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A numerical control finish turning method for annular ω groove of titanium alloy thin-walled disk ring

A processing method and technology of thin-walled discs, which are applied in metal processing equipment, workpieces, turning equipment, etc., can solve the problems of not meeting the size and technical requirements of parts, affecting the processing efficiency and processing quality of parts, and difficult to guarantee the size and technical conditions. , to achieve the effect of solving the technical requirements of processing accuracy and efficient processing, solving the low processing efficiency, and improving the research and production efficiency

Inactive Publication Date: 2016-08-24
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Application Information

AI Technical Summary

Problems solved by technology

The structure of the part is complex, and the CNC machining route and method will directly affect the processing efficiency and quality of the part. Therefore, whether the size and technical conditions can meet the requirements of the design drawings, the CNC machining tool routing, that is, the processing concept plays a vital role.
[0003] At the present stage, the production site generally adopts the contour mode trial cutting method for processing. This kind of NC program is more flexible in processing, and the contour points and the position of the advance and retreat tools can be adjusted and modified at will, but it requires high-tech operators with processing experience to complete the development and processing. , otherwise some dimensions and technical conditions are difficult to guarantee
During the processing, the operator groped for tool compensation based on his own processing experience. The material of this part is titanium alloy, which is a difficult-to-machine material, and the characteristics of the part are not easy to form. If the processing is not in place, additional processing is required. The cutting force is relatively large, which may not meet the size and technical requirements of the part

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  • A numerical control finish turning method for annular ω groove of titanium alloy thin-walled disk ring
  • A numerical control finish turning method for annular ω groove of titanium alloy thin-walled disk ring
  • A numerical control finish turning method for annular ω groove of titanium alloy thin-walled disk ring

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Embodiment Construction

[0031] The specific implementation manners of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0032] The turning process of the annular Ω groove of the titanium alloy thin-walled disc ring is divided into three processes: rough turning, semi-finishing turning and finishing turning, and the finishing turning process of the annular Ω groove of the titanium alloy thin-walled disc ring is divided into rough machining and semi-finishing There are three stages of finishing and finishing. This embodiment is aimed at the numerical control finishing machining of the annular Ω groove of the titanium alloy thin-walled disk ring, and implements the method on the numerical control vertical lathe.

[0033] A kind of numerical control finish turning processing method of annular Ω groove of titanium alloy thin-walled disk ring, Figure 6 shown, including the following steps:

[0034] Step 1: Determine the margin of each processing stag...

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Abstract

The invention provides a numerical control finish turning processing method of an annular Omega-shaped groove of a titanium alloy thin wall disc ring piece. The numerical control finish turning processing method of the annular Omega-shaped groove of the titanium alloy thin wall disc ring piece includes: confirming an allowance in each finish turning processing stage of the annular Omega-shaped groove of the titanium alloy thin wall disc ring piece; confirming a processing scheme of the finish turning stages of the annular Omega-shaped groove of the titanium alloy large diameter thin wall disc ring piece; compiling a numerical control turning program of the finish turning stages of the annular Omega-shaped groove of the titanium alloy large diameter thin wall disc ring piece; controlling a processing route of each numerical control finish turning processing stage of the annular Omega-shaped groove of the titanium alloy thin wall disc ring piece. The numerical control finish turning processing method of the annular Omega-shaped groove of the titanium alloy thin wall disc ring piece breaks a technical bottleneck in processing of a titanium alloy piece of special structure, improves processing efficiency on the premise of meeting processing technology requirements of the annular Omega-shaped groove of the titanium alloy large diameter thin wall disc ring piece in numerical control turning of a titanium alloy material supercharging first stage disc, achieves high efficiency processing of the annular Omega-shaped groove of the titanium alloy large diameter thin wall disc ring piece, solves the problems that the annular Omega-shaped groove of the titanium alloy large diameter thin wall disc ring piece is low in processing efficiency and long in machine occupying time, and alleviates production bottlenecks in machining of a vertical lathe.

Description

technical field [0001] The invention relates to the technical field of mechanical numerical control machining, in particular to a numerical control finishing machining method for an annular Ω groove of a titanium alloy thin-walled disk ring. Background technique [0002] In the field of mechanical processing technology, especially in titanium alloy processing and manufacturing, the processing of titanium alloy disc parts and the annular Ω groove of large-diameter and thin-walled parts is a major technical difficulty. Conditions, low work efficiency and machining accuracy are difficult to meet the requirements of parts and production. Such parts generally appear in advanced models. The efficiency of their development and processing is extremely low and the repair rate is high. Controlling deformation is also a major difficulty. Due to the limitation of on-site production conditions, general disk parts are processed on the CNC horizontal lathe, and there are certain deformati...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23B7/12
CPCB23B1/00B23B2215/64B23B2220/126B23B2220/24
Inventor 于洁史前凯闫峰杨洋郭涛
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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