Hafnium-Optimized Nickel Superalloy for Turbomachine Oxidation Resistance

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Solution Overview

Problem

Existing nickel-based superalloys used in turbomachines lack optimal oxidation resistance, which is crucial for high-temperature applications in the aeronautical field.

Innovation Solution

A nickel-based superalloy composition with a hafnium content optimized between 500 ppm and 1100 ppm, optionally including niobium, carbon, zirconium, or boron, providing improved oxidation resistance without the need for additional coatings.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If hafnium content is increased to improve oxidation resistance, then oxidation resistance is improved, but excessive hafnium oxide formation decreases oxide layer toughness and protective role

Engineering Contradiction:
Improveoxidation resistanceVSAvoidexcessive hafnium oxide formation
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The patent applies parameter changes by precisely controlling the hafnium content within the range of 500-1100 ppm. This optimization ensures sufficient hafnium oxide formation for anchoring the oxide layer and blocking cation diffusion, while preventing excessive oxide formation that would compromise interface toughness. The specific parameter range resolves the contradiction between needing enough hafnium for protection and avoiding excess that would harm the oxide layer quality.

Inventive Principle:
Principle #35Parameter changes

2Object-generated harmful factors

If hafnium content is decreased to reduce oxide formation, then excessive oxide formation is avoided, but oxidation resistance deteriorates due to insufficient oxide layer anchoring

Engineering Contradiction:
Improveoxide layer qualityVSAvoidoxidation resistance
Core Design Contradiction:
Object-generated harmful factorsVSReliability

Solution Approach 1:

The patent establishes that hafnium content must be maintained within 500-1100 ppm to ensure sufficient oxide layer anchoring and cation blocking capability. Below this range, the oxide layer lacks proper anchoring and protective function. The parameter optimization ensures minimum effective concentration while avoiding the harmful effects of excess hafnium.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If additional coatings are applied to improve oxidation resistance, then oxidation resistance is improved, but device complexity and manufacturing cost increase

Engineering Contradiction:
Improveoxidation resistanceVSAvoidcoating requirements
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent enables the superalloy to serve itself by incorporating sufficient hafnium (500-1100 ppm) that allows the base material to form its own protective oxide layer without requiring additional coatings. The optimized composition provides intrinsic oxidation resistance, eliminating the need for extra protective coatings and simplifying the overall device structure.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

By changing the chemical composition parameter of hafnium content to the optimized range, the patent fundamentally alters the oxidation behavior of the superalloy, enabling it to form protective oxides spontaneously during service without requiring external coating applications.

Inventive Principle:
Principle #35Parameter changes

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 optimized hafnium content enhances oxidation resistance, maintaining mechanical properties comparable to AM-1, allowing use in engine parts without additional coatings and improving the protective oxide layer formation.

Implementation Method 1

the oxide HfO2 does not fulfill the role of a structure anchoring the oxide layer on the superalloy surface

Methodology Applied
Scientific EffectOxidation: Oxidation

Implementation Method 2

the hafnium does not sufficiently block the outward diffusion of cations

Methodology Applied
Scientific EffectDiffusion: Diffusion

Data Source

PatentUS12392256B2Superalloy turbomachine part with an optimized hafnium content
Publication Date: 2025.08.19 SAFRAN AIRCRAFT ENGINES SAS
  • US12392256B2 patent drawing
  • US12392256B2 patent drawing

AI summary

A turbomachine part includes a nickel-based superalloy substrate including, in mass content, 5.0% to 8.0% cobalt, 6.5% to 10% chromium, 0.5% to 2.5% molybdenum, 5.0% to 9.0% tungsten, 6.0% to 9.0% tantalum, 4.5% to 5.8% aluminum, hafnium in a mass content between 500 ppm and 1100 ppm, and optionally including niobium in a mass content less than or equal to 1.5%, and optionally at least one of carbon, zirconium and boron each in a mass content less than or equal to 100 ppm, the remainder being composed of nickel and unavoidable impurities.