A numerical control machining method for super-large complex thin-walled parts of titanium alloy

A technology of thin-walled parts and processing methods, applied in metal processing equipment, metal processing machinery parts, manufacturing tools, etc., can solve problems such as surface springback, increased processing difficulty, and complex overall structure of parts, so as to control the deformation of parts , Great reference, the effect of high-quality and efficient processing

Active Publication Date: 2021-03-19
SHENYANG AIRCRAFT CORP
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Problems solved by technology

Therefore, the overall structure of the part becomes complex, and the processing difficulty increases accordingly.
At the same time, the part itself is made of titanium alloy, which is a difficult-to-machine metal. Due to factors such as large cutting force, high milling heat, and surface springback during processing, the processing efficiency is low and the product quality is unstable.

Method used

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  • A numerical control machining method for super-large complex thin-walled parts of titanium alloy
  • A numerical control machining method for super-large complex thin-walled parts of titanium alloy
  • A numerical control machining method for super-large complex thin-walled parts of titanium alloy

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[0074] The specific implementation manners of the present invention will be further described below in conjunction with the accompanying drawings and technical solutions.

[0075] It should be understood that the appended drawings are not to scale, presenting a suitably simplified representation of various features illustrative of the basic principles of the invention. The specific design features of the invention disclosed herein, including, for example, specific dimensions, orientations, locations and shapes will be determined in part by the particular intended application and use environment.

[0076] In the accompanying figures, the same or equivalent parts (elements) are designated with the same reference numerals.

[0077] In the description of the present invention, it should be noted that the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", " The orientations or positional relationships indicated by "vertical", "horizon...

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Abstract

The invention provides a numerical control processing method for titanium alloy ultra-large and complex thin-walled parts, which includes the following steps: using a clamp with adjustable support and a modular flexible vacuum clamp of a numerical control machine tool to realize the positioning and clamping of the front and back sides of the part ;A stress-free clamping method for super-large parts is adopted to ensure that there is no clamping stress during the clamping process of the parts; according to the principle of datum coincidence, the establishment of the processing coordinate system is realized by using the automatic online detection function attached to the equipment; The sequence, milling method, cutting amount, etc., formulate the process flow of rough machining, semi-finishing, and finishing; use the equipment's own online detection function to automatically detect the machining accuracy and process compliance of the parts. The method proposed by the invention can realize high-quality and high-efficiency machining of ultra-large thin-walled parts, and effectively controls the deformation of the parts and the out-of-tolerance of geometric dimensions caused by human factors.

Description

technical field [0001] The invention belongs to the technical field of mechanical processing, and in particular relates to a numerical control processing method for ultra-large and complex thin-walled titanium alloy parts. Background technique [0002] In order to improve the performance of the aircraft, the overall design and thin-wall design tend to be widely used for large parts on the aircraft, and the processing and assembly precision is high. Therefore, the overall structure of the part becomes complicated, and the processing difficulty increases accordingly. At the same time, the part itself is made of titanium alloy, which is a difficult-to-machine metal. Due to factors such as large cutting force, high milling heat, and surface springback during processing, the processing efficiency is low and the product quality is unstable. In this way, there are higher requirements for the overall processing methods such as the selection of process equipment, parts clamping, arr...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23C3/00B23Q3/06
CPCB23C3/00B23Q3/065
Inventor 李晓亮齐东昱林海鹏刘驰
Owner SHENYANG AIRCRAFT CORP
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