18-06-2014 дата публикации
Номер: CN103863561A
Принадлежит:
The invention discloses a vertical take-off and landing unmanned aerial vehicle with foldable aerofoils, and relates to foldable unmanned aerial vehicles. The vertical take-off and landing unmanned aerial vehicle with foldable aerofoils is provided with a left aerofoil, a right aerofoil, a main aerofoil, a left aerofoil propeller engine, a right aerofoil propeller engine, a main propeller engine, a left camera, a right camera, a main camera, a left control plane, a right control plane and a main control plane; the left aerofoil and the right aerofoil are respectively connected with the main aerofoil; the left aerofoil propeller engine is arranged deadly above the inner side of the left aerofoil; the right aerofoil propeller engine is arranged deadly above the inner side of the right aerofoil; the main propeller engine is arranged deadly above the main aerofoil; the left camera is arranged on the outer side edge of the left aerofoil; the right camera is arranged on the right side edge of ...
Подробнее