Multi-joint measuring arm based digital measuring system and method for geometric characteristics of guided missile

A technology for measuring system and geometric characteristics, applied in ammunition, ammunition test, weapon accessories, etc., can solve the problems of low measurement efficiency, affecting production efficiency, and occupying a large number of personnel

Inactive Publication Date: 2019-06-28
SHANGHAI SPACE PRECISION MACHINERY RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] The purpose of the present invention is to provide a missile geometric characteristic measurement method based on a multi-joint measuring arm to solve the problems of low measurement efficiency, large occupation of personnel and influence on the overall production efficiency in the existing horizontal measurement

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  • Multi-joint measuring arm based digital measuring system and method for geometric characteristics of guided missile
  • Multi-joint measuring arm based digital measuring system and method for geometric characteristics of guided missile

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Embodiment Construction

[0029] A system and method for measuring geometric characteristics of a missile based on a multi-joint measuring arm proposed by the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. Advantages and features of the present invention will be apparent from the following description and claims. It should be noted that the drawings are all in a very simplified form and use imprecise ratios, which are only used to facilitate and clearly assist the purpose of illustrating the embodiments of the present invention.

[0030] Such as Figure 1~2 As shown, the embodiment of the present invention provides a kind of missile geometric characteristic measurement system based on multi-joint measuring arm, comprises data acquisition and processing system 1, measurement support 2, multi-joint measurement arm 3 and supporting platform 4; Data acquisition and processing system 1 is composed of computer , data line a...

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Abstract

The invention provides a multi-joint measuring arm based digital measuring system and method for geometric characteristics of a guided missile. The measuring system comprises a guided missile supporting platform, a multi-joint measuring arm, measuring brackets and a data acquiring processing system, wherein the guided missile supporting platform is a platform capable of providing all missile support, so that the missile is guaranteed to meet requirements of a measuring state; the multi-joint measuring arm is a market mature product, has arm length greater than 3.5 meters, has measuring precision not smaller than 0.5 mm, and is used for acquiring coordinate values of each measuring point on the missile body; the measuring brackets are supporting structures of the multi-joint measuring arm,are fixedly arranged on the supporting platform, and are arranged front and rear separately; and the data acquiring system consists of a computer, a data line and data processing software, and is usedfor acquiring and processing the measured data of the measuring arm to form a measured report form. According to the multi-joint measuring arm based digital measuring system and the method provided by the invention, process flow is optimized, digital measuring is realized, and turnover, among stations, of the guided missile is reduced while efficiency is improved.

Description

technical field [0001] The invention relates to the field of missile assembly, in particular to a system and method for digitally measuring missile geometric characteristics based on a multi-joint measuring arm. Background technique [0002] Missile assembly is an important production process of missile products. It is the whole process of assembling the parts, parts and components of each subsystem into a complete missile, and verifying its performance through testing and testing to ensure that its performance meets the factory state. The final assembly is a general inspection of the previous manufacturing quality and the performance of each subsystem, and a comprehensive verification of the coordination and reliability of the connection parts and subsystems. At the same time, it plays a vital role in the quality and production cycle control of the missile. . [0003] Full-body assembly and quality characteristic measurement are key links in the final assembly process. Th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B35/02
Inventor 王磊毛旦平
Owner SHANGHAI SPACE PRECISION MACHINERY RES INST
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