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Airplane luggage compartment lock
The invention provides an aircraft luggage compartment lock. The aircraft luggage compartment lock comprises a mounting seat; the spring bolt assembly comprises a spring bolt and a linkage plate, the spring bolt is slidably arranged on the mounting base in a penetrating mode, one end of the linkage plate is connected with one end of the spring bolt, and a clamping hole is formed in the linkage plate; the lock body mechanism comprises a lock rod, a lock head assembly and a linkage rod, the lock rod is rotatably arranged on the mounting base in a penetrating mode and penetrates through the linkage plate, the lock head assembly is used for driving the lock rod to rotate, one end of the linkage rod is arranged on the lock rod in a sleeving mode, and the other end of the linkage rod is clamped with the clamping hole; the control assembly is used for driving the lock rod to rotate. Due to the fact that after the lock rod rotates, the lock tongue can be driven by the linkage rod and the linkage plate to stretch out of or retract into the installation base, the firmness of the locking state of the airplane luggage compartment lock is guaranteed, meanwhile, the structure of the airplane luggage compartment lock is simplified, the light weight of the luggage compartment lock is achieved, the manufacturing cost of the luggage compartment lock is reduced, and the practicability of the airplane luggage compartment lock is improved. And further, partial requirements of a helicopter on the luggage compartment lock are met.
本发明提供了一种飞机行李舱锁，包括：安装座；锁舌组件包括锁舌和联动板，锁舌可滑动地穿设于安装座上，联动板一端与锁舌的一端连接，联动板上开设有卡孔；锁体机构包括锁杆、锁头组件以及联动杆，锁杆可转动的穿设于安装座上并贯穿联动板，锁头组件用于带动锁杆转动，联动杆的一端套设于锁杆上，另一端与卡孔卡合；控制组件用于带动锁杆转动。因为锁杆转动后能够通过联动杆和联动板带动锁舌伸出或缩入安装座，从而在保证本飞机行李舱锁锁固状态的牢固性的同时，通过简化飞机行李舱锁的结构，实现行李舱锁的轻量化，并且也因此减少了行李舱锁的制造成本，进而满足了直升飞机对行李舱锁的部分要求。
Airplane luggage compartment lock
The invention provides an aircraft luggage compartment lock. The aircraft luggage compartment lock comprises a mounting seat; the spring bolt assembly comprises a spring bolt and a linkage plate, the spring bolt is slidably arranged on the mounting base in a penetrating mode, one end of the linkage plate is connected with one end of the spring bolt, and a clamping hole is formed in the linkage plate; the lock body mechanism comprises a lock rod, a lock head assembly and a linkage rod, the lock rod is rotatably arranged on the mounting base in a penetrating mode and penetrates through the linkage plate, the lock head assembly is used for driving the lock rod to rotate, one end of the linkage rod is arranged on the lock rod in a sleeving mode, and the other end of the linkage rod is clamped with the clamping hole; the control assembly is used for driving the lock rod to rotate. Due to the fact that after the lock rod rotates, the lock tongue can be driven by the linkage rod and the linkage plate to stretch out of or retract into the installation base, the firmness of the locking state of the airplane luggage compartment lock is guaranteed, meanwhile, the structure of the airplane luggage compartment lock is simplified, the light weight of the luggage compartment lock is achieved, the manufacturing cost of the luggage compartment lock is reduced, and the practicability of the airplane luggage compartment lock is improved. And further, partial requirements of a helicopter on the luggage compartment lock are met.
本发明提供了一种飞机行李舱锁，包括：安装座；锁舌组件包括锁舌和联动板，锁舌可滑动地穿设于安装座上，联动板一端与锁舌的一端连接，联动板上开设有卡孔；锁体机构包括锁杆、锁头组件以及联动杆，锁杆可转动的穿设于安装座上并贯穿联动板，锁头组件用于带动锁杆转动，联动杆的一端套设于锁杆上，另一端与卡孔卡合；控制组件用于带动锁杆转动。因为锁杆转动后能够通过联动杆和联动板带动锁舌伸出或缩入安装座，从而在保证本飞机行李舱锁锁固状态的牢固性的同时，通过简化飞机行李舱锁的结构，实现行李舱锁的轻量化，并且也因此减少了行李舱锁的制造成本，进而满足了直升飞机对行李舱锁的部分要求。
Airplane luggage compartment lock
飞机行李舱锁
CHEN JINHONG (author) / XU KAICHUAN (author) / MA CHUNHAO (author)
2024-10-01
Patent
Electronic Resource
Chinese
IPC:
E05B
LOCKS
,
Schlösser
Vehicle luggage compartment control method, vehicle luggage compartment and vehicle
| European Patent Office | 2024