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Mechanical spring lock of helicopter control cabinet

A technology for control cabinets and helicopters, applied to cylinder locks, locks with turning keys, building locks, etc., can solve the problems of lengthening maintenance and repair cycles, increasing keys, and difficult management, so as to save production cycle and save development cost, ease of operation

Inactive Publication Date: 2014-02-26
HEFEI UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The principle is similar to that of ordinary tumbler locks, but the structural strength has been improved. The advantages are high reliability, simple maintenance and repair, and no external input is required. The disadvantage is that in order to ensure the safety of the helicopter and the pilot, each helicopter control cabinet Lock cylinders are different, and maintenance personnel must match a key for each helicopter. In this way, the number of keys provided by maintenance personnel will increase with the number of helicopters, making management more difficult and indirectly lengthening the maintenance cycle.

Method used

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  • Mechanical spring lock of helicopter control cabinet
  • Mechanical spring lock of helicopter control cabinet
  • Mechanical spring lock of helicopter control cabinet

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0075] see Figure 6 , the driver inserts the key 18 into the flat square long counterbore of the inner lock core 3, the arc edge of the front section is in axial contact with the ejector rod 9, and the ejector rod double-headed key 20 of the ejector rod 9 is connected to the inner lock core 3 In the inner lock core double key hole 22. The bottom edge of five pairs of grooves on both sides of the front section of the driver's key 18 is respectively in contact with one end face of five pairs of inner layer pins 4 of the inner lock core 3, and the other end face of the five pairs of inner layer pins 4 is respectively in contact with the middle layer lock. One end face of the five pairs of pins 5 in the middle layer of the core 2 is in contact with the upper and lower busbars of the cylinder of the inner lock core 3, and the radial connection between the cylinder of the inner lock core 3 and the oblong counterbore of the middle lock core 2 completely disengaged. And or middle l...

Embodiment 2

[0079] see Figure 7 , the maintenance personnel inserts the key 19 into the flat square long counterbore of the inner lock cylinder 3, and the arc-shaped raised edge of the front section pushes the ejector rod 9 to move axially, so that the compression spring 15 at the rear end of the ejector rod 9 is compressed, and the ejector rod The push rod double key 20 of 9 breaks away from the inner lock core double key hole 22 of the inner lock core 3 and is keyed in the middle layer lock core double key hole 23 of the middle layer lock core 2 . The five pairs of groove bottoms on both sides of the front section of the key 19 are used by maintenance personnel to contact with one end faces of the five pairs of inner layer pins 4 of the inner lock core 3 respectively, and the other end faces of the five pairs of inner pins 4 are respectively in contact with the middle layer lock. One end faces of the five pairs of middle layer pins 5 of the core 2 are correspondingly in contact with ea...

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Abstract

The invention relates to a mechanical spring lock of a helicopter control cabinet. The mechanical spring lock comprises an outer lock core, a middle lock core, an inner lock core, a mandrel, a cam driving lever and a spring bolt, wherein the inner lock core and the middle lock core are arranged inside the outer lock core; outer, middle and inner layers of spring pieces are correspondingly arranged inside the inner lock core, the middle lock core and the outer lock core; the cam driving lever is connected with and arranged inside the spring bolt through the mandrel. The inner lock core rotates, the middle lock core and the outer lock core are fixed, and the spring bolt pops out when a key of a driver is inserted and rotated, and a lock is converted into an unlocked state from a locked state; the inner lock core and the middle lock core simultaneously rotate, and the outer lock core is fixed when a key of a maintainer is inserted and rotated, so that the lock is converted into the unlocked state from the locked state. The mechanical spring lock has the characteristics that with a three-layer nested structure, the lock of each control cabinet corresponds to one key of the driver while locks of all control cabinets can be unlocked by the maintainer with one key due to different lengths of the inner, middle and outer layers of spring pieces, so that the lock is easy to operate and convenient to manage.

Description

technical field [0001] The invention relates to a mechanical pin lock device, in particular to a mechanical pin lock for a helicopter control cabinet. Background technique [0002] As the packaging platform of the helicopter control system, the helicopter control cabinet is packaged with the electrical control system, communication system, remote sensing monitoring system, internal sensor monitoring system and alarm system, etc. To protect checkpoints, in order to prevent man-made intentional damage or unconscious misoperation, the control cabinets of helicopters are equipped with safety locks. In this way, for the use and maintenance of the helicopter, both the helicopter pilot and the maintenance personnel must be equipped with the key or password of the control cabinet. [0003] At present, the locks used in the control cabinet of the helicopter are mainly in the following ways: [0004] 1. Electronic lock. Including digital combination locks, induction combination loc...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): E05B27/00E05B65/52E05B15/00
Inventor 黄康周志红赵韩刘鹏熊杨寿
Owner HEFEI UNIV OF TECH
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