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Non-equidistant texture finishing abrasion-reducing turning blade

A non-isometric and finishing technology, applied in metal processing equipment, cutting tools for lathes, turning equipment, etc., can solve problems such as high cutting temperature, tool wear, and large cutting force, and achieve lower cutting temperature and lower cutting speed. Force, enhance the effect of heat dissipation

Inactive Publication Date: 2019-05-21
HARBIN UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problems of large cutting force, high cutting temperature, serious tool wear and damage in the process of high-temperature alloy finishing, the present invention provides a non-equidistant texture finish machining wear-reducing blade, which is mainly used in automotive Finishing process of superalloy under fog cooling

Method used

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  • Non-equidistant texture finishing abrasion-reducing turning blade
  • Non-equidistant texture finishing abrasion-reducing turning blade
  • Non-equidistant texture finishing abrasion-reducing turning blade

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Embodiment Construction

[0015] figure 1 It is a three-dimensional diagram of non-equidistant texture finish machining and anti-friction turning blades. The main body of the blade is designed as an 80° rhombic turning blade with a radius of 0.8mm and the material is cemented carbide.

[0016] figure 2 It is a three-dimensional enlarged view of the micro-texture, which are the enlarged views of the micro-texture of the rake face and the micro-texture of the flank respectively.

[0017] exist image 3 Among them, there are non-equidistant arc-shaped groove micro-textures (1) distributed on the rake face. The groove widths of the micro-textures are different, and its size conforms to the arithmetic sequence with the first term being 20 μm and the tolerance being 5 μm. The texture spacing size conforms to the arithmetic sequence whose first term is 60 μm and the tolerance is 10 μm. The distribution mode is that the closer to the cutting edge, the denser the texture, and the smaller the texture groove ...

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Abstract

The invention relates to a non-equidistant texture finishing abrasion-reducing turning blade. The blade is provided with non-equidistant micro-textures with unequal groove widths and intervals on thefront blade surface and rear blade surface, and the distribution mode of the non-equidistant micro-textures is designed to be dense in front and sparse in back according to the stress distribution condition of a cutter during cutting. The closer the texture is to a cutting edge, the denser the texture is and the smaller the groove width is, thus the problem of breakage of the micro-textures is solved, the abrasion and breakage of the cutter are reduced, and the cutting force is reduced. A cuttings breaking table is machined on the front face of the blade to control cuttings breaking, the cutting edge of the blade is a curved edge, the flow direction of cuttings is changed, and the cuttings are prevented from winding or scratching a workpiece. A volume groove is designed on a polygonal convex table of the front blade surface, and a guide groove enhances the heat dissipation capability of the blade and reduces the cutting temperature.

Description

technical field [0001] The invention relates to a non-equidistant texture finish machining antifriction turning blade. The invention belongs to the technical field of metal cutting tool wear reduction, and is mainly used in the finishing process of high-temperature alloys under steam-mist cooling. Background technique [0002] Nickel-based superalloy GH4169 is a nickel-based alloy material with high hardness, high strength, corrosion resistance and high temperature resistance, which can maintain good stability even in very harsh environments. Because of its excellent performance, it has been widely used in aviation field in recent years. Nickel-based superalloy GH4169 is often used to make heat-resistant parts such as discs and blades of aerospace engines and gas turbines, and occupies an important position in the aviation, aerospace and atomic energy industries. In recent years, with the rapid development of the defense industry, great progress has been made in the fields...

Claims

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Application Information

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IPC IPC(8): B23B27/10B23B27/14B23B27/22
Inventor 冯新敏于闯胡景殊
Owner HARBIN UNIV OF SCI & TECH
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