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TiAlSiN/CrAlSiN纳米多层涂层刀具干切削TC4钛合金切削性能

刘杰 华俊芳 段慧珍 易根苗 邓欣

宇航材料工艺2024,Vol.54Issue(4):103-109,7.
宇航材料工艺2024,Vol.54Issue(4):103-109,7.DOI:10.12044/j.issn.1007-2330.2024.04.015

TiAlSiN/CrAlSiN纳米多层涂层刀具干切削TC4钛合金切削性能

Cutting Performance of TiAlSiN/CrAlSiN Nano-multilayer Coated Tools During Dry Cutting of TC4 Titanium Alloy

刘杰 1华俊芳 1段慧珍 1易根苗 1邓欣2

作者信息

  • 1. 广州番禺职业技术学院智能制造学院,广州 511483
  • 2. 广东工业大学机电工程学院,广州 510006
  • 折叠

摘要

Abstract

Cutting tools of titanium alloys are subject to severe wear due to its chemical activity and high cutting temperatures.Applying coatings to the tool surface is an effective way to extend tool service time.Using PVD cathodic arc evaporation technology,the TiAlSiN/CrAlSiN nano-multilayer coating tool was made by alternately superposing TiAlSi target and CrAlSi target,which are used to cut conventional titanium alloy and 3D printed titanium alloy,respectively.The obtained TiAlSiN/CrAlSiN nanomultilayer coatings exhibit high hardness.When cutting titanium alloys,the tool wear is characterized by coating delamination,craters on the rake face,uniform wear on flank face,and chipping on tool nose.The main cause of tool wear is adhesion,followed by high temperature oxidation.Among the three cutting parameters,the effect of cutting speed on cutting force and cutting temperature is much greater than that of depth of cut and feed.Compared with conventional TC4,the cutting temperature and cutting force of 3D printed TC4 are lower than those of conventional TC4 due to the decrease of elongation and hardness and the increase of elastic modulus,and the tool life is correspondingly prolonged.

关键词

纳米多层涂层/TiAlSiN/CrAlSiN/刀具磨损/钛合金/3D打印钛合金

Key words

Nano-multilayer coating/TiAlSiN/CrAlSiN/Tool wear/Titanium alloy/3D-printed titanium alloy

分类

航空航天

引用本文复制引用

刘杰,华俊芳,段慧珍,易根苗,邓欣..TiAlSiN/CrAlSiN纳米多层涂层刀具干切削TC4钛合金切削性能[J].宇航材料工艺,2024,54(4):103-109,7.

基金项目

2022年度广东省普通高校特色创新类项目(2022KTSCX294) (2022KTSCX294)

广州市基础与应用基础研究项目(202201010393,202201011848) (202201010393,202201011848)

佛山市科技创新团队项目(FSOAAKJ919-4402-0023) (FSOAAKJ919-4402-0023)

季华实验室项目(X190061UZ190) (X190061UZ190)

宇航材料工艺

OA北大核心CSTPCD

1007-2330

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