A dual-axis ball head for use in an unmanned aerial vehicle, a triple-axis ball head for use in the unmanned aerial vehicle, and a multi-rotor aerial vehicle, comprising a machine frame component, a transmission component, and a photographing component. The machine frame component comprises a first frame bracket (2), a second frame bracket (2), and a third frame bracket (6). The transmission component comprises a first motor (3) and a second motor (5), and also comprises a connecting rod (12). Two free ends of the connecting rod (12) respectively are rotatably arranged on two open ends of the second frame bracket (4). The connecting rod (12) is fixed onto the third frame bracket (6) via a fastener (13). By hingedly arranging the free ends of the connecting rod (12) onto the second frame bracket (4), both together constitute a parallel quadrilateral connecting rod, when the second frame bracket (4) rotate for a certain number of degrees in relation to the third frame bracket (6), the connecting rod (12) moves in tandem for same number of degrees, a rotation track of the second frame bracket (4) is thus not affected. The connecting rod (12) is fixed via the fastener (13) onto the third frame bracket (6), and the connecting rod (12) provides same with effective support in the vertical direction, thus improving the load capacity and stiffness of the second frame bracket (4), and effectively reducing the degree of distention thereof.
Dual-axis platform for use in an unmanned aerial vehicle, Tri-axis platform for use in an unmanned aerial vehicle, and multi-rotor aerial vehicle
15.12.2016
Patent
Elektronische Ressource
Englisch
IPC: | F16M Rahmen, Gehäuse oder Grundplatten von Kraftmaschinen oder anderen Maschinen oder von Apparaten, nicht auf eine besondere Art von Maschine oder Apparat eingeschränkt, die anderweitig vorgesehen ist , FRAMES, CASINGS, OR BEDS, OF ENGINES OR OTHER MACHINES OR APPARATUS, NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUS PROVIDED FOR ELSEWHERE / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Europäisches Patentamt | 2017
Europäisches Patentamt | 2016
|Europäisches Patentamt | 2024
|