Tilting adherent aircraft and auxiliary structure
Tilting adherent aircraft and auxiliary structure
- Neue Suche nach: LIU XINGCHAO
- Neue Suche nach: YANG DAWEI
- Neue Suche nach: WANG TAO
- Neue Suche nach: XIE ZHENG
- Neue Suche nach: PAN DAN
- Neue Suche nach: LIU XINGCHAO
- Neue Suche nach: YANG DAWEI
- Neue Suche nach: WANG TAO
- Neue Suche nach: XIE ZHENG
- Neue Suche nach: PAN DAN
The invention relates to the technical field of aircrafts, in particular to a tiltable adherent aircraft and an auxiliary structure. Comprising a machine body, a plurality of airflow channels are formed in the machine body, blades and power parts connected with the blades are arranged on the airflow channels, and the power parts are used for driving the blades to rotate forwards and backwards so as to change the flow direction of airflow above and below the machine body passing through the airflow channels; a plurality of upper supporting foot stools are arranged on the upper surface of the machine body, and trundles are arranged on the upper supporting foot stools; a mounting seat is further arranged on one side of the upper surface of the fuselage, and an auxiliary structure is arranged on the mounting seat and serves as a force-exerting rotating part for rotation of the aircraft. An auxiliary structure and an upper supporting foot stool are arranged. And rotation and state switching are realized by means of an auxiliary structure and motor differential speed. In the wall attaching state, the aircraft has a stable force exerting position, is slightly influenced by wind power and is not prone to destructive collision with the wall surface. And stable and long-time fixed-point monitoring and other tasks can be realized.
本发明涉及飞行器技术领域，具体是涉及一种可倾转贴壁飞行器及辅助结构。包括机身，所述机身上开设有多个气流通道，所述气流通道上设桨叶和与所述桨叶连接的动力部件，所述动力部件用于驱动所述桨叶正反转以改变机身上下方气流通过所述气流通道的流向；所述机身上表面设置有多个上支撑脚架，所述上支撑架上设置有脚轮；所述机身的上表面一侧还设置有安装座，所述安装座上设置有辅助结构，以作为飞行器旋转的着力旋转部位。通过设有辅助结构和上支撑脚架。借助辅助结构和电机差速实现旋转和状态切换。在贴壁状态下，飞行器有稳定的着力处，受风力影响小，也不易与壁面再发生破坏性碰撞。可以实现稳定、长时间的定点监视等任务。
Dokumentinformationen
Tilting adherent aircraft and auxiliary structure
一种可倾转贴壁飞行器及辅助结构
2024-02-20
Patent
Elektronische Ressource
Chinesisch