Ni-Base Superalloy Composition Using Hf Eutectics for SLM Crack Control

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Solution Overview

Problem

Ni-base superalloys with high γ′ phase content are susceptible to hot cracking during Selective Laser Melting (SLM), limiting their industrialization, especially in high-temperature applications like the gas turbine industry, as existing solutions either fail to completely prevent cracking or are economically unviable.

Innovation Solution

A Ni-base superalloy composition with increased Hafnium (Hf) content and controlled Hf/C ratio, along with SLM processing under a protective atmosphere, to form low-melting eutectics and reduce hot cracking susceptibility by enhancing the backfilling process during solidification.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If high γ′ phase content is used to strengthen the alloy, then mechanical strength is improved, but hot cracking susceptibility increases during SLM processing

Engineering Contradiction:
Improvemechanical strengthVSAvoidhot cracking susceptibility
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent modifies the chemical composition parameters of the Ni-base superalloy by reducing Si content to ≤0.01 wt.% and Zr content to ≤0.005 wt.%, while adjusting other alloying elements. This parameter change resolves the contradiction by preventing hot cracking during SLM while maintaining high γ′ phase content (5-11 wt.%) for mechanical strength

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent creates a composite microstructure consisting of γ matrix phase and γ′ precipitates with controlled distribution and morphology. By optimizing the composite structure through precise compositional control, the material achieves both high strength from γ′ precipitation hardening and resistance to hot cracking through the refined microstructure

Inventive Principle:
Principle #40Composite materials

2Reliability

If Si and Zr content is reduced to prevent hot cracking, then hot cracking susceptibility decreases, but alloy cost and mechanical properties are affected

Engineering Contradiction:
Improvehot cracking susceptibilityVSAvoidalloy composition control
Core Design Contradiction:
ReliabilityVSQuantity of substance

Solution Approach 1:

The patent establishes specific parameter ranges for alloying elements: Si ≤0.01 wt.%, Zr ≤0.005 wt.%, Al 3-6 wt.%, Ti 2-4 wt.%, with Hf 0.5-2 wt.% and C 0.05-0.2 wt.%. These parameter changes optimize the balance between hot cracking resistance and mechanical properties while controlling material costs through selective element reduction

Inventive Principle:
Principle #35Parameter changes

3Reliability

If processing temperature is increased to prevent cracking, then hot cracking susceptibility decreases, but equipment complexity and oxidation risk increase

Engineering Contradiction:
Improvehot cracking susceptibilityVSAvoidSLM equipment requirements
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent modifies the processing parameters by implementing a two-stage temperature protocol: initial heating to 1200±50°C for crack prevention, followed by controlled cooling and reheating to 900-1100°C for final densification. This parameter optimization reduces hot cracking while managing equipment complexity and oxidation through controlled thermal cycles

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent employs an inert or controlled atmosphere environment during SLM processing to prevent oxidation of the alloy at elevated temperatures. This atmosphere control enables high-temperature processing for crack prevention while mitigating oxidation risks through environmental management

Inventive Principle:
Principle #39Inert atmosphere (Inert environment)

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

Significantly reduces hot cracking susceptibility during SLM processing, enabling the production of crack-free parts with improved surface quality and geometric freedom, while maintaining mechanical properties and reducing material costs.

Implementation Method 1

Selective laser melting of γ′ (Gamma Prime) Ni3(Al,Ti) hardened Ni-base superalloys

Methodology Applied
Scientific EffectLaser melting: Laser

Implementation Method 2

forming low-melting eutectics and reducing hot cracking susceptibility by enhancing the backfilling process during solidification

Methodology Applied
Scientific EffectEutectic solidification: Phase Change

Data Source

PatentUS10941466B2Ni-base superalloy composition and method for SLM processing such Ni-base superalloy composition
Publication Date: 2021.03.09 GENERAL ELECTRIC TECH GMBH
  • US10941466B2 patent drawing
  • US10941466B2 patent drawing
  • US10941466B2 patent drawing

AI summary

A Ni-base superalloy composition to be used for powder-based additive manufacturing (AM) technology, such as selective laser melting (SLM) or electron beam melting (EBM). The cracking susceptibility during an AM process is considerably reduced by controlling the amount of elements, especially Hf, that form low-melting eutectics.