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Method for optimally sorting aircraft structural part automatic programming processing units based on technological process

A technology for aircraft structural parts and processing units, applied in the direction of electrical program control, digital control, etc., can solve problems such as long paths, combined explosions, and low efficiency of manual sequencing

Active Publication Date: 2014-08-27
SHENYANG AIRCRAFT CORP
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AI Technical Summary

Problems solved by technology

[0003] In order to solve the above-mentioned existing technical problems, the present invention provides a process-based automatic programming and processing unit optimization and sorting method for aircraft structural parts. Inefficiency, long paths, and combined explosion problems in automatic programming process decision-making make the processing sequence process meet the actual processing process requirements, and significantly reduce the time of empty cutting and improve the processing efficiency of parts

Method used

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  • Method for optimally sorting aircraft structural part automatic programming processing units based on technological process
  • Method for optimally sorting aircraft structural part automatic programming processing units based on technological process
  • Method for optimally sorting aircraft structural part automatic programming processing units based on technological process

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Embodiment Construction

[0029] The invention is based on the CAD / CAM system platform and realizes a method for optimizing and sorting automatic programming and processing units of aircraft structural parts.

[0030] The embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. This embodiment is implemented on the premise of the technical solution of the invention, and detailed implementation methods and specific implementation processes are provided, but the protection scope of the present invention is not limited to The following implementation examples.

[0031] The detailed steps of the automatic programming and processing unit optimization sorting implementation of the aircraft structural parts based on the technological process proposed by the present invention are as follows:

[0032] Step 1): process construction. Input the process plan file, the plan is stored in xml, in the form of a tree structure, deeply traverse the process pla...

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Abstract

The invention provides a method for optimally sorting aircraft structural part automatic programming processing units based on a technological process. The method comprises the steps that the technological process is built, and the machining craft process of parts is built through the tree structure of the depth traversal process scheme according to an input technological scheme file; the machining units are grouped, a set of tool sequences is obtained according to a given technological scheme, the grouping rule of the machining units is built according to the machining units, target machining units and real-time make-up machining units with tools associated in the tool sequences, and the special requirements of different types of make-up machining units and technologies, and the machining units are divided into four groups; the machining units are sorted, an overall layering and a virtual layering method are adopted, rough machining deformation is reduced, and layered machining and sorting are achieved. According to the method, the sorting result conforms to the practical technological requirement, interference and excessive cutting in the machining process are effectively reduced, the machining path is short, and the machining efficiency is high.

Description

technical field [0001] The invention relates to a process-based automatic programming and processing unit optimization and sequencing method for aircraft structural parts, which is used for automatic optimization and sequencing of processing units in the numerical control programming of aircraft structural parts, and belongs to the technical field of aircraft digital manufacturing. By applying this method, the optimal sorting of processing units can be realized. The sorting results are highly in line with the process requirements and the processing paths are reduced, which improves the design efficiency and quality of NC machining of aircraft structural parts, thereby shortening the aircraft development cycle. Background technique [0002] The rapid development and wide application of numerical control related technologies such as computers, programming, and high-speed machining have promoted the development of aircraft structural parts manufacturing technology. Modern aircra...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/19
Inventor 陈树林杜宝瑞周敏赵璐王芳李文强
Owner SHENYANG AIRCRAFT CORP
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