According to the electric tilting helicopter wing, a flap steering engine end adjusting support is connected with a middle hinge structure of a flap conversion rocker arm, one end of a flap control surface connecting rocker arm is connected with the right end of the flap conversion rocker arm, and the other end of the flap control surface connecting rocker arm is connected with a flap control surface fixing connector; the aileron steering engine root mounting frame is located on the wing rib, and a single lug of the aileron steering engine root mounting frame is connected with double lugs of the aileron steering engine root; a middle fixing frame of the aileron steering engine is positioned on the rear beam, and two sides of the aileron steering engine are respectively arranged on the wing ribs; an aileron steering engine end adjusting support is connected with the rear beam, and an aileron steering engine end double-lug connector is connected with the left end of an aileron conversion rocker arm; an aileron steering engine end adjusting support is connected with a middle hinge structure of an aileron conversion rocker arm, one end of an aileron control plane connecting rocker arm is connected with the right end of the aileron conversion rocker arm, and the other end of the aileron control plane connecting rocker arm is connected with an aileron control plane fixing connector. A force transmission path of bending, twisting and shearing loads caused by concentrated mass of aerodynamic loads, a transmission system and a rotor system is provided, and the strength and rigidity of the flap and aileron steering engine connecting structure are guaranteed.
本发明提供一种电动倾转直升机机翼,该结构中襟翼舵机端部调节支座与襟翼转换摇臂中部铰链结构连接,襟翼舵面连接摇臂一端与襟翼转换摇臂右端连接,另一端与襟翼舵面固定接头连接;副翼舵机根部安装框位于翼肋上,副翼舵机根部安装框的单耳片与副翼舵机根部双耳片连接;副翼舵机中部固定框位于在后梁上,两侧边分别设置在翼肋上;副翼舵机端部调节支座与后梁连接,副翼舵机端部双耳接头与副翼转换摇臂左端连接;副翼舵机端部调节支座与副翼转换摇臂中部铰链结构连接,副翼舵面连接摇臂一端与副翼转换摇臂右端连接,另一端与副翼舵面固定接头连接;本发明提供了由气动载荷、传动系统和旋翼系统的集中质量引起的弯、扭、剪载荷的传力路径,保证了襟翼、副翼舵机连接结构的强度与刚度。
Electric tilting helicopter wing
一种电动倾转直升机机翼
2025-02-11
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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