一种尾桨集流环及直升机尾桨结构

By designing a lightweight tail rotor collector ring and combining it with a current detection circuit, the problems of complex tail rotor collector ring structure and detection of anti-icing heating components were solved, achieving lightweight design and real-time fault monitoring, and simplifying the installation and maintenance process.

CN117864395BActive Publication Date: 2026-07-17WUHAN AVIATION INSTR

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
WUHAN AVIATION INSTR
Filing Date
2023-12-20
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

The existing tail rotor collector ring has a complex structure and is heavy, and dynamic faults in the anti-icing heating components are difficult to detect, making testing and maintenance inconvenient.

Method used

The tail rotor adopts a coaxial design with the rotor assembly and stator assembly, combined with the brush box and conductive ring assembly, and integrates a current detection circuit. The integrity of the tail rotor heating circuit is monitored in real time through the circuit board, and it is connected to the drive shaft through a clamp, simplifying the structure.

Benefits of technology

It achieves a lightweight design, simplifies the installation and disassembly process, enables real-time monitoring of the integrity of the tail rotor heating circuit during high-speed rotation, locates faulty blades, and improves testing and maintenance efficiency.

✦ Generated by Eureka AI based on patent content.

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Abstract

本发明属于直升机旋翼防除冰技术领域,具体涉及一种尾桨集流环及直升机尾桨结构。包括转子组件(1),转子组件(1)插入定子组件(2)并同轴设置,转子组件(1)与定子组件(2)间能绕中轴线相对转动;定子组件(2)一侧安装有电刷盒(3);转子组件(1)包括基座(101),基座(101)伸入定子组件(2)的内端侧壁上堆叠有导电环组件(102);电刷盒(3)的电刷(302)与导电环组件(102)电搭接,电刷(302)经弹片(301)与定子组件(2)连接;基座(101)的外端唇口沿周向分布有水滴状槽(104)。本发明能可靠传输直升机尾桨防冰电流和信号,具有体积小、可定位故障桨叶的特点。
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