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Part assembly out-of-tolerance analysis method and device, equipment and storage medium

A technology of parts assembly and analysis methods, applied in design optimization/simulation, word processing, resources, etc., can solve the problems of low efficiency of parts out-of-tolerance acquisition, out-of-tolerance parts assembly, etc.

Pending Publication Date: 2022-01-28
CHENGDU AIRCRAFT INDUSTRY GROUP
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Problems solved by technology

[0004] The main purpose of the present invention is to provide an analysis method, device, equipment and storage medium for parts assembly out-of-tolerance, aiming to solve the problem of low efficiency in obtaining parts out-of-tolerance by adopting the existing method for obtaining part out-of-tolerance in the prior art technical problem

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  • Part assembly out-of-tolerance analysis method and device, equipment and storage medium
  • Part assembly out-of-tolerance analysis method and device, equipment and storage medium
  • Part assembly out-of-tolerance analysis method and device, equipment and storage medium

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Embodiment Construction

[0042] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0043] refer to figure 1 , figure 1 It is a schematic diagram of the electronic device structure of the hardware operating environment involved in the solution of the embodiment of the present invention.

[0044] Such as figure 1 As shown, the computer device may include: a processor 1001 , such as a central processing unit (Central Processing Unit, CPU), a communication bus 1002 , a user interface 1003 , a network interface 1004 , and a memory 1005...

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Abstract

The invention discloses a part assembly out-of-tolerance analysis method and device, equipment and a storage medium, and is used for electronic equipment, and the method comprises the following steps: determining a plurality of to-be-measured points and a plurality of measurement reference surfaces of the to-be-measured points in a target assembly part; obtaining the minimum distance between each point to be measured and the reference surface; determining a comparison result of each minimum distance and a preset tolerance interval; and based on the plurality of comparison results, obtaining out-of-tolerance analysis results of the plurality of points to be measured. The invention further discloses a part assembly out-of-tolerance analysis device, electronic equipment and a computer readable storage medium. According to the method, the minimum distance and data copying do not need to be obtained manually, the out-of-tolerance analysis time is greatly shortened, and the out-of-tolerance analysis efficiency is improved.

Description

technical field [0001] The invention relates to the technical field of part assembly analysis, in particular to an analysis method, device, equipment and storage medium for part assembly out-of-tolerance. Background technique [0002] At present, in the field of aircraft component assembly, laser trackers are often used to measure the actual spatial position information of parts, thereby generating a large amount of measurement data. In order to compare the actual situation of parts manufacturing and assembly, it is necessary to measure the tolerance of parts. At present, it is necessary to import the measurement data of the part into the measurement software, assemble and compare it with the theoretical digital model of the part, and form a digital model file of the measurement assembly. In specific applications, the actual out-of-tolerance information in different areas of the part is usually manually measured point by point using the measurement tool of the measurement so...

Claims

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Application Information

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IPC IPC(8): G06Q10/06G06F30/10G06F30/20G06F40/18
CPCG06Q10/0639G06F30/20G06F30/10G06F40/18
Inventor 赵颖丁海涛邓珍波
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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