Grain Refiners for Additive Manufacturing Aluminum Alloys

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Solution Overview

Problem

Conventional aluminum alloys are prone to solidification cracking during additive manufacturing, limiting their use in high-strength applications, and existing methods to prevent cracking, such as adding silicon, are not suitable for aerospace-grade materials.

Innovation Solution

Incorporating grain refiners like TiB2, TiC, TiAl, and AlB2 into aluminum alloys during the additive manufacturing process to refine the grain structure and prevent cracking, with the grain refiners being added in specific proportions to the metal alloy melt pool to form a modified alloy with improved solidification characteristics.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If conventional aluminum alloys are used in additive manufacturing, then the manufacturing process can be performed, but solidification cracking occurs during solidification

Engineering Contradiction:
Improveadditive manufacturing processabilityVSAvoidresistance to solidification cracking
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

Grain refiners (TiB2, TiC, TiAl, AlB2) are added to the aluminum alloy powder feedstock before additive manufacturing. These refiners pre-establish nucleation sites that will guide grain formation during the manufacturing process, preventing solidification cracking before it occurs

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The grain structure parameters of the aluminum alloy are fundamentally changed by adding grain refiners. This transforms the microstructure from coarse, crack-prone grains to fine, controlled grains with specific orientations that resist solidification cracking while maintaining high strength

Inventive Principle:
Principle #35Parameter changes

2Reliability

If silicon is added to aluminum alloy to prevent cracking, then solidification cracking is reduced, but the alloy strength decreases and becomes unsuitable for aerospace applications

Engineering Contradiction:
Improveresistance to solidification crackingVSAvoidalloy strength
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

Grain refiners (TiB2, TiC, TiAl, AlB2) serve as intermediary substances that mediate between the conflicting requirements of crack resistance and strength. These refiners provide nucleation sites for grain formation, controlling solidification to prevent cracking without compromising the high strength properties needed for aerospace applications

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The invention creates a composite aluminum alloy system by incorporating grain refiner particles into the aluminum matrix. This composite structure combines the crack-resistance benefits of refined grain structure with the high strength of aerospace-grade aluminum alloys, avoiding the strength reduction associated with silicon addition

Inventive Principle:
Principle #40Composite materials

3Strength

If high strength aluminum alloys are used for aerospace applications, then the mechanical properties are sufficient, but the alloys are prone to solidification cracking during additive manufacturing

Engineering Contradiction:
Improvemechanical strengthVSAvoidadditive manufacturing processability
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

Grain refiners are incorporated into the high strength aluminum alloy powder before additive manufacturing. This preliminary action establishes a controlled grain structure that enables these high-strength alloys to be successfully manufactured additively by preventing solidification cracking during the process

Inventive Principle:
Principle #10Preliminary action

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 modified alloys exhibit enhanced strength and resistance to solidification cracking, enabling the production of high-strength aluminum alloys suitable for aerospace applications by refining the grain structure and improving mechanical properties.

Implementation Method 1

incorporating grain refiners like TiB2, TiC, TiAl, and AlB2 into aluminum alloys during the additive manufacturing process to refine the grain structure

Methodology Applied
Scientific EffectNucleation: Nucleation

Implementation Method 2

solidifying at least a portion of the melt pool to form a modified alloy comprising an amount of the at least one grain refiner in the modified alloy in the range of between from 1.5% to 3.5% by weight

Methodology Applied
Scientific EffectGrain refinement: Crystallisation

Implementation Method 3

exposing the feedstocks to an energy source to form a melt pool comprising the at least one metal alloy and the at least one grain refiner

Methodology Applied
Scientific EffectLaser heating: Laser

Implementation Method 4

spraying or otherwise injecting a powder or a liquid into a focused beam of a high-power laser or nexus of a plurality of high-powered lasers under controlled atmospheric conditions, thereby creating a weld pool

Methodology Applied
Scientific EffectMelting: Melting

Implementation Method 5

solidifying at least a portion of the melt pool to form a modified alloy

Methodology Applied
Scientific EffectSolidification: Crystallisation

Data Source

PatentEP3446813B1Method of tailoring high strength aluminum alloys for additive manufacturing through the use of grain refiners
Publication Date: 2021.08.04 THE BOEING CO
  • EP3446813B1 patent drawingFigure 1A
  • EP3446813B1 patent drawingFigure 1B~1C
  • EP3446813B1 patent drawingFigure 2

AI summary

Provided is a method for modifying a metal alloy for use in additive manufacturing. The method includes providing a metal alloy; providing at least one grain refiner; forming a melt pool that includes the at least one metal alloy and the at least one grain refiner; and solidifying at least a portion the melt pool to form a modified alloy.