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Rapid docking mechanism for target stimulator bow cap and seeker

A target simulator and docking mechanism technology, applied in metal processing, metal processing equipment, manufacturing tools, etc., can solve problems such as damage to the seeker, inability to achieve rapid installation, potential safety hazards, etc., to achieve accurate docking, convenient and fast docking, The effect of high safety factor

Inactive Publication Date: 2013-09-11
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantage of this installation method is that it takes a long time to install and requires the cooperation of multiple people. At the same time, it will bring the risk of possible damage to the seeker. It cannot be installed quickly and there is a huge potential safety hazard.

Method used

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  • Rapid docking mechanism for target stimulator bow cap and seeker
  • Rapid docking mechanism for target stimulator bow cap and seeker

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0014] Example: see figure 1 , figure 2 .

[0015] A fast docking mechanism for a target simulator head cover and a seeker, including a lift car 1, the lift platform 2 of the lift car 1 is controlled by a hydraulic lift mechanism, and the target simulator head cover 3 is arranged on the lift of the hydraulic lift mechanism. On the platform 2, the lift car 1 is provided with a push rod 4.

[0016] The rise of the hydraulic lifting mechanism is controlled by the ascending pedal 5, and the descending is controlled by the descending hydraulic switch 6. The ascending pedal 5 and the descending hydraulic switch 6 control the hydraulic system to drive the hydraulic lifting mechanism to drive the lifting platform up and down, which is a common technology in the prior art The means are not described here.

[0017] The target simulator head cover 3 is firmly connected with the two-dimensional micro-adjustment device and adjusted by the two-dimensional micro-adjustment device 7 ....

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Abstract

The invention relates to the technical field of design of accessory structures of missile seekers, in particular to a rapid docking mechanism for a target stimulator bow cap and a seeker. The rapid docking mechanism for the target stimulator bow cap and the seeker comprises a lifting trolley, wherein lifting and descending of a lifting platform of the lifting trolley are controlled by a hydraulic lifting mechanism, the target stimulator bow cap is arranged on a lifting platform of the hydraulic lifting mechanism, and a push rod is arranged on the lifting trolley. According to the rapid docking mechanism for the target stimulator bow cap and the seeker, docking between the target stimulator bow cap and the seeker is convenient and rapid, and can be achieved in a quite short time, operation carried out by a plurality of persons is not needed, accurate docking is achieved through the lifting trolley with the hydraulic lifting mechanism and a two-dimensional micro-adjustment device, and the security coefficient is high.

Description

technical field [0001] The invention relates to the technical field of missile seeker auxiliary structure design, in particular to a rapid docking mechanism for a target simulator head cover and a seeker. Background technique [0002] The target simulator hood is used to provide simulated target images in conjunction with the qualitative or quantitative detection of the seeker. When using it, the target simulator hood needs to be docked with the seeker. The early installation method of the target simulator head cover is to fix the fastening mechanism of the head cover on the seeker first, and then install the alignment mechanism, and fix the alignment mechanism by rotating the handwheel on the fastening mechanism, and then align The pressure ring on the mechanism is tightened, and after the alignment mechanism is fixed, a person needs to lift the target simulator hood and slowly move closer to the alignment mechanism. Care must be taken during the approaching process to avoi...

Claims

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Application Information

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IPC IPC(8): B23P19/10
Inventor 陈涛张洪宇刘永安张成标金敏喻芳冯燕袁欢欢罗海鹰鞠新星
Owner JIANGXI HONGDU AVIATION IND GRP
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