Aircraft and aircraft control method thereof
Aircraft and aircraft control method thereof
- Neue Suche nach: GUO HONGTAO
- Neue Suche nach: LYU BINBIN
- Neue Suche nach: LIU DAWEI
- Neue Suche nach: LI YANG
- Neue Suche nach: YE LIN
- Neue Suche nach: YU LI
- Neue Suche nach: ZHANG CHANGRONG
- Neue Suche nach: ZHA JUN
- Neue Suche nach: GUO PENG
- Neue Suche nach: GUO HONGTAO
- Neue Suche nach: LYU BINBIN
- Neue Suche nach: LIU DAWEI
- Neue Suche nach: LI YANG
- Neue Suche nach: YE LIN
- Neue Suche nach: YU LI
- Neue Suche nach: ZHANG CHANGRONG
- Neue Suche nach: ZHA JUN
- Neue Suche nach: GUO PENG
The invention relates to the field of aircraft manufacturing, in particular to an aircraft and an aircraft control method thereof. The aircraft comprises a fuselage body and wings which are symmetrically arranged, a control part is arranged at the position, close to a wing tip, of any wing, each control part is used for controlling rolling motion of the corresponding wing, each control part comprises a rolling restraining device, each rolling restraining device comprises a shell and a sliding block, and the sliding blocks are movably arranged in the shells. The aircraft further comprises a driving assembly and a control assembly. The driving assembly is arranged in the shell and drives the sliding blocks to move in the shells. The control assembly is used for controlling the driving assembly to work, the sliding blocks and the shells are correspondingly provided with a plurality of open holes respectively, and the open holes of the sliding blocks and the open holes of the shells are selectively communicated along with the movement of the sliding blocks. According to the aircraft, the original aerodynamic configuration and the overall structure of the wings are not damaged, the occurrence of tumbling in the flight process is effectively improved, and the stability and the flight quality of the aircraft are not influenced.
本发明涉及飞行器制造领域，具体而言，涉及一种飞行器及其飞行器控制方法。包括机身和对称设置机翼，在任一机翼靠近翼梢处设置有控制部，控制部用于控制机翼的翻滚运动，控制部包括翻滚抑制装置，翻滚抑制装置包括壳体和滑块，滑块可移动地设置在壳体中。还包括驱动组件，驱动组件设置在壳体中，驱动滑块在壳体中移动。控制组件，控制驱动组件的工作，滑块与壳体分别对应设置有多个开孔，滑块开孔与壳体开孔随滑块的运动可选择的实现连通。本发明在不破坏机翼原有的气动外形和总体结构，有效的改进飞行过程中翻滚的出现，同时还不会影响到飞行器的稳定性和飞行品质。
Dokumentinformationen
Aircraft and aircraft control method thereof
一种飞行器及其飞行器控制方法
2020-12-25
Patent
Elektronische Ressource
Chinesisch
| IPC: | B64C AEROPLANES , Flugzeuge |
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