Metal Additive Manufacturing Support Removal by Thermal Pulse

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Solution Overview

Problem

The removal of support structures from additive manufactured metallic components, particularly high-strength metals like superalloys, is challenging due to their strong interface with the component, which can lead to damage during removal and geometric distortion.

Innovation Solution

Exposing the component and support structure to a thermal pulse to weaken or break the interface between them, allowing for easier mechanical removal, and optionally applying additional thermal pulses for surface finishing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If support structures are designed with strong interface to component, then support strength is improved, but support removal difficulty increases

Engineering Contradiction:
Improvesupport strengthVSAvoidsupport removal difficulty
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

A heat treatment process is applied before support removal to selectively reduce the strength of the interface between supports and component. This preliminary thermal action weakens the bond at the interface region, allowing easy support removal while preserving the strong interface during the additive manufacturing process itself

Inventive Principle:
Principle #10Preliminary action

2Ease of manufacture

If support structures are designed with lattice or toothed profile, then support removal ease is improved, but interface strength decreases

Engineering Contradiction:
Improvesupport removal easeVSAvoidinterface strength
Core Design Contradiction:
Ease of manufactureVSStrength

Solution Approach 1:

Heat treatment is applied as a preliminary step before mechanical support removal. This thermal process selectively weakens the interface strength, enabling the use of simple support profiles without compromising either interface strength during manufacturing or ease of removal afterward

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The heat treatment process changes the physical parameters of the interface region, reducing its strength through thermal effects. This parameter change allows the interface to be strong during manufacturing but easy to separate during removal, resolving the contradiction between these two requirements

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If sharp cutting tools with considerable force are used for support removal, then support removal effectiveness is improved, but component surface damage increases

Engineering Contradiction:
Improvesupport removal effectivenessVSAvoidcomponent surface quality
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

Heat treatment is applied before mechanical support removal to pre-weakens the interface. This preliminary action reduces the force required for support removal, enabling the use of less aggressive cutting tools that preserve component surface quality while maintaining removal effectiveness

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 thermal pulse method effectively reduces the strength of the interface without affecting the material properties of the component, facilitating easier support removal and improving fatigue properties, while subsequent thermal pulses can enhance surface finish by reducing roughness.

Implementation Method 1

exposing the component and support structure to at least one thermal pulse so as to weaken or break the interface(s) between the support structure and component

Methodology Applied
Scientific EffectThermal heating: Heating

Data Source

PatentUS11059103B2Additive manufacturing
Publication Date: 2021.07.13 SIEMENS ENERGY GLOBAL GMBH & CO KG
  • US11059103B2 patent drawing
  • US11059103B2 patent drawing
  • US11059103B2 patent drawing

AI summary

A method of additive manufacturing metallic components, the method includes: forming a component in a layer by layer process, the component being formed integrally with at least one non-perforated support structure to be separated from the component after the layer by layer process, the support structure being formed with at least one wall that is non-perforated; and wherein after completion of the layer by layer process, the method includes exposing the component and support structure to at least one thermal pulse so as to weaken, or break, the interface(s) between the support structure and component prior to removal of the support.