The invention belongs to a full-size airplane static strength ground test pose control technology, and particularly relates to an airplane ground test pose active control device and method, and position control hydraulic cylinders, which comprise a plurality of vertical position control hydraulic cylinders respectively installed on each undercarriage of an airplane; the drivers are respectively arranged between each undercarriage of the airplane and the position control hydraulic cylinder; the displacement sensors are respectively arranged on each undercarriage of the airplane and comprise a lateral displacement sensor and a plurality of vertical displacement sensors; the control system is respectively connected with the position control hydraulic cylinder, the driver and the displacement sensor, and adopts a step-by-step or simultaneous control mode of the driver and the position control hydraulic cylinder during control, so that the attitude of the aircraft is kept at a preset position.
本申请属于全尺寸飞机静强度地面试验位姿控制技术,特别涉及一种飞机地面试验位姿主动控制装置及方法,位控液压缸,包括分别安装在飞机各个起落架上的多个垂向的位控液压缸;驱动器,分别安装在飞机各个起落架与位控液压缸之间;位移传感器,分别安装在飞机各个起落架上,包括侧向的位移传感器以及多个垂向的位移传感器;控制系统,分别连接位控液压缸、驱动器以及位移传感器,控制时采用驱动器与位控液压缸分步或者同时控制的方式,是飞机姿态保持预设位置。
Aircraft ground test pose active control device and method
一种飞机地面试验位姿主动控制装置及方法
2024-03-05
Patent
Electronic Resource
Chinese
IPC: | G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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