The invention discloses a helicopter comprehensive suspended beam assembling device, and relates to the technical field of helicopter suspended beam machining and assembling. The device comprises suspended beam bodies and a mounting sleeve, the suspended beam bodies are fixedly connected with the mounting sleeve through a clamping mechanism, a connecting rod is fixedly connected between the opposite side walls of the two suspended beam bodies through a width adjusting mechanism, a fixed sleeve is fixedly connected to the upper surface of the mounting sleeve, and a telescopic rod is slidably connected to the upper surface of the fixed sleeve; a plurality of symmetrically-distributed round holes are formed in the two side walls of the fixing sleeve, a fixing rod is fixedly connected between the inner walls of the telescopic rod, an elastic fixing piece is fixedly connected to the lower surface of the fixing rod, and a protruding head is fixedly connected to the lower surface of the elastic fixing piece and penetrates through the telescopic rod. The problems that most of existing helicopter comprehensive suspended beam assembling devices are fixedly mounted and are difficult to dismount, mount and replace in real time, and meanwhile, the mounting height of the device is difficult to adjust in real time when an existing suspended beam is mounted are solved.
本发明公开了一种直升机综合挂梁装配装置,涉及直升机挂梁加工装配技术领域。本发明包括挂梁本体和安装套,挂梁本体通过卡接机构与安装套进行固定连接,两挂梁本体相对面侧壁之间通过调宽机构固定连接有连接杆,安装套的上表面固定连接有固定套筒,固定套筒上表面滑动连接有伸缩杆,固定套筒两侧壁均开设有若干对称分布的圆孔,伸缩杆内壁之间固定连接有固定杆,固定杆下表面固定连接有弹性固件,弹性固件的下表面固定连接有凸头,凸头贯穿伸缩杆。本发明解决了现有的直升机综合挂梁装配装置大多之间进行固定安装,难以对其进行实时拆卸安装更换等,同时现有的挂梁在安装时难以实时调节装置的安装高度的问题。
Helicopter comprehensive suspended beam assembling device
一种直升机综合挂梁装配装置
2021-08-13
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 |
Helicopter comprehensive suspended beam assembling device
European Patent Office | 2021
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Emerald Group Publishing | 2000
Criteria for Externally Suspended Helicopter Loads
NTIS | 1971
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