一种用于飞机设备舱口盖的锁紧机构及使用方法,含有口盖锁轴和活动手柄,所述的口盖锁轴设置在飞机设备舱口盖上,口盖锁轴的一端连接口盖的锁闩,口盖锁轴的另一端有T型接口,所述的活动手柄上设有手柄、手柄轴、和限位机构,手柄轴固定连接在手柄上,手柄轴上设有旋转销,限位机构镶嵌在手柄轴与手柄之间,活动手柄的手柄轴和旋转销与口盖锁轴的T型接口匹配。通过活动手柄与口盖锁轴13相对位置锁定,便可通过操作手柄实现口盖的开启/关闭和姿态调整。
According to the locking mechanism for the aircraft equipment hatch cover and the using method, the locking mechanism comprises a cover lock shaft and a movable handle, the cover lock shaft is arranged on the aircraft equipment hatch cover, one end of the cover lock shaft is connected with a plunger latch of the cover, the other end of the cover lock shaft is provided with a T-shaped connector, the movable handle is provided with a handle, a handle shaft and a limiting mechanism, and the limiting mechanism is arranged on the handle shaft. The handle shaft is fixedly connected to the handle, a rotating pin is arranged on the handle shaft, the limiting mechanism is embedded between the handle shaft and the handle, and the handle shaft of the movable handle and the rotating pin are matched with the T-shaped connector of the covering cap locking shaft. Opening/closing and posture adjustment of the covering cap can be achieved by operating the handle through relative position locking of the movable handle and the covering cap locking shaft 13.
一种用于飞机设备舱口盖的锁紧机构及使用方法
17.06.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |