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Airplane trunk door lock structure
The invention discloses an airplane trunk door lock structure, and particularly relates to the field of trunk structures, and the airplane trunk door lock structure comprises a trunk body mounted in a cabin; the box door is rotationally connected to the box body; the door lock assembly comprises a plunger latch connected to the box body; the locking assembly comprises a lock seat, a handle, a rotating shaft, a cam and a lock hook, the lock latch is matched with the lock hook, the lock seat is installed on the box door, the handle is elastically and rotatably connected to the lock seat, the cam and the lock hook which are located on the inner side and the outer side of the lock seat respectively rotate synchronously, a clamping groove is formed in the side end of the handle, and a clamping block is fixed to the side end of the cam; the clamping block is arranged in the clamping groove, the groove length of the clamping groove is larger than that of the clamping block, the two sides of the locking assembly are each of a double-spring structure, when the trunk door is closed, the lock hook can be automatically buckled with the plunger latch and is not in linkage with the handle, the door lock is in a double-lock-hook mode, the internal structure is simple, the mechanical property is reliable, and the trunk door lock can be applied to various upturning type trunks.
本发明公开了一种飞机行李箱门锁结构,具体涉及行李箱结构领域,包括箱体,安装于机舱内;箱门,转动连接于箱体上;门锁组件,包括连接于箱体上的锁闩;锁紧组件,包括锁座、手柄、转轴、凸轮和锁钩,锁闩和锁钩相配合,锁座安装于箱门上,手柄弹性转动连接于锁座上,分别位于锁座内外侧的凸轮和锁钩同步转动,手柄侧端开设有卡槽,凸轮的侧端固定有卡块,卡块置于卡槽内且卡槽的槽长大于卡块的长度,锁紧组件的两侧均采用双弹簧结构,箱门关闭时锁钩能够自行与锁闩扣紧,不与手柄联动,并且门锁采用双锁钩形式,内部结构简单、力学性能可靠,可应用于各类上翻式行李箱上。
Airplane trunk door lock structure
The invention discloses an airplane trunk door lock structure, and particularly relates to the field of trunk structures, and the airplane trunk door lock structure comprises a trunk body mounted in a cabin; the box door is rotationally connected to the box body; the door lock assembly comprises a plunger latch connected to the box body; the locking assembly comprises a lock seat, a handle, a rotating shaft, a cam and a lock hook, the lock latch is matched with the lock hook, the lock seat is installed on the box door, the handle is elastically and rotatably connected to the lock seat, the cam and the lock hook which are located on the inner side and the outer side of the lock seat respectively rotate synchronously, a clamping groove is formed in the side end of the handle, and a clamping block is fixed to the side end of the cam; the clamping block is arranged in the clamping groove, the groove length of the clamping groove is larger than that of the clamping block, the two sides of the locking assembly are each of a double-spring structure, when the trunk door is closed, the lock hook can be automatically buckled with the plunger latch and is not in linkage with the handle, the door lock is in a double-lock-hook mode, the internal structure is simple, the mechanical property is reliable, and the trunk door lock can be applied to various upturning type trunks.
本发明公开了一种飞机行李箱门锁结构,具体涉及行李箱结构领域,包括箱体,安装于机舱内;箱门,转动连接于箱体上;门锁组件,包括连接于箱体上的锁闩;锁紧组件,包括锁座、手柄、转轴、凸轮和锁钩,锁闩和锁钩相配合,锁座安装于箱门上,手柄弹性转动连接于锁座上,分别位于锁座内外侧的凸轮和锁钩同步转动,手柄侧端开设有卡槽,凸轮的侧端固定有卡块,卡块置于卡槽内且卡槽的槽长大于卡块的长度,锁紧组件的两侧均采用双弹簧结构,箱门关闭时锁钩能够自行与锁闩扣紧,不与手柄联动,并且门锁采用双锁钩形式,内部结构简单、力学性能可靠,可应用于各类上翻式行李箱上。
Airplane trunk door lock structure
一种飞机行李箱门锁结构
MIAO PENG (author) / WANG HAIXIANG (author) / YANG YIMING (author) / YIN YANJIAO (author) / YU ZHIGANG (author) / FENG QINGXIAO (author)
2024-10-08
Patent
Electronic Resource
Chinese
IPC:
E05B
LOCKS
,
Schlösser