The invention relates to the technical field of aviation aircrafts, and provides a manufacturing method of a flap assembly, the flap assembly and a vertical take-off and landing aircraft, the method comprises the following steps: rotationally connecting a wing box section with a flap section, and arranging a ducted fan propulsion mechanism on the flap section; a driving mechanism with a harmonic reducer is in driving connection with the flap section, so that the driving mechanism drives the flap section to rotate through the harmonic reducer; a locking mechanism with a pneumatic spring is connected with the flap section, so that the locking mechanism locks the flap section through the pneumatic spring. According to the manufacturing method of the flap assembly, the harmonic reducer is used for driving the flap section to rotate, so that the torque of the driving mechanism is amplified, and the flap section is driven to rotate more easily; and the pneumatic spring is connected with the flap section to lock the flap section, so that the flap section is better prevented from rotating, the rotation angle between the flap section and the wing box section is ensured to be unchanged, the influence on the flight state of the vertical take-off and landing aircraft is avoided, and the safety is improved.
本发明涉及航空飞行器技术领域,提供一种襟翼组件的制造方法、襟翼组件及垂直起降飞行器,该方法包括以下步骤:将机翼盒段与襟翼段旋转连接,并将涵道风扇推进机构设于襟翼段;将具有谐波减速器的驱动机构与襟翼段驱动连接,使驱动机构通过谐波减速器驱动襟翼段旋转;将具有气动弹簧的锁止机构与襟翼段连接,使锁止机构通过气动弹簧锁定襟翼段。本发明提供的襟翼组件的制造方法,通过将谐波减速器来驱动襟翼段旋转,从而放大驱动机构的扭矩,更容易地驱动襟翼段旋转;且还将气动弹簧与襟翼段连接来锁定襟翼段,更好地防止襟翼段转动,从而保证襟翼段与机翼盒段之间的旋转角度不变,避免影响垂直起降飞行器的飞行状态,提高了安全性。
Flap assembly manufacturing method, flap assembly and vertical take-off and landing aircraft
襟翼组件的制造方法、襟翼组件及垂直起降飞行器
2025-05-09
Patent
Electronic Resource
Chinese
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