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Web notch structure machining structure

A processing method and notch technology, applied in the field of metal cutting and CNC machining of aerospace structural parts, can solve the problems of high level of fitter, difficult to guarantee accuracy, poor stiffness of the web, etc., to reduce workload and quality risks, Eliminates the effect of snapping knife broach and improving stability

Active Publication Date: 2019-11-22
CHENGDU AIRCRAFT INDUSTRY GROUP
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, there are three disadvantages in this processing: first, removing the boss will generate more fitter workload, which affects the processing efficiency of the part; second, although the rigidity of the part is guaranteed in the CNC process, it will pass the difficulty Fitter, when the fitter is grinding, the stiffness of the web is still poor, and the knife is easy to bounce during grinding, which requires a high level of fitter; third, the end face depends on the fitter to ensure the size and shape tolerance, and its accuracy is difficult to guarantee
In actual production, there are cases where parts are out of tolerance or even scrapped due to the fitter’s mistake in grinding the web notch

Method used

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Embodiment Construction

[0015] In order to understand the present invention more clearly, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0016] The invention provides a method for processing a web notch structure, which includes retaining a process boss above the notch whose size has been processed in place, and the boundary of the process boss in the width direction of the notch exceeds the notch boundary by more than 0.5mm until the web After all other features of the part are processed in place, the process boss is removed.

[0017] Wherein, removing the process boss includes first milling the process boss thin (that is, removing part of the volume of the process boss), until the effective connection depth between the process boss and the notch in the depth direction of the notch is 1 to 2 mm, After milling the process boss, reduce the feed speed to one-third of the original, mill the process boss, and lift the tool ...

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Abstract

The invention discloses a web notch structure machining structure. The web notch structure machining structure comprises the following steps: reserving a process boss above a notch of which the size is machined in place, wherein the boundary, in the width direction of the notch, of the process boss exceeds over 0.5 mm of the boundary of the notch; and removing the process boss until other characteristics of a web component are all machined in place. By utilizing the machining method disclosed by the invention, the notch structure can be subjected to numerical control machining stably; only a residue of 0.05 mm is remained at the edge of the notch; a bench worker only needs to do the work approximating polishing; the polishing amount is small; and a cutter is not easily rebounded in a benchworking process.

Description

technical field [0001] The invention relates to the field of metal cutting processing, in particular to the field of numerical control processing of aeronautical structural parts, and in particular to a method for processing a web notch structure. Background technique [0002] Aeronautical structural parts often have a web structure with a notch due to assembly requirements. However, when this web structure is CNC-machined, at the end position of the notch (such as figure 1 As shown), it is easy to cause the knife to be broached, resulting in parts quality problems. [0003] Traditional numerical control methods for such web structures such as figure 2 As shown, the web 1 of the part and the process boss 3 are connected by a sheet connection 2, and the process boss is pressed tightly during processing to ensure the rigidity of the structure with notches during processing, and then the process boss is removed by a fitter. And sand the edges in place. However, there are th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23P15/00
CPCB23P15/00
Inventor 刘翘楚王元军邓乙凡吴国伟杨玲牛印
Owner CHENGDU AIRCRAFT INDUSTRY GROUP