The invention belongs to the field of aerospace equipment, and particularly relates to a passive follow-up loading device for a deformable wing and a working method. The loading device comprises a supporting frame, a test wing surface bracket, a test wing surface, a high-pressure cylinder assembly and a plurality of passive loading modules, the test airfoil supports are arranged on the two sides of the supporting frame, test airfoils are arranged on the test airfoil supports, and the passive loading modules are arranged on the supporting frame and used for adjusting the tension of the steel wire rope; the passive loading module comprises a connecting assembly, a pulley assembly, a loading assembly, a measuring assembly and a bearing square tube, the connecting assembly is arranged on the testing wing surface and connected with the multiple steel wire ropes, and the pulley assembly and the bearing square tube are arranged on the supporting frame in a staggered mode. The follow-up loading device adopts a modular design, is single in part, simple in structure, good in interchangeability, convenient to install and low in cost, shortens the preparation period, and also reduces the danger at the same time.
本发明属于航空航天设备领域,特别是涉及一种变形翼被动式随动加载装置及工作方法;该加载装置,包括:支撑框架、测试翼面支架、测试翼面、高压气缸组件、多个被动加载模块;测试翼面支架设于支撑框架的两侧,且在测试翼面支架上设有测试翼面,多个被动加载模块设于支撑框架上,被动加载模块用于调节钢丝绳的拉力;被动加载模块包括连接组件、滑轮组件、加载组件、测量组件、以及承载方管,连接组件设于测试翼面上,连接组件分别与多个钢丝绳连接,滑轮组件和承载方管错位设于支撑框架上。该随动加载装置采用模块化设计,零件单一,结构简单,互换性好,安装方便,且成本低,降低了准备周期,同时也降低了危险性。
Deformable wing passive follow-up loading device and working method
一种变形翼被动式随动加载装置及工作方法
2024-09-27
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 |