The invention provides an aircraft control surface loading test device and an aircraft control surface loading test method, and relates to the technical field of aircraft testing. The aircraft control surface loading test device comprises a rack, a driving mechanism, a loading mechanism and a power mechanism, the driving mechanism is arranged on the rack; the loading mechanism is arranged on the driving mechanism, the driving mechanism is used for driving the loading mechanism to move relative to the rack, and the loading mechanism is used for pressing the control surface; and the power mechanism is connected with the loading mechanism and is used for providing driving force for pressing the control surface for the loading mechanism. Therefore, the adaptability and universality of the aircraft control surface loading test device are improved, and the cost is effectively reduced. And the control surface loading test device is compact in structure, small in occupied space and convenient to disassemble and transport.
本发明提供了一种飞机舵面加载试验装置及飞机舵面加载试验方法,涉及飞机测试技术领域。飞机舵面加载试验装置包括台架、驱动机构、加载机构以及动力机构;驱动机构设置于台架;加载机构设置于驱动机构,驱动机构用于驱动加载机构相对台架移动,加载机构用于压持舵面;动力机构与加载机构连接,动力机构部用于为加载机构提供压持舵面的驱动力。因此提高了飞机舵面加载试验装置的适应性及通用性,有效降低了成本;且舵面加载试验装置结构紧凑,占用空间小,便于拆卸和运输。
Aircraft control surface loading test device and aircraft control surface loading test method
一种飞机舵面加载试验装置及飞机舵面加载试验方法
2024-03-29
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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