Cabin door latching mechanism

A technology for door latches and hatches, which is applied in building locks, building structures, construction, etc., can solve the problems of different forms, weights, costs, and reliability, difficult to meet actual needs, and complex structures, and achieve light weight, The effect of ingenious structure and simple latch mechanism

Active Publication Date: 2020-01-17
中航通飞华南飞机工业有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the different functions and forms of the cabin doors, the existing cabin door latch mechanisms are designed in different forms, weights, costs and reliability, especially nowadays, the aircraft cabin door latch mechanisms generally have the problems of complex structure and heavy weight, which are becoming more and more difficult to meet actual needs

Method used

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  • Cabin door latching mechanism
  • Cabin door latching mechanism
  • Cabin door latching mechanism

Examples

Experimental program
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Effect test

Embodiment Construction

[0031] Provided following embodiment in conjunction with accompanying drawing:

[0032] Please also see figure 1 , figure 2 , image 3 , Figure 4 , Figure 7 , the door latch mechanism of the present invention is located on the door frame and includes a rocker arm assembly 1 , a lock 2 , a bolt 3 and a connecting rod 4 . Among them, the rocker arm assembly 1 is connected with the driving source of the mechanism, the rocker arm assembly 1 rotates around the axis a5, the latch 3 can rotate around the axis b7, and the lock 2 can rotate around the axis c6, and the three axes are parallel to each other and distributed in a triangle.

[0033] see figure 1 , figure 2 , image 3 As shown, the rocker arm assembly 1 and the latch 3 are connected by a connecting rod 4, and the intersection point D of the rocker arm assembly 1 and the connecting rod 4 adopts an over-center design, that is, the intersection point D passes through the connecting line AE during the movement to reac...

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PUM

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Abstract

The invention relates to the field of cabin door design, and particularly discloses a cabin door latching mechanism. The cabin door latching mechanism is located on a cabin door frame and comprises arocker arm assembly, a lock, a latch and a connecting rod, the rocker arm assembly is connected to a driving source, the rocker arm assembly, the lock and the latch can rotate around the self axis, and the three axes are parallel to one another and distributed in a triangular mode. According to the cabin door latching mechanism, the rocker arm assembly and the lock adopt clearance fit so as to achieve the purpose of driving the lock and maintain the position of the lock after complete opening, meanwhile, the possibility of mislocking is avoided, the driving source and the limiting device of the lock are omitted accordingly, the weight is reduced, and the system is simplified; and the rocker arm assembly drives the latch through the connecting rod, the point of intersection connected to oneend of the rocker arm assembly adopts over-center design, the point of intersection connected to one end of the latch adopts non-over-center design, the purpose of noninterference with the lock during unlatching and latching is achieved, meanwhile, the fact that the lock locks the position of the latch can be ensured, therefore, the entire latching mechanism is simple in structure, light in weight, and high in reliability, the connecting rod and the rocker arm assembly adopt adjustable design, and assembling and adjusting are facilitated.

Description

technical field [0001] The invention belongs to the field of hatch design, in particular to a hatch latch mechanism. [0002] technical background [0003] In the process of modern structural design, hatch doors have been widely used. Hatch doors are divided into hazard doors and non-hazard doors. The hazard door locking mechanism requires higher reliability and generally needs to be designed as a latch mechanism. The function of the latch is to maintain the position of the hatch, and the function of the lock is to maintain the position of the bolt. Due to the different functions and forms of the cabin doors, the existing cabin door latch mechanisms are designed in different forms, weights, costs and reliability. Especially now, aircraft cabin door latch mechanisms generally have complex structures and heavy weights, which are increasingly difficult to meet. actual needs. Contents of the invention [0004] The purpose of the present invention is to provide a hatch door la...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): E05B15/00E05B15/10E05B65/00
CPCE05B15/00E05B15/0053E05B15/10E05B65/00
Inventor 谷刚张浩戴赛丰
Owner 中航通飞华南飞机工业有限公司
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