Nano-multilayer Coating for Cutting Tools Comb Crack Resistance

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Solution Overview

Problem

Cutting tools used in metal machining face challenges with thermal cracks ('comb cracks') and mechanical fatigue leading to chipping, requiring enhanced resistance and toughness, especially at the cutting edge.

Innovation Solution

A nano-multilayer coating comprising alternating layers of Ti1-XAlXN and Cr1-yAlYN, with specific composition and thickness ranges, applied directly on the substrate, and analyzed using θ-2θ XRD to optimize peak intensity ratios, enhancing comb crack resistance and edge line toughness.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If the coating is made tougher to reduce chipping, then mechanical fatigue resistance improves, but comb crack resistance deteriorates

Engineering Contradiction:
Improveedge line toughnessVSAvoidcomb crack resistance
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The coating is divided into multiple alternating nanolayers of TiAlN and CrAlN with different compositions and properties. The TiAlN layers provide toughness and crack resistance while the CrAlN layers provide hardness and wear resistance. This segmentation allows the coating to simultaneously achieve high edge line toughness and comb crack resistance through the synergistic effect of alternating soft and hard layers.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The coating uses a composite nano-multilayer structure combining TiAlN and CrAlN materials with specific aluminum content ranges. The TiAlN layer (40-70 at% Al) provides ductility and crack resistance, while the CrAlN layer (60-80 at% Al) provides hardness and thermal stability. This composite structure resolves the contradiction by integrating materials with complementary properties at the nanoscale.

Inventive Principle:
Principle #40Composite materials

2Reliability

If the coating is made harder to resist wear, then comb crack resistance improves, but edge line toughness deteriorates

Engineering Contradiction:
Improvecomb crack resistanceVSAvoidedge line toughness
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The coating alternates between harder CrAlN layers and tougher TiAlN layers at the nanoscale. The CrAlN layers (60-80 at% Al) provide hardness and wear resistance, while the TiAlN layers (40-70 at% Al) provide ductility and toughness. This segmentation distributes the mechanical stresses, allowing the hard layers to resist wear while the tough layers prevent catastrophic failure.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different regions of the coating have different local properties: CrAlN layers are optimized for hardness and wear resistance, while TiAlN layers are optimized for toughness and crack resistance. The local composition and structure are tailored to provide the specific property needed at that location, achieving overall performance optimization.

Inventive Principle:
Principle #3Local quality

3Ease of manufacture

If the layer period thickness is increased, then manufacturing complexity reduces, but comb crack resistance deteriorates

Engineering Contradiction:
Improvecoating deposition simplicityVSAvoidcomb crack resistance
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent specifies precise parameter ranges for the nano-multilayer structure: layer period thickness of 2-16 nm, TiAlN layer thickness of 0.5-4 nm, and CrAlN layer thickness of 0.5-4 nm. These parameter optimizations ensure that the coating achieves maximum comb crack resistance while remaining manufacturable using conventional PVD techniques. The specific aluminum content ranges (40-70 at% for TiAlN, 60-80 at% for CrAlN) further optimize the balance between resistance and manufacturability.

Inventive Principle:
Principle #35Parameter changes

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 nano-multilayer coating significantly improves comb crack resistance and edge line toughness, extending tool life by providing a balanced resistance to thermal and mechanical loads during metal machining operations.

Implementation Method 1

In milling, the thermal load will vary over time whereby thermal tensions are induced which may lead to so-called thermal cracks, herein referred to as 'comb cracks', in coatings. Increasing the comb crack resistance is thus of great importance to increase the tool lifetime.

Methodology Applied
Scientific EffectThermal stress resistance:

Implementation Method 2

Also, mechanical load may lead to fatigue in the cutting edge leading to chipping whereby small fragments of the cutting edge may come loose from the rest of the substrate. A sufficient toughness of the coating, in particular at the cutting edge, may reduce such chipping.

Methodology Applied
Scientific EffectMechanical fatigue resistance:

Implementation Method 3

the peak intensity ratio of I(200)/I(111) as measured by θ-2θ X-Ray-Diffraction (XRD) on the flank face is >1

Methodology Applied
Scientific EffectX-Ray Diffraction: X-Ray

Data Source

PatentEP4386110A1A coated cutting tool
Publication Date: 2024.06.19 SANDVIK COROMANT
  • EP4386110A1 patent drawingFigure 1~2
  • EP4386110A1 patent drawingFigure 3
  • EP4386110A1 patent drawingFigure 4

AI summary

The invention relates to a coated cutting tool (1) comprising a substrate (5) and a coating (6), wherein the coating (6) comprises a nano-multilayer (8) consisting of alternating layers of i) a first nanolayer (9) of Ti1-XAlXN, wherein 0.63≤ x ≤0.95, and ii) a second nanolayer (10) of Cr1-yAlyN, wherein 0.5≤ y ≤ 0.9 wherein a sequence of one first nanolayer (9) and one second nanolayer (10) forms a layer period, wherein a) the layer period of the nano-multilayer (8) has an average thickness ≤ 16 nm and ≥ 2 nm, b) the thickness of the nano-multilayer (8) ranges from 150 nm to 10 µm; and c) the peak intensity ratio of I(200)/I(111) as measured by XRD on the flank face is >1.