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Anti-fatigue efficient milling parameter optimization control method for titanium alloy thin-wall component

A thin-walled component, optimized control technology, applied in the direction of electrical digital data processing, special data processing applications, instruments, etc., can solve the problems of poor surface integrity characteristics, low material removal rate, etc., to achieve good residual stress and improve material removal , to meet the effect of high reliability and long life

Inactive Publication Date: 2018-09-21
NORTHWESTERN POLYTECHNICAL UNIV
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Problems solved by technology

[0004] The purpose of the present invention is to provide a fatigue-resistant high-efficiency milling parameter optimization control method for titanium alloy thin-walled components to solve the problems of poor surface integrity characteristics and low material removal rate in the milling process of titanium alloy thin-walled components

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  • Anti-fatigue efficient milling parameter optimization control method for titanium alloy thin-wall component
  • Anti-fatigue efficient milling parameter optimization control method for titanium alloy thin-wall component
  • Anti-fatigue efficient milling parameter optimization control method for titanium alloy thin-wall component

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Embodiment Construction

[0044] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0045] The invention discloses a fatigue-resistant high-efficiency milling parameter optimization control method for titanium alloy thin-walled components, which specifically includes the following steps:

[0046] Step 1. Establish the primary selection milling process parameter domain of titanium alloy thin-walled components, and conduct an orthogonal test to measure the surface integrity parameters of the test components, and establish the relationship between the milling process parameters and surface integrity characteristics of titanium alloy thin-walled components, specifically Methods as below:

[0047] Step 1.1. Determine the primary milling process parameter domain for titanium alloy thin-walled components.

[0048] In this embodiment, Ti1023 titanium alloy is selected, and the surface integrity milling process parameter domain C is f...

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Abstract

The invention discloses an anti-fatigue efficient milling parameter optimization control method for a titanium alloy thin-wall component. The method comprises the following steps that: establishing the primary election technological parameter domain of a titanium alloy thin-wall component; carrying out an orthogonal test; testing the surface integrity parameter of a test component; establishing acharacteristic relational expression of a titanium alloy thin-wall component milling technological parameter and surface integrity; according to the relational expression of the titanium alloy thin-wall component milling technological parameter and the surface integrity, a target function and a milling technological parameter constraint condition, establishing an optimization model for the anti-fatigue efficient milling parameter of the titanium alloy thin-wall component; and through an optimization tool in MATLAB, solving the optimization model for the anti-fatigue efficient milling parameterof the titanium alloy thin-wall component to obtain the anti-fatigue efficient milling parameter of the titanium alloy thin-wall component. By use of the method, the problems of poor surface integrity characteristic and low material removal rate in a milling process of the titanium alloy thin-wall component are solved.

Description

【Technical field】 [0001] The invention belongs to the technical field of anti-fatigue precision cutting and processing, and in particular relates to a parameter optimization control method for anti-fatigue and high-efficiency milling of titanium alloy thin-walled components. 【Background technique】 [0002] Titanium alloy materials have excellent mechanical properties, low density, high specific strength, corrosion resistance, high and low temperature resistance, and are another important structural material after steel and iron. A variety of information and data show that the use of titanium alloys instead of steel materials in aircraft engines can reduce the weight of the engine structure by 30% to 40%. Therefore, titanium alloys are widely and widely used in the manufacture of aircraft engines and airframes, which can effectively improve the thrust-to-weight ratio of the engine and the efficiency of the airframe mechanism, and help alleviate the thermal barrier phenomenon....

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F30/17G06F2111/04
Inventor 张定华姚倡锋任军学武导侠谭靓沈雪红
Owner NORTHWESTERN POLYTECHNICAL UNIV
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