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Corner numerical control processing automatic programming method for aircraft complicated structural component

A complex structure, automatic programming technology, applied in computer control, general control system, program control and other directions, can solve the problems of lack of machining plan and effective optimization of machining parameters, large workload, low quality of programming, etc. The effect of optimizing processing parameters, improving efficiency and quality, and shortening the development cycle

Inactive Publication Date: 2015-11-04
BEIHANG UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] (1) The process regulations are cumbersome, the workload is heavy, and the time is long;
[0006] (2) The quality of the program depends on the experience and level of the technicians, resulting in low or unstable programming quality;
[0007] (3) It is difficult to effectively inherit excellent experience and expert knowledge;
[0008] (4) Lack of effective optimization of processing schemes and processing parameters

Method used

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  • Corner numerical control processing automatic programming method for aircraft complicated structural component
  • Corner numerical control processing automatic programming method for aircraft complicated structural component
  • Corner numerical control processing automatic programming method for aircraft complicated structural component

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Embodiment Construction

[0035] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some 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 making creative efforts belong to the protection scope of the present invention.

[0036] The invention will be further described in detail below in conjunction with the accompanying drawings, as the appended figure 1 Shown is the interactive operation parameter input interface described in the embodiment of the present invention, wherein "select program node" is the preparation work for workpiece processing, "select continuous corner" and "select discontinuous multi-corner" are to select the type of corner to be processed, and fi...

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Abstract

The invention discloses a corner numerical control processing automatic programming method for an aircraft complicated structural component, which comprises the steps of 1) side steering plane calculation; 2) cutting element calculation; 3) interference domain construction; 4) residual domain calculation; and 5) processing unit construction. Therefore, automatic programming of a corner processing numerical control program can be realized. According to the corner numerical control processing automatic programming method, the programming personnel need not to carry out tedious interactive operations or complicated geometric parameter calculation, programming for the corner processing numerical control program can be completed by only interactively selecting any one corner plane, and problems of low or unstable program quality and the like caused by a practice that technicists carry out programming interactively in a mode of relying on experience are effectively avoided. The corner numerical control processing automatic programming method can significantly improve the efficiency and the quality of corner processing, shorten the product development period and improve the market competitiveness of products.

Description

technical field [0001] The invention relates to the field of numerical control machining and manufacturing of aircraft complex structural parts in aviation manufacturing, in particular, an automatic programming method for corner numerical control machining of aircraft complex structural parts. Background technique [0002] In modern aircraft design, in order to meet the requirements of high performance, integral structural parts with superior performance are widely used, such as integral structures such as wall panels, beams, frames and wing ribs. In order to meet the structural weight design requirements, there are a large number of cavity structures in the overall structural part. The corner is an important sub-feature of the cavity structure, and its processing efficiency and quality directly affect the processing efficiency and quality of the part. The overall structural parts have the characteristics of complex structure, high processing precision requirements, and high...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/4093
CPCG05B19/4093
Inventor 郑国磊崔志伟石叶楠周敏陈树林王勃
Owner BEIHANG UNIV
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