灵翼飞航科技有限公司

本发明专利技术提出了一种新型舵面连接结构，包括：机翼端肋片单元、舵面端肋片单元、旋转轴、桁条和机翼；所述舵面端肋片单元一端与桁条连接，另一端与机翼端肋片单元连接；所述旋转轴穿过舵面端肋片单元，两端与机翼固定连接；所述机翼端肋片单元由N1层肋片构成，所述N1≥3；所述舵面端肋片单元由N2层肋片构成，所述N2≥3。本发明专利技术提出的一种新型舵面连接结构，对目前市面上较为简单的铰接连接进行了优化，将原本的点接触受力或者小面积的面接触受力改为较大面积的面接触受力，改善了受力情况，提高了承受力，减少损坏的几率。
A new type of rudder surface connection structure

The invention provides a new type of rudder surface connection structure, which includes the fin end fin unit, the rudder surface end ribbed unit, the rotation axis, the truss and the wing, and the end of the rudder side fin unit is connected with the truss and the other end is connected with the fin end fin unit, and the rotating shaft passes through the fin unit of the rudder surface, and the ends are fixed to the wing. The wing end fin unit is composed of N1 layer fins, the N1 < 3, and the rudder surface end fin unit is composed of N2 layer fins, the N2 < 3. A new type of rudder face connection structure is proposed, which optimizes the simple articulated connection on the market. The force of the original contact force or small area surface contact is changed to the surface contact force of the larger area. The force condition is improved, the bearing capacity is improved and the damage probability is reduced.

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