Magnesium Alloy Forming via High Strain Rate Preform Processing

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Solution Overview

Problem

Magnesium-based alloys are limited in forming components that can withstand high-strain rate processes due to cracking issues, restricting their use in lightweight metal components for vehicles where high strength and ductility are required.

Innovation Solution

A method involving a first deforming process with a predetermined strain rate and temperature to form a preform with a tailored microstructure, followed by a second high-strain rate process, which includes heat treatment to prevent cracking and enhance mechanical properties, using compositions with zirconium, manganese, scandium, rare earth metals, zinc, and aluminum.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If magnesium-based alloys are subjected to high strain rate processes, then productivity and manufacturing capability are improved, but cracking occurs reducing reliability

Engineering Contradiction:
Improvemanufacturing capabilityVSAvoidcracking resistance
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

A preform is created before the final high-strain-rate forming process. This preform undergoes preliminary deformation and microstructure development that prepares the material to withstand subsequent high-strain-rate processing without cracking, enabling both high productivity and reliability

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent applies temperature and strain rate parameter changes during processing. By controlling temperature during the preform creation and final forming, and by using dynamic strain rate control, the material properties are optimized to prevent cracking while maintaining high manufacturing capability

Inventive Principle:
Principle #35Parameter changes

2Reliability

If magnesium-based alloys are limited to low strain rate processes, then cracking is avoided improving reliability, but productivity and manufacturing versatility are reduced

Engineering Contradiction:
Improvecracking resistanceVSAvoidmanufacturing capability
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The preform creation step performs preliminary deformation at controlled conditions, preparing the microstructure in advance. This allows the final high-strain-rate forming to proceed without cracking, thereby improving both reliability and productivity

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent employs dynamic strain rate control during the forming process. By adjusting the strain rate dynamically based on material response, the process achieves both high productivity through faster forming and high reliability by preventing cracking through adaptive rate control

Inventive Principle:
Principle #15Dynamics

3Manufacturing precision

If high strain rate processes are applied to magnesium alloys, then manufacturing precision and component performance are improved, but the alloy composition complexity increases

Engineering Contradiction:
Improvecomponent qualityVSAvoidalloy composition
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent optimizes processing parameters including temperature, strain rate, and deformation stages rather than relying solely on complex alloy compositions. This approach achieves high manufacturing precision while maintaining relatively simple alloy compositions

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The preform creation step performs preliminary microstructure development that simplifies the requirements for the final forming process. This staged approach achieves high component quality without requiring overly complex alloy compositions

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

Enables the formation of magnesium-based alloy components that are substantially free of cracking and exhibit improved mechanical properties, suitable for automotive applications, by controlling strain rates and temperatures to create thermally stable microstructures that resist dynamic recrystallization.

Implementation Method 1

The matrix undergoes dynamic recrystallization during the treating to form refined grains

Methodology Applied
Scientific EffectDynamic recrystallization: Crystallisation

Implementation Method 2

prior to the treating, the method further includes heat-treating the casting to homogenize the magnesium-based alloy, form thermally-stable refined precipitates

Methodology Applied
Scientific EffectHeat treatment: Heat Treatment

Implementation Method 3

The preform includes one or more intermetallic species selected from the group consisting of: ZnZr, AlMn, MnSc, AlRE

Methodology Applied
Scientific EffectPrecipitation: Precipitation

Data Source

PatentUS11655513B2Methods of forming magnesium-based alloy articles at high strain rates
Publication Date: 2023.05.23 GM GLOBAL TECHNOLOGY OPERATIONS LLC
  • US11655513B2 patent drawing
  • US11655513B2 patent drawing
  • US11655513B2 patent drawing

AI summary

Methods of making magnesium-based alloy components, such as automotive components, include treating a casting comprising a magnesium-based alloy to a first deforming process to form a preform. In one aspect, the first deforming process has a first maximum predetermined strain rate of greater than or equal to about 0.001/s to less than or equal to about 1/s in an environment having a temperature of ≥to about 250° C. to ≤to about 450° C. In another aspect, the first deforming process is cold deforming that is followed by annealing. The preform is then subjected to a second deforming process having a second maximum predetermined strain rate of ≥about 1/s to ≤about 100/s in an environment having a temperature of ≥about 150° C. to ≤about 450° C. to form the magnesium-based alloy component substantially free of cracking. A solid magnesium-based alloy component having select microstructures are also provided.