A vertical take-off and landing unmanned plane includes a fuselage, wings, a first motor, a first propeller, a second motor and a second propeller, the first motor comprises a first motor bearing, the angle between the first motor bearing axis and the fuselage symmetry plane is less than 90-degree, the first motor is connected with the head of the fuselage, the first motor can rotate around a rotation shaft perpendicular to the fuselage symmetry plane; the first propeller is connected with the first motor bearing; the second motor includes a second motor bearing, the second motor bearing axis is located in the fuselage symmetry plane, and the second motor is connected with the tail of the fuselage, the second propeller is connected with the second motor bearing, and is located on the upper side of the fuselage. The first motor of the vertical take-off and landing unmanned plane can rotate around the rotation shaft perpendicular to the fuselage symmetry plane, the vertical take-off and landing unmanned plane zero horizontal velocity take-off and landing and hovering can be achieved, and the vertical take-off and landing unmanned plane can horizontally fly at high speed.
Vertical take-off and landing unmanned plane
2016-02-24
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2015
|VERTICAL TAKE-OFF AND LANDING UNMANNED AERIAL VEHICLE
Europäisches Patentamt | 2019
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