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Numerical control machine tool data management system and method

A technology of data management system and CNC machine tool, applied in general control system, control/adjustment system, program control, etc., can solve the problems of poor precision and stability, improve production efficiency, avoid error superposition, and automatically compensate for thermal deformation Effect

Pending Publication Date: 2021-07-16
AECC COMML AIRCRAFT ENGINE CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved by the present invention is to provide a CNC machine tool data management system and method, which can overcome the problems of poor precision and stability of domestic CNC machine tools

Method used

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  • Numerical control machine tool data management system and method
  • Numerical control machine tool data management system and method
  • Numerical control machine tool data management system and method

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Embodiment Construction

[0030] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the following briefly introduces the drawings that need to be used in the description of the embodiments. Obviously, the accompanying drawings in the following description are only some examples or embodiments of the present application, and those skilled in the art can also apply the present application to other similar scenarios. Unless otherwise apparent from context or otherwise indicated, like reference numerals in the figures represent like structures or operations.

[0031] As indicated in this application and claims, the terms "a", "an", "an" and / or "the" do not refer to the singular and may include the plural unless the context clearly indicates an exception. Generally speaking, the terms "comprising" and "comprising" only suggest the inclusion of clearly identified steps and elements, and these steps and elements do not constitute an exclusive list, and ...

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Abstract

The invention provides a numerical control machine tool data management method. The method comprises the steps of collecting a real-time detection result of a workpiece machining process of a numerical control machine tool; performing quality evaluation on the machined workpiece to obtain quality evaluation information of the workpiece; inputting a real-time detection result and a quality evaluation information into a numerical control machine tool model, and analyzing the form and location tolerance and the surface roughness of the workpiece to obtain a workpiece error; adjusting operating parameters, dynamic precision and cutter parameters in a digital control program of the numerical control machine tool according to the workpiece errors; and enabling the numerical control machine tool to carry out secondary machining on the surface with the workpiece error so as to compensate the workpiece error.

Description

technical field [0001] The present invention mainly relates to the field of numerical control machine tool manufacturing, in particular to a numerical control machine tool data management system and method. Background technique [0002] High bypass ratio turbofan aeroengine is the main driving force of civil aviation technology. It must strictly abide by the airworthiness requirements of civil aviation in all aspects of product design, testing and production. Its main key components such as fan blades, turbine discs, and overall blades The processing quality requirements of discs, casings, etc. are extremely strict. Therefore, the CNC machining machine tools for its components must also meet the requirements of high precision, high performance, and high stability. At present, domestic high-end CNC machine tools still have a big gap with the CNC processing equipment in Europe and the United States in terms of their own geometric accuracy, position accuracy, thermal stability...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/4065
CPCG05B19/4065
Inventor 王智勇陈亚林
Owner AECC COMML AIRCRAFT ENGINE CO LTD
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