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Cutting angle acquiring method for restraining milling burr of carbon fiber laminate

A technology of cutting angle and carbon fiber layer, which is applied in the field of milling of carbon fiber laminate composite materials, to achieve the effect of avoiding burrs and reducing the length of defects

Active Publication Date: 2017-01-11
SOUTHWEST JIAOTONG UNIV +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

This new technology helps prevent damage from small cracks or imperfections during processing of composites made up by layers of fibers. By millering it slightly beyond an angled cut-off line, these flaws can become less visible compared to previous methods without this technique being applied. Additionally, if there were any differences between different materials for example due to changes over time (such as temperature), adjustments could also affect how well they work together.

Problems solved by technology

Technological Problem addressed in this patents relating to the use of carbon fibers for various purposes including making composite structures like vehicles or airplanes due to their superior physical performance compared to traditional metals (such as steel). These composites require specialized techniques involving machining processes called sandwich blinds, which involves laying up individual sheets of preform beforehand without damaging them while they still hold together tightly enough to resist deformation under heavy loads. Additionally, these compositions must exhibit improved durability over long periods of operation because they often experience severe impact from external factors such as temperature changes, moisture absorption, abrasion, etc., causing cracks and fractures.

Method used

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  • Cutting angle acquiring method for restraining milling burr of carbon fiber laminate
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  • Cutting angle acquiring method for restraining milling burr of carbon fiber laminate

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Embodiment Construction

[0022] The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments. The method of the present invention includes constructing a relationship model between milling burrs and cutting force angles, and calculating the cutting angle at which the cutting force is parallel to the carbon fiber layer. Carbon fiber laminates are made of multi-layer prepregs laminated according to different fiber directions. The prepregs are composited by reinforcing material carbon fiber and matrix material resin. Its structure is as follows: figure 1 shown.

[0023] The milling process of carbon fiber laminates is as follows: figure 2 shown. It can be seen that due to the relationship between the helix angle of the cutter itself, when the cutter teeth cut the material, the milling force on the material is F, and its direction is perpendicular to the rake face of the cutter tooth, which can be decomposed into F along the feed ...

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Abstract

The invention discloses a cutting angle acquiring method for restraining milling burr of a carbon fiber laminate. The method comprises the following steps: constructing a calculating model for milling burr and cutting force angle of the carbon fiber laminate; acquiring the cutting angle with the cutting force parallel to a carbon fiber layer; accordingly designing an orthogonal experiment for comparing the burr defect under an appointed technical condition; selecting the cutting angle for effectively restraining the milling burr of the carbon fiber laminate. According to the method provided by the invention, the structure modification for machine tool is not required and the method has the advantages of simple and convenient operation, high calculation efficiency and high practicability.

Description

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Claims

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Application Information

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Owner SOUTHWEST JIAOTONG UNIV
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