Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Lock hook assembly for aircraft engine hood and locking mechanism of lock hook assembly
The invention relates to the technical field of aviation, in particular to a lock hook assembly for an aircraft engine hood and a locking mechanism of the lock hook assembly. A lock hook assembly for an aircraft engine hood comprises a lock hook component used for being buckled with and separated from a lock point on the engine hood, and a connecting rod component with one end connected with the lock hook component in a fastened mode, and one end of the connecting rod component is driven to enable the lock hook component to be buckled with and separated from the lock point. A length adjusting assembly is arranged between the latch hook component and the connecting rod component and used for adjusting the length of the latch hook component relative to the connecting rod component. The invention further provides a locking mechanism for the aircraft engine hood, the locking mechanism comprises the lock hook assembly, a handle component and a linkage assembly, and when the handle component is pulled vertically, the linkage assembly is used for driving the connecting rod component to rotate transversely; after the distance between the lock point and the lock hook component is loosened, the distance of the lock hook can be adjusted again, and then the locking force is kept; by means of the locking mechanism, the time for disassembling and installing the engine hood is greatly saved, the overall maintenance time is saved, and the maintenance efficiency is higher.
本发明涉及航空技术领域，特指一种用于飞机发动机罩的锁钩组件及其锁闭机构；一种用于飞机发动机罩的锁钩组件，包括：锁钩部件，用于与发动机罩上的锁点扣合和脱离，连杆部件，其一端与锁钩部件紧固连接，驱动该连杆部件的一端使锁钩部件与锁点扣合和脱离；锁钩部件和连杆部件之间设有长度调节组件，用于调节锁钩部件相对连杆部件的长度；还提供一种用于飞机发动机罩的锁闭机构，包括：上述的锁钩组件、手柄部件和联动组件，竖向扳动手柄部件时，联动组件用于带动连杆部件横向转动；锁点与锁钩部件的距离松动后，能够重新调节锁钩的距离，进而保持锁紧力；锁闭机构大大节省了拆开和安装发动机罩的时间，节省了整体检修时间，检修效率更高。
Lock hook assembly for aircraft engine hood and locking mechanism of lock hook assembly
The invention relates to the technical field of aviation, in particular to a lock hook assembly for an aircraft engine hood and a locking mechanism of the lock hook assembly. A lock hook assembly for an aircraft engine hood comprises a lock hook component used for being buckled with and separated from a lock point on the engine hood, and a connecting rod component with one end connected with the lock hook component in a fastened mode, and one end of the connecting rod component is driven to enable the lock hook component to be buckled with and separated from the lock point. A length adjusting assembly is arranged between the latch hook component and the connecting rod component and used for adjusting the length of the latch hook component relative to the connecting rod component. The invention further provides a locking mechanism for the aircraft engine hood, the locking mechanism comprises the lock hook assembly, a handle component and a linkage assembly, and when the handle component is pulled vertically, the linkage assembly is used for driving the connecting rod component to rotate transversely; after the distance between the lock point and the lock hook component is loosened, the distance of the lock hook can be adjusted again, and then the locking force is kept; by means of the locking mechanism, the time for disassembling and installing the engine hood is greatly saved, the overall maintenance time is saved, and the maintenance efficiency is higher.
本发明涉及航空技术领域，特指一种用于飞机发动机罩的锁钩组件及其锁闭机构；一种用于飞机发动机罩的锁钩组件，包括：锁钩部件，用于与发动机罩上的锁点扣合和脱离，连杆部件，其一端与锁钩部件紧固连接，驱动该连杆部件的一端使锁钩部件与锁点扣合和脱离；锁钩部件和连杆部件之间设有长度调节组件，用于调节锁钩部件相对连杆部件的长度；还提供一种用于飞机发动机罩的锁闭机构，包括：上述的锁钩组件、手柄部件和联动组件，竖向扳动手柄部件时，联动组件用于带动连杆部件横向转动；锁点与锁钩部件的距离松动后，能够重新调节锁钩的距离，进而保持锁紧力；锁闭机构大大节省了拆开和安装发动机罩的时间，节省了整体检修时间，检修效率更高。
Lock hook assembly for aircraft engine hood and locking mechanism of lock hook assembly
一种用于飞机发动机罩的锁钩组件及其锁闭机构
LE MEIJIAN (Autor:in) / LIU YIXIAO (Autor:in) / ZHUANG FENGKAI (Autor:in) / HE HUI (Autor:in)
11.06.2024
Patent
Elektronische Ressource
Chinesisch