The invention relates to the technical field of aircraft installation, and discloses an aircraft body central wing assembly system which comprises a first assembly hanging bracket and two first vertical rods fixedly connected to the outer surface of the upper end of the first assembly hanging bracket, and the first assembly hanging bracket is arranged on the outer surface of the rear end of the first assembly hanging bracket; a mold frame is arranged between the first assembly hanging brackets, and the outer surface of the lower end of the mold frame is movably connected with a machine body central wing. According to the aircraft body central wing assembly system, the scale strips and the corresponding pointers are arranged on the two sides of the assembly hanging bracket, an operator can rapidly and accurately adjust the height of the hanging bracket by directly reading the scales, it is ensured that the two sides are unified, the assembly process is simplified, efficiency is improved, assembly errors are greatly reduced, and the production efficiency is improved. The problem of inclination of the central wing of the aircraft body is effectively avoided, and the stability and the safety of the aircraft are powerfully guaranteed.
本发明涉及飞机安装技术领域,且公开了一种机体中央翼装配系统,包括第一装配吊架,以及固定连接在第一装配吊架上端外表面的两个第一竖杆,第一装配吊架的后端外表面设置有第一装配吊架,第一装配吊架与第一装配吊架之间设置有模具架,模具架的下端外表面活动连接有机体中央翼。本发明所述的一种机体中央翼装配系统,在装配吊架的两侧设置了刻度条与对应的指针,通过直接读取刻度,操作人员可以迅速而准确地调整吊架的高度,确保两侧达到统一,这不仅简化了装配流程,提高了效率,而且大大降低了装配误差,有效避免了机体中央翼的倾斜问题,为飞机的稳定性和安全性提供了有力保障。
Aircraft body central wing assembly system
一种机体中央翼装配系统
2024-04-19
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 |