The invention discloses a plane interior trim part clamping mechanism with an anti-vibration function. The plane interior trim part clamping mechanism comprises a luggage compartment, a first anti-vibration mechanism is arranged at the top of the luggage compartment, a second anti-vibration mechanism is arranged behind the luggage compartment, the first anti-vibration mechanism comprises two corresponding spring grooves, springs are arranged in the spring grooves, and pull rods are arranged in the springs; a damping ring is arranged between a cabin and the luggage compartment, a guide sleeve is arranged at the top of the luggage compartment, the pull rod is connected with a pressing rod arranged in the luggage compartment, the head of the pressing rod is hinged to the tail of one pull rod,and the tail of the pressing rod is fixed to the other pull rod through nuts; and the second anti-vibration mechanism comprises a lever, a fulcrum is arranged in the middle of the lever, the head ofthe lever is connected with the rear portion of the luggage compartment, a compression rod A is arranged at the tail of the lever and connected with a spring device A, a spring device B is arranged between the cabin and the rear portion of the luggage compartment, and the spring device B is connected with a compression rod B on the lever. The plane interior trim part clamping mechanism is stable in structure, good in vibration resistance, convenient to install and labor-saving, and tool-free installation is basically achieved.
本发明公开了一种具有抗振功能的飞机内饰件夹持机构,包括行李舱,行李舱顶部设有第一抗振机构,行李舱的后方设有第二抗振机构,第一抗振机构包括两个对应的弹簧槽,弹簧槽内设有弹簧,弹簧内设有拉杆,机舱与行李舱之间设有减震圈,行李舱的顶部设有导向套,拉杆与设于行李舱内的按压杆相连,按压杆的头部与拉杆的尾部铰接在一起,按压杆的尾部通过螺母固定在另一拉杆上;第二抗振机构包括杠杆,杠杆的中部设有支点,杠杆的头部与行李舱的后方相连,杠杆的尾部上设有压缩杆A,压缩杆A与弹簧装置A相连,机舱与行李舱的后方之间设有弹簧装置B与杠杆上的压缩杆B相连。本发明结构稳固,抗振性能好,基本实现免工具安装,安装方便,节省人力。
Plane interior trim part clamping mechanism with anti-vibration function
一种具有抗振功能的飞机内饰件夹持机构
2020-12-15
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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Interior trim part with touch control function and method for manufacturing interior trim part
Europäisches Patentamt | 2022
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