The present disclosure relates to a landing gear system that may include: a sleeve coupled to a fuselage of an aircraft, such as a city aerial mobile vehicle; a steering lever, one side of which is inserted into the sleeve and the other side of which is connected to a tire; a magnetorheological (MR) damper including a cylinder coupled to the sleeve and a piston coupled to the steering rod; a sensor unit configured to measure a condition of the urban aerial vehicle; and a controller configured to control a damping force of the MR damper based on measurement data of the sensor unit. The sensor unit may include a first sensor for measuring a stroke of the MR damper and a second sensor for measuring an acceleration of the bushing.

    本公开涉及一种起落架系统,其可以包括:套管,联接到诸如城市空中移动体车辆的飞行器的机身;转向杆,其一侧插入套管,另一侧连接到轮胎;磁流变(MR)减振器,包括联接到套管的气缸和联接到转向杆的活塞;传感器单元,被配置为测量城市空中移动体车辆的状况;以及控制器,被配置为基于传感器单元的测量数据控制MR减振器的阻尼力。传感器单元可以包括用于测量MR减振器的行程的第一传感器和用于测量套管的加速度的第二传感器。


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    Title :

    Landing gear system with magnetorheological damper


    Additional title:

    具有磁流变减振器的起落架系统


    Contributors:

    Publication date :

    2024-06-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein



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