In-Situ Heat Treatment of AM Metal Layers for Strength and Tolerance

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Solution Overview

Problem

Additive manufacturing processes result in components with inferior mechanical properties and dimensional tolerances compared to traditional methods, due to inadequate cooling rates and thermal stresses, leading to the need for time-consuming post-formation processing to achieve desired mechanical properties and tolerances.

Innovation Solution

Implementing in-situ thermal management during deposition via induction heating and rapid quenching, combined with electromagnetic stirring, to control the heat affected zone and achieve solution heat treatment, thereby optimizing microstructure and macrostructure.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Shape

If additive manufacturing processes are used to create complex geometries, then geometric complexity is improved, but mechanical properties deteriorate due to slow cooling rates

Engineering Contradiction:
Improvegeometric complexityVSAvoidmechanical properties
Core Design Contradiction:
ShapeVSStrength

Solution Approach 1:

The additive manufacturing process is divided into discrete layers that are deposited and heat treated sequentially. Each layer undergoes solution heat treatment and quenching independently before the next layer is added, allowing control of microstructure in each segment while building the complex geometry layer by layer

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Solution heat treatment and quenching are performed on each deposited layer immediately after deposition, before subsequent layers are added. This preliminary heat treatment establishes the desired microstructure and mechanical properties in each layer before it becomes part of the final component

Inventive Principle:
Principle #10Preliminary action

2Strength

If rapid cooling is applied to achieve desired microstructure, then mechanical properties are improved, but thermal stresses and distortion increase

Engineering Contradiction:
Improvemechanical propertiesVSAvoidthermal stresses
Core Design Contradiction:
StrengthVSStress or pressure

Solution Approach 1:

The component is built and heat treated in small sequential layers rather than as a single large component. This segmentation limits the volume of material subjected to rapid cooling at any one time, reducing thermal gradients and associated stresses while still achieving the desired microstructure in each layer

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The heat treatment process is made dynamic by adjusting parameters such as heating rate, holding time, and quenching rate for each individual layer based on its position and the accumulated thermal history. This dynamic control allows optimization of cooling rate to achieve desired microstructure while minimizing thermal stresses

Inventive Principle:
Principle #15Dynamics

3Strength

If post-formation heat treatment is applied to improve mechanical properties, then strength is improved, but manufacturing time increases

Engineering Contradiction:
Improvemechanical propertiesVSAvoidmanufacturing time
Core Design Contradiction:
StrengthVSLoss of time

Solution Approach 1:

The solution heat treatment and quenching operations are merged with the additive manufacturing process itself, rather than being performed as separate post-processing steps. Each layer undergoes heat treatment immediately after deposition, combining the manufacturing and heat treatment operations into a single integrated process

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

Heat treatment is performed preliminarily on each layer during the deposition process rather than as a final post-processing step on the complete component. This eliminates the need for separate post-formation heat treatment cycles and reduces total manufacturing time

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 method results in components with improved mechanical properties and dimensional stability, approaching or exceeding those of traditionally manufactured components without additional post-formation processing.

Implementation Method 1

heating, for example via induction heating, to provide in-situ heat treatment

Methodology Applied
Scientific EffectInduction heating: Induction Heating

Implementation Method 2

followed by rapid cryogenic quenching or rapid cooling

Methodology Applied
Scientific EffectRapid quenching: Cooling

Implementation Method 3

electromagnetic stirring

Methodology Applied
Scientific EffectElectromagnetic stirring: Electromagnetic Stirring

Data Source

PatentUS12502825B2Method and apparatus for in-situ thermal management and heat treatment of additively manufacturing components
Publication Date: 2025.12.23 SPIRIT AEROSYSTEMS INC
  • US12502825B2 patent drawing
  • US12502825B2 patent drawing
  • US12502825B2 patent drawing

AI summary

Methods for in-situ solution heat treating an additively manufactured metallic component in order to increase the mechanical properties thereof and systems to perform the same. The method can include depositing filler material on a substrate forming a deposition layer, measuring the temperature of a heat affected zone corresponding to the deposition layer, and solution heat treating the deposition layer subsequent to the depositing and proximate to the deposition head. The solution heat treating can include heating the deposition layer to a solution temperature so as to achieve solution heat treatment and controlling the cooling rate of the deposition layer to at or above the critical cooling rate of the filler material until a target temperature is reached. Optionally, the method can include inducing an electron flow in the deposition layer to electromagnetically stir molten filler material in the heat affected zone.