sections. Ailerons 7 are connected with top surface of outer wing 6 by flexible skin 16.
EFFECT: higher aerodynamics.
7 cl, 12 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HIGH-SPEED UNMANNED AERIAL VEHICLE | 2021 |
|
RU2787906C1 |
| UNMANNED FLYING VEHICLE (VARIANTS) | 2002 |
|
RU2213024C1 |
| RAM WING SEA PLANE | 2012 |
|
RU2532658C2 |
| HIGH-CAPACITY AIRCRAFT | 2007 |
|
RU2335430C1 |
| BEAM OF AIRCRAFT-TYPE UNMANNED AERIAL VEHICLE WITH VERTICAL TAKE-OFF AND LANDING (VTOL) | 2024 |
|
RU2830728C1 |
| AIRCRAFT WITH FOLDING WING AND DEVICE FOR AIRCRAFT WING FOLDING | 2009 |
|
RU2403177C1 |
| UNMANNED AERIAL VEHICLE AND METHOD OF ITS ASSEMBLY | 2024 |
|
RU2830724C1 |
| "TAILLESS" FLARECRAFT | 2022 |
|
RU2776632C1 |
| UAV FROM STANDARDIZED PARTS AND ASSEMBLIES AND PRODUCTION METHOD | 2023 |
|
RU2812011C1 |
| WING OF AIRCRAFT-TYPE UNMANNED AERIAL VEHICLE WITH VERTICAL TAKEOFF AND LANDING (VTOL) | 2024 |
|
RU2830730C1 |
