High Entropy Alloy with Nanoscale Self-Ordering for Additive Manufacturing

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current high-temperature superalloys used in aerospace applications face challenges such as poor printability, weldability, and anisotropic mechanical properties, leading to cracking and limited practical utility in 3D-printed materials, which restrict their application in extreme environments.

Innovation Solution

A multi-component high entropy alloy with a composition of Co, Ni, Cr, Al, Ti, Mo, and Nb is developed, featuring a nanoscale atomic self-ordering structure and a method involving selective laser melting to achieve high density and isotropic mechanical properties, overcoming the limitations of traditional superalloys.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If traditional precipitate-strengthened superalloys are used for geometric complexity structural engine components, then high temperature protection and strength are improved, but printability and weldability deteriorate, leading to cracking and poor mechanical properties

Engineering Contradiction:
Improvehigh temperature protectionVSAvoidprintability
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The patent changes the compositional parameters by using multi-component high entropy alloy design with at least five major elements (Co, Ni, Cr, Al, Ti, Mo, Nb, Ta) each at 5-35 at.%, replacing traditional Ni-based superalloy compositions. This compositional parameter change fundamentally alters the material's printability and cracking resistance while maintaining high-temperature strength

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent creates a composite microstructure consisting of ordered precipitates (γ′-Co3(Al,W) and γ''-CoNiAl phases) within a disordered FCC matrix. This composite structure provides both the high-temperature strength from ordered precipitates and the printability/weldability from the disordered matrix, resolving the contradiction between strength and ease of manufacture

Inventive Principle:
Principle #40Composite materials

2Shape

If traditional superalloys are used in 3D printing, then complex geometries can be fabricated, but anisotropy in microstructures and mechanical properties occurs in building direction and scanning direction, limiting practical utility

Engineering Contradiction:
Improvecomplex geometriesVSAvoidisotropy
Core Design Contradiction:
ShapeVSStability of the object's composition

Solution Approach 1:

The patent uses specific 3D printing parameters (laser power 200-500W, scanning speed 100-1000mm/s, layer thickness 20-100μm, hatch spacing 50-200μm) to control the solidification process. These parameter changes promote equiaxed grain formation and reduce directional solidification effects, achieving isotropic mechanical properties while maintaining complex geometry fabrication capability

Inventive Principle:
Principle #35Parameter changes

3Strength

If multi-component high entropy alloys are developed for aerospace applications, then high strength and ductility are achieved, but manufacturing complexity increases due to multiple element composition control

Engineering Contradiction:
Improvetensile strengthVSAvoidcomposition control
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The patent establishes specific composition ranges for each element (Co: 10-70 at.%, Ni: 10-50 at.%, Cr: 0.1-20 at.%, Al: 0.1-20 at.%, Ti: 0.01-10 at.%, Mo: 0.01-10 at.%, Nb: 0.01-10 at.%, Ta: 0.1-10 at.%) to ensure formation of the desired microstructure. This parameter standardization simplifies manufacturing complexity by providing clear compositional guidelines while achieving ultrahigh strength

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent utilizes selective laser melting's rapid cooling rate to automatically create nanoscale microstructures and self-ordering structures during the printing process itself, without requiring post-processing heat treatment or additional manufacturing steps. This self-service approach reduces manufacturing complexity despite the multi-component composition

Inventive Principle:
Principle #25Self-service

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 resulting alloy exhibits exceptional strength, ductility, and isotropic properties, with a high tensile strength of up to 1.5 GPa and uniform elongation of 22.5%, significantly improving the service life and formability of aerospace components.

Implementation Method 1

melting and solidifying the spherical alloy powder by selective laser to obtain the multi-component high entropy alloy with a nanoscale atomic self-ordering structure

Methodology Applied
Scientific EffectSelective Laser Melting: Laser

Implementation Method 2

Its rapid cooling rate is particularly adept at creating nanoscale microstructures

Methodology Applied
Scientific EffectRapid Solidification: Freezing

Data Source

PatentUS20240344183A1Multi-component high entropy alloy with nanoscale atomic self-ordering structure and preparation methods thereof
Publication Date: 2024.10.17 CITY UNIVERSITY OF HONG KONG
  • US20240344183A1 patent drawing
  • US20240344183A1 patent drawing
  • US20240344183A1 patent drawing

AI summary

The present invention uses additive manufacturing technology to develop a new L12 reinforced multi-component high entropy alloy, which has high density and excellent strength and ductility mechanical properties. The selective laser melting process employed in crafting these multi-component high entropy alloys renders them safer, more cost-effective, and significantly reduces processing time, thus positioning them as highly competitive offerings within the market.