The invention provides a fault monitoring device and method for an aviation servo actuation test bench, and belongs to the technical field of aircraft detection.The fault monitoring device comprises a hydraulic test system and a control system, the hydraulic test system is used for simulating faults of a servo actuation system and collecting data through various sensors, and the control system is used for controlling the hydraulic test system; and the control system is used for controlling the hydraulic test system to reach required monitoring conditions and collecting monitoring data, is provided with a deep learning model, carries out training through collected fault simulation data, and is used for comprehensively analyzing and effectively detecting various fault types after training. According to the invention, the reliability and safety of the servo system are obviously improved, and the method is of great significance for ensuring the performance of an aircraft and carrying out preventive maintenance.
本发明提供了一种航空伺服作动测试台故障监测装置及方法,属于飞机检测技术领域,故障监测装置包括液压测试系统和控制系统,液压测试系统用于模拟伺服作动系统故障并通过各种传感器采集数据,控制系统用于控制液压测试系统达到所需监测条件,采集监测数据,其搭载有深度学习模型,通过采集的故障模拟数据进行训练,训练后用于全面分析并有效检测各种故障类型。本发明显著提升了伺服系统的可靠性和安全性,对于确保航空器性能和进行预防性维护具有重要意义。
Fault monitoring device and method for aviation servo actuation test bench
一种航空伺服作动测试台故障监测装置及方法
2024-12-10
Patent
Electronic Resource
Chinese
IPC: | 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 / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung |
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