The invention provides a steering engine structure and an aircraft, and relates to the technical field of aircraft control systems, the steering engine structure is used for being arranged in a driving cabin of the aircraft, and the steering engine structure comprises a supporting assembly; the driving motor is arranged on the supporting assembly; the shaft body is rotationally connected to the supporting assembly, the shaft body is connected with a rotor of the driving motor through a first transmission assembly, the shaft body is used for being connected with a control surface of the aircraft, and the control surface can swing when the shaft body rotates; the feedback assembly is arranged on the driving motor and connected with the rotor, and the feedback assembly is used for monitoring the implementation position of the rotor; and the control terminal is in signal connection with the driving motor and the feedback assembly, and has the characteristics of simple structure, small size, light weight and capability of realizing multi-circle rotation action, is easy to mount and dismount, and is suitable for the control requirements of various aircrafts.

    本发明提供一种舵机结构及飞行器,涉及飞行器操纵系统技术领域,用于设置在飞行器的驱动舱内,该舵机结构包括:支撑组件;驱动电机,驱动电机设置在支撑组件上;轴体,轴体转动连接在支撑组件上,轴体与驱动电机的转子通过第一传动组件连接,轴体用于与飞行器的舵面连接,舵面能够在轴体转动时进行摆动;反馈组件,反馈组件设置在驱动电机上并与转子连接,反馈组件用于监测转子的实施位置;控制终端,控制终端与驱动电机和反馈组件信号连接,具有结构简单、尺寸小、重量轻、可实现多圈旋转动作的特点,易于安装和拆卸,适用于各类飞行器的控制需求。


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    Title :

    Steering engine structure and aircraft


    Additional title:

    一种舵机结构及飞行器


    Contributors:
    LYU JIANLIANG (author) / LIANG DONG (author) / CHAI LIREN (author) / CAO XINLEI (author) / YANG TAO (author) / WANG SHUAIBING (author) / YU SHILEI (author) / JIA LIZHEN (author)

    Publication date :

    2025-02-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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