FIELD: aviation.
SUBSTANCE: invention relates to the aviation industry, and can be used in development of unmanned aerial vehicles for various purposes. Unmanned aerial vehicle comprises fuselage provided with instrument compartment with constant payload, antenna system and power supply unit and wings connected therewith. Wings are made replaceable. In the fuselage there are at least four seats for installation and fixation of replaceable wings, the number and location of which is determined depending on the selected aerodynamic scheme.
EFFECT: higher functionality of unmanned aerial vehicle and wider field of its application with simultaneous simplification of design.
6 cl, 17 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| CONVERTIPLANE | 2019 |
|
RU2723516C1 |
| DRONE AIRCRAFT (VERSIONS) | 2015 |
|
RU2613629C2 |
| CONVERTIPLANE | 2017 |
|
RU2657706C1 |
| VERTICAL OR SHORT TAKEOFF AND LANDING UNIVERSAL UNMANNED AIRCRAFT | 2015 |
|
RU2604755C1 |
| UNMANNED AERIAL VEHICLE | 2023 |
|
RU2812164C1 |
| SMALL UNMANNED AERIAL VEHICLE | 2023 |
|
RU2812634C1 |
| FLIGHT VEHICLE (VERSIONS), FLIGHT VEHICLES PARTS, METHOD OF EXPLOITING FLIGHT VEHICLE AND ITS PARTS | 2010 |
|
RU2466061C2 |
| TRANSPORT CARGO UNMANNED AIRCRAFT | 2021 |
|
RU2776617C1 |
| UNMANNED AERIAL VEHICLE | 2021 |
|
RU2754277C1 |
