A platform for research: civil engineering, architecture and urbanism
A platform for research: civil engineering, architecture and urbanism
Lock seat assembly, cabin door lock and locking device
The invention relates to a lock seat assembly, a cabin door lockset and a locking device, and belongs to the technical field of cabin door locks, the locking device comprises the cabin door lockset, the cabin door lockset comprises a lock seat assembly, a lock box assembly and a locking indication assembly, the lock seat assembly comprises a lock seat main body, a lock box, a lock box and a locking indication assembly, the lock seat main body is provided with two fixing parts, and the two fixing parts are used for being connected with a door frame of a cabin door; the two locking pieces are arranged on the surfaces of the two fixing parts respectively in an attached mode, each locking piece is connected with the corresponding fixing part in a meshed mode through a tooth-shaped connecting part, and each tooth-shaped connecting part is provided with a plurality of tooth-shaped single bodies; and the two groups of fasteners are used for fixing the lock seat main body and the two locking pieces on a door frame of the cabin door in a detachable manner. Structural parts in the lock bracket assembly are reduced, so that the mounting height of the lock bracket main body is reduced, and the requirement of small space of a helicopter can be met.
本发明涉及一种锁座组件、舱门锁具以及锁闭装置，属于舱门锁技术领域，锁闭装置包括舱门锁具，舱门锁具包括锁座组件、锁盒组件以及锁闭指示组件，锁座组件包括：锁座主体，具有两个固定部，两个所述固定部用于与所述舱门的门框连接；两个锁定件，以贴合的方式分别设置在两个所述固定部的表面，每个所述锁定件均通过一个齿形连接部与对应的所述固定部啮合连接，所述齿形连接部具有若干个齿形单体；以及两组紧固件，用于将所述锁座主体和两个所述锁定件以可拆卸的方式固定在所述舱门的门框上。本发明通过减少锁座组件内的结构件，使得锁座主体的安装高度得到降低，能够适应直升机空间小的需求。
Lock seat assembly, cabin door lock and locking device
The invention relates to a lock seat assembly, a cabin door lockset and a locking device, and belongs to the technical field of cabin door locks, the locking device comprises the cabin door lockset, the cabin door lockset comprises a lock seat assembly, a lock box assembly and a locking indication assembly, the lock seat assembly comprises a lock seat main body, a lock box, a lock box and a locking indication assembly, the lock seat main body is provided with two fixing parts, and the two fixing parts are used for being connected with a door frame of a cabin door; the two locking pieces are arranged on the surfaces of the two fixing parts respectively in an attached mode, each locking piece is connected with the corresponding fixing part in a meshed mode through a tooth-shaped connecting part, and each tooth-shaped connecting part is provided with a plurality of tooth-shaped single bodies; and the two groups of fasteners are used for fixing the lock seat main body and the two locking pieces on a door frame of the cabin door in a detachable manner. Structural parts in the lock bracket assembly are reduced, so that the mounting height of the lock bracket main body is reduced, and the requirement of small space of a helicopter can be met.
本发明涉及一种锁座组件、舱门锁具以及锁闭装置，属于舱门锁技术领域，锁闭装置包括舱门锁具，舱门锁具包括锁座组件、锁盒组件以及锁闭指示组件，锁座组件包括：锁座主体，具有两个固定部，两个所述固定部用于与所述舱门的门框连接；两个锁定件，以贴合的方式分别设置在两个所述固定部的表面，每个所述锁定件均通过一个齿形连接部与对应的所述固定部啮合连接，所述齿形连接部具有若干个齿形单体；以及两组紧固件，用于将所述锁座主体和两个所述锁定件以可拆卸的方式固定在所述舱门的门框上。本发明通过减少锁座组件内的结构件，使得锁座主体的安装高度得到降低，能够适应直升机空间小的需求。
Lock seat assembly, cabin door lock and locking device
锁座组件、舱门锁具以及锁闭装置
SHI SONGCHAO (author) / ZHANG HONGJIA (author) / HAO XINXIN (author) / ZHANG JUN (author)
2024-06-04
Patent
Electronic Resource
Chinese
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