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Unmanned aerial vehicle clamping mechanism and unmanned aerial vehicle nest
The invention provides an unmanned aerial vehicle clamping mechanism and an unmanned aerial vehicle nest. The unmanned aerial vehicle clamping mechanism comprises a take-off and landing plate, two clamping assemblies and a frame. The frame is used for mounting the take-off and landing plate and the clamping assembly; each clamping assembly comprises two parallel clamping rods, the clamping rods are arranged on the two sides of the upper portion of the lifting plate, and the clamping rods of one clamping assembly are arranged above the clamping rods of the other clamping assembly. At least one clamping assembly comprises a synchronous belt and a motor used for driving the synchronous belt, the synchronous belt comprises an upper synchronous belt and a lower synchronous belt, and the upper synchronous belt and the lower synchronous belt are fixedly connected with the clamping rods of one clamping assembly respectively. The unmanned aerial vehicle clamping mechanism is simple in structure and low in cost.
本发明提供了一种无人机夹持机构及无人机机巢,该无人机夹持机构包括起降板、两组夹持组件和框架。所述框架用于安装所述起降板和所述夹持组件;所述夹持组件包括两个平行设置的夹持杆,所述夹持杆设于所述起降板的上方的两侧,其中一组所述夹持组件的所述夹持杆设于另一组夹持组件的所述夹持杆的上方;至少有一组所述夹持组件包括同步带和用于驱动所述同步带的电机,所述同步带包括上同步带和下同步带,所述上同步带和下同步带分别固定连接一组所述夹持组件的所述夹持杆。该无人机夹持机构结构简单且成本较低。
Unmanned aerial vehicle clamping mechanism and unmanned aerial vehicle nest
The invention provides an unmanned aerial vehicle clamping mechanism and an unmanned aerial vehicle nest. The unmanned aerial vehicle clamping mechanism comprises a take-off and landing plate, two clamping assemblies and a frame. The frame is used for mounting the take-off and landing plate and the clamping assembly; each clamping assembly comprises two parallel clamping rods, the clamping rods are arranged on the two sides of the upper portion of the lifting plate, and the clamping rods of one clamping assembly are arranged above the clamping rods of the other clamping assembly. At least one clamping assembly comprises a synchronous belt and a motor used for driving the synchronous belt, the synchronous belt comprises an upper synchronous belt and a lower synchronous belt, and the upper synchronous belt and the lower synchronous belt are fixedly connected with the clamping rods of one clamping assembly respectively. The unmanned aerial vehicle clamping mechanism is simple in structure and low in cost.
本发明提供了一种无人机夹持机构及无人机机巢,该无人机夹持机构包括起降板、两组夹持组件和框架。所述框架用于安装所述起降板和所述夹持组件;所述夹持组件包括两个平行设置的夹持杆,所述夹持杆设于所述起降板的上方的两侧,其中一组所述夹持组件的所述夹持杆设于另一组夹持组件的所述夹持杆的上方;至少有一组所述夹持组件包括同步带和用于驱动所述同步带的电机,所述同步带包括上同步带和下同步带,所述上同步带和下同步带分别固定连接一组所述夹持组件的所述夹持杆。该无人机夹持机构结构简单且成本较低。
Unmanned aerial vehicle clamping mechanism and unmanned aerial vehicle nest
无人机夹持机构及无人机机巢
CHEN YANZHOU (Autor:in) / WANG GANJUN (Autor:in) / SU HAOHUI (Autor:in) / CHEN BOFAN (Autor:in)
29.07.2022
Patent
Elektronische Ressource
Chinesisch
IPC:
B64F
GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT
,
Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen
/
B60L
PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES
,
Antrieb von elektrisch angetriebenen Fahrzeugen
/
E04H
Gebäude oder ähnliche Bauwerke für besondere Zwecke
,
BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES
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