According to the technical scheme, the novel aircraft wing installation auxiliary bracket is characterized in that a damping mechanism and an installation mechanism are arranged on a base, the damping mechanism comprises a damping piece and a placing piece, the damping piece is fixedly connected with the placing piece through a second fixing table, and the installation mechanism comprises a lifting piece and a clamping piece; the placing piece and the clamping piece each comprise a deflection set, a tightening set is arranged on the deflection set on the lifting piece, and the deflection set is fixedly connected with the tightening set through a first fixing rod. According to the lifting device, the buffering mechanism is arranged, and the damping part is arranged below the placing frame, so that when a wing is placed on the placing frame through the lifting device, the impact force between the wing and the placing frame is reduced through the damping part, and the wing is prevented from being damaged in the placing process; the wing is fixed between the placing frame and the tightening frame through tightening of the tightening group, so that the placing angle of the wing is adjusted by driving the sliding assembly and the tightening assembly to deflect, and different parts of the wing can be conveniently assembled.
本发明公开了一种新型飞机机翼安装辅助托架,其技术方案要点是:底座上设置有减震机构和安装机构,减震机构包括有减震件和放置件,减震件通过二号固定台与放置件固定连接,安装机构包括有升降件和卡紧件,放置件与卡紧件均包括有偏转组,升降件上的偏转组上设置有收紧组,偏转组通过一号固定杆与收紧组固定连接。本发明设置有缓冲机构,通过在放置架下设置的减震件,当机翼通过吊装装置放在放置架上通过减震件从而减少机翼与放置架之间的冲击力,从而避免机翼在放置的过程中损坏;通过收紧组的收紧从而使机翼固定在放置架与收紧架之间,从而通过带动滑动组件与收紧组件进行偏转,从而来调节机翼放置的角度,从而方便机翼进行不同部位的组装。
Novel airplane wing installation auxiliary bracket
一种新型飞机机翼安装辅助托架
2023-10-27
Patent
Elektronische Ressource
Chinesisch
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 |
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