Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Unmanned aerial vehicle hatch cover opening and closing structure
The invention relates to an unmanned aerial vehicle hatch cover opening and closing structure. The unmanned aerial vehicle hatch cover opening and closing structure comprises a hatch cover and a fuselage provided with a cabin. The hatch cover shields the cabin and further comprises an opening and closing assembly; the opening and closing assembly comprises an opening and closing base, an opening and closing elastic piece and a connecting piece hinged to the opening and closing base; the connecting piece is provided with a stress body, and the opening and closing elastic piece is arranged on the fuselage and abuts against the stress body; the connecting piece is connected with the hatch cover; and seen from the axis line where the opening and closing base is hinged to the connecting piece, the stress body in the cover closing state and the stress body in the cover opening state are located on the two sides of the axis line where the opening and closing base is hinged to the connecting piece correspondingly. The hatch cover is convenient to open and close; meanwhile, the opening state and the closing state of the hatch cover can be ensured; in the opening and closing process of the hatch cover, the elastic force borne by the stress body is uniform, and it can be ensured that the opening and closing process of the hatch cover is smoothly conducted; and the opening and closing assembly is a whole and can be pre-assembled into a whole and then installed on an unmanned aerial vehicle, and assembly of the unmanned aerial vehicle is facilitated.
本发明涉及无人机舱盖开合结构，其包括舱盖及、设置有机舱的机身；舱盖遮挡机舱，还包括开合组件；开合组件包括开合基座、开合弹性片及、与开合基座铰接的连接件；连接件设置有受力体，开合弹性片设置在机身上且与受力体相抵；连接件与舱盖连接；沿开合基座与连接件铰接的轴心线看，合盖状态时的受力体、开盖状态时的受力体分别位于开合基座与连接件铰接的轴心线的两侧。本发明便于打开、关闭舱盖，同时，能够分别确保舱盖开盖状态、合盖状态；能够确保舱盖开合的过程，受力体受到的弹力比较均，能够确保舱盖开合的过程顺利地进行；开合组件为一个整体，能够预组装为一体再安装到无人机上，便于无人机的组装。
Unmanned aerial vehicle hatch cover opening and closing structure
The invention relates to an unmanned aerial vehicle hatch cover opening and closing structure. The unmanned aerial vehicle hatch cover opening and closing structure comprises a hatch cover and a fuselage provided with a cabin. The hatch cover shields the cabin and further comprises an opening and closing assembly; the opening and closing assembly comprises an opening and closing base, an opening and closing elastic piece and a connecting piece hinged to the opening and closing base; the connecting piece is provided with a stress body, and the opening and closing elastic piece is arranged on the fuselage and abuts against the stress body; the connecting piece is connected with the hatch cover; and seen from the axis line where the opening and closing base is hinged to the connecting piece, the stress body in the cover closing state and the stress body in the cover opening state are located on the two sides of the axis line where the opening and closing base is hinged to the connecting piece correspondingly. The hatch cover is convenient to open and close; meanwhile, the opening state and the closing state of the hatch cover can be ensured; in the opening and closing process of the hatch cover, the elastic force borne by the stress body is uniform, and it can be ensured that the opening and closing process of the hatch cover is smoothly conducted; and the opening and closing assembly is a whole and can be pre-assembled into a whole and then installed on an unmanned aerial vehicle, and assembly of the unmanned aerial vehicle is facilitated.
本发明涉及无人机舱盖开合结构，其包括舱盖及、设置有机舱的机身；舱盖遮挡机舱，还包括开合组件；开合组件包括开合基座、开合弹性片及、与开合基座铰接的连接件；连接件设置有受力体，开合弹性片设置在机身上且与受力体相抵；连接件与舱盖连接；沿开合基座与连接件铰接的轴心线看，合盖状态时的受力体、开盖状态时的受力体分别位于开合基座与连接件铰接的轴心线的两侧。本发明便于打开、关闭舱盖，同时，能够分别确保舱盖开盖状态、合盖状态；能够确保舱盖开合的过程，受力体受到的弹力比较均，能够确保舱盖开合的过程顺利地进行；开合组件为一个整体，能够预组装为一体再安装到无人机上，便于无人机的组装。
Unmanned aerial vehicle hatch cover opening and closing structure
无人机舱盖开合结构
WANG HUA (Autor:in) / LI XIANGCHENG (Autor:in) / LIU WEI (Autor:in)
11.06.2021
Patent
Elektronische Ressource
Chinesisch
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