Wing control surface
Wing control surface
- Neue Suche nach: XIAO SHAN
- Neue Suche nach: XUE HUIMIN
- Neue Suche nach: WANG MEIQI
- Neue Suche nach: ZHANG NING
- Neue Suche nach: WANG XIANHAO
- Neue Suche nach: XIAO SHAN
- Neue Suche nach: XUE HUIMIN
- Neue Suche nach: WANG MEIQI
- Neue Suche nach: ZHANG NING
- Neue Suche nach: WANG XIANHAO
The invention belongs to the technical field of wing design, and particularly relates to a wing control surface. The wing control surface comprises an upper panel (1) and a lower panel (2), an included angle is formed between the upper panel (1) and the lower panel (2), so that the distance between the upper panel (1) and the lower panel (2) at a wing front edge (3) is smaller than the distance between the upper panel (1) and the lower panel (2) at a wing rear edge (4), and the upper panel (1) and the lower panel (2) are supported by a corrugated core plate (5) formed in a wavy folding mode. The lightweight design of the control surface structure is achieved, and the bearing performance of the control surface structure is improved.
本申请属于机翼设计技术领域，特别涉及一种机翼舵面。该机翼舵面包括上面板(1)及下面板(2)，上面板(1)与下面板(2)之间具有夹角，以使得上面板(1)与下面板(2)在机翼前缘(3)处的距离小于在机翼后缘(4)处的距离，所述上面板(1)与下面板(2)之间通过波浪型折叠方式形成的波纹芯板(5)进行支撑。本申请实现了舵面结构的轻量化设计，提高了舵面结构的承载性能。
Dokumentinformationen
Wing control surface
一种机翼舵面
2023-12-29
Patent
Elektronische Ressource
Chinesisch
| IPC: | B64C AEROPLANES , Flugzeuge |