Fin control surface driving device
CN224409669UActive Publication Date: 2026-06-26TIANJIN FENGMING UAV TECHNOLOGY CO LTD
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Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- TIANJIN FENGMING UAV TECHNOLOGY CO LTD
- Filing Date
- 2025-09-01
- Publication Date
- 2026-06-26
AI Technical Summary
Technical Problem
[0003]在现有技术中,可将所述驱动装置设置于机身内部,但不同无人机的舵面在飞行过程中受到的铰链力矩不同,因此需要的偏转角度和扭矩不同,而能输出大扭矩的驱动装置体积更大,而机身内部的装配空间往往有限,存在能够适配机身空间的体积较小的驱动装置,其输出扭矩不足的情况
Benefits of technology
[0018]根据本申请某些实施例提供的技术方案,所述传动组件和驱动机构均设置于机身的内部,所述舵面位于机身外部,所述舵面组件的舵面转动轴贯穿机身与所述舵面连接。
✦ Generated by Eureka AI based on patent content.
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Figure CN224409669U_ABST
Abstract
The application provides a tail rudder driving device, and relates to the technical field of unmanned aerial vehicles.The tail rudder driving device comprises a transmission assembly, a driving mechanism and a rudder assembly.The transmission assembly comprises a first transmission arm, a transmission shaft and a second transmission arm.The first transmission arm is fixedly connected with the transmission shaft, and the transmission shaft is movably connected with the second transmission arm to adjust the length of the second transmission arm.The minimum length of the second transmission arm is greater than that of the first transmission arm.The driving mechanism is fixedly connected with the first transmission arm and is used for driving the first transmission arm to rotate.The rudder assembly is fixedly connected with the second transmission arm, so that the driving mechanism drives the rudder to rotate through the first transmission arm, the transmission shaft and the second transmission arm.Because the length of the second transmission arm is greater than that of the first transmission arm, according to the torque transmission principle, the torque is amplified through the length difference when the torque is transmitted through the transmission assembly, so that the tail rudder driving device with a small volume installed in the fuselage can output greater torque and meet the deflection requirements of the rudder.
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