Multilayer Cutting Tool Coating for Wear and Comb Crack Resistance

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Solution Overview

Problem

Existing coated cutting tools face challenges in wear resistance and comb crack resistance, especially in dry machining and machining with coolant, which affects their performance in steel and cast material machining.

Innovation Solution

A coated cutting tool with a specific multilayer structure comprising a 4-14 µm thick Ti1-xAlxN inner layer, a 0.05-1 µm thick TiCN intermediate layer, and a 1-9 µm thick α-Al2O3 outer layer, where the α-Al2O3 layer exhibits a controlled texture coefficient and Σ3 grain boundary orientation for enhanced wear resistance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a conventional coated cutting tool structure is used, then the tool can perform basic cutting operations, but the wear resistance and comb crack resistance are insufficient

Engineering Contradiction:
Improvewear resistance and comb crack resistanceVSAvoidcoating structure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The coating is divided into three distinct layers with specific functions: an inner layer of Ti1-xAlxN (4-14 μm) providing base wear resistance and adhesion, an intermediate layer of TiCN (0.05-1 μm) enhancing bond strength and reducing internal stress, and an outer layer of α-Al2O3 (1-9 μm) providing exceptional crater wear and comb crack resistance. This segmentation allows each layer to optimize its properties for its specific function, resolving the contradiction between improved reliability and increased structural complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent employs a composite coating structure combining three different materials (Ti1-xAlxN, TiCN, and α-Al2O3) with complementary properties. The Ti1-xAlxN provides toughness and adhesion, TiCN adds intermediate bonding and stress management, while α-Al2O3 delivers superior wear and crack resistance. This composite approach achieves enhanced reliability by leveraging the synergistic effects of multiple materials rather than relying on a single coating layer.

Inventive Principle:
Principle #40Composite materials

2Reliability

If the α-Al2O3 layer thickness is increased to improve wear resistance, then crater wear resistance improves, but the risk of comb crack formation increases

Engineering Contradiction:
Improvecrater wear resistanceVSAvoidcomb crack resistance
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The coating is divided into three distinct layers with specific functions: an inner layer of Ti1-xAlxN (4-14 μm) providing base wear resistance and adhesion, an intermediate layer of TiCN (0.05-1 μm) enhancing bond strength and reducing internal stress, and an outer layer of α-Al2O3 (1-9 μm) providing exceptional crater wear and comb crack resistance. This segmentation allows each layer to optimize its properties for its specific function, resolving the contradiction between improved reliability and increased structural complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The TiCN intermediate layer acts as a mediator between the Ti1-xAlxN substrate and the α-Al2O3 outer layer. It provides a transition zone that manages thermal expansion differences and mechanical stress between the two outer layers, preventing stress concentration that would lead to comb cracks while still allowing the α-Al2O3 layer to provide its full wear protection capability.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If a thin TiCN intermediate layer is used to improve adhesion, then layer bonding improves, but the complexity of the coating process increases

Engineering Contradiction:
Improvelayer adhesionVSAvoidcoating process complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The coating is divided into three distinct layers with specific functions: an inner layer of Ti1-xAlxN (4-14 μm) providing base wear resistance and adhesion, an intermediate layer of TiCN (0.05-1 μm) enhancing bond strength and reducing internal stress, and an outer layer of α-Al2O3 (1-9 μm) providing exceptional crater wear and comb crack resistance. This segmentation allows each layer to optimize its properties for its specific function, resolving the contradiction between improved reliability and increased structural complexity.

Inventive Principle:
Principle #1Segmentation

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The proposed coating structure significantly improves wear resistance and comb crack resistance, leading to extended tool life and improved performance in both dry and coolant-assisted machining of steel and cast materials.

Implementation Method 1

the α-Al2O3 layer exhibits an X-ray diffraction pattern, as measured using CuKα radiation and theta-2theta scan, and the texture coefficient TC(hkl) is defined according to Harris formula

Methodology Applied
Scientific EffectTexture coefficient control: Crystallisation

Implementation Method 2

Coated cutting tools are known in the art and hard material layers may be applied by PVD and/or CVD

Methodology Applied
Scientific EffectPhysical Vapour Deposition: Physical Vapour Deposition

Implementation Method 3

Coated cutting tools are known in the art and hard material layers may be applied by PVD and/or CVD

Methodology Applied
Scientific EffectChemical Vapour Deposition: Chemical Vapour Deposition

Data Source

PatentEP3574129B1Coated cutting tool for chip forming metal machining of steel
Publication Date: 2025.04.16 WALTER AG
  • EP3574129B1 patent drawingFigure 1~2
  • EP3574129B1 patent drawing
  • EP3574129B1 patent drawing

AI summary

The present invention relates to a coated cutting tool comprising a substrate and a coating, wherein the coating comprises an inner layer of 4-14 µm thick Ti1-xAlxN, an intermediate layer of 0.05-1 µm TiCN and at least one outer layer of 1-9 µm α-Al2O3, wherein said α-Al2O3 layer exhibits an X-ray diffraction pattern, as measured using CuKα radiation and theta-2theta scan, and the texture coefficient TC(hkl) is defined according to Harris formula, wherein the (hkl) reflections used are (0 2 4), (1 1 6), (3 0 0) and (0 0 12), I(hkl) = measured intensity (peak intensity) of the (hkl) reflection, l0(hkl) = standard intensity according to ICDD's PDF-card No. 00-042-1468, n = number of reflections used in the calculation, and 3 < TC(0 0 12) < 4.