Nickel Aluminide Coating via Low-Temperature Diffusion

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Solution Overview

Problem

Current methods for producing nickel aluminide coatings on materials like Nb—Si alloys face challenges such as the use of halogenated gases, high temperatures, high pressures, and the inability to achieve homogeneous coatings on complex shapes, leading to oxidation issues and coating cracking due to mismatched coefficients of expansion.

Innovation Solution

A method involving the deposition of nickel on a metal substrate, followed by the application of an aluminium foil and heat treatment below the melting temperature of aluminium under reduced pressure, to form a nickel aluminide coating without halogenated gases or high pressures, allowing for a multilayer coating with adapted coefficients of expansion.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If pack cementation with halogenated activator is used to deposit silicon-based coating, then oxidation resistance is improved, but harmful halogenated gases are formed that degrade the microstructure

Engineering Contradiction:
Improveoxidation resistanceVSAvoidhalogenated gases
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The patent removes halogenated activators from the pack cementation process entirely, extracting the harmful element while maintaining the protective coating function through alternative chemistry (silicon powder with aluminum powder mixture)

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent uses simple, inexpensive silicon and aluminum powders as consumable reactants that form the protective coating through controlled reaction, replacing expensive and harmful halogenated chemicals

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

2Stability of the object's composition

If high temperature heat treatment is used to form nickel aluminide coating, then coating stability is improved, but substrate deformation and energy consumption increase

Engineering Contradiction:
Improvecoating stabilityVSAvoidheat treatment temperature
Core Design Contradiction:
Stability of the object's compositionVSTemperature

Solution Approach 1:

The patent changes the temperature parameter from conventional high temperature (above aluminum melting point) to low temperature (below aluminum melting point, specifically 500-650°C), achieving coating formation through controlled diffusion rather than melting

Inventive Principle:
Principle #35Parameter changes

3Manufacturing precision

If conventional diffusion coating methods are used, then coating homogeneity is improved, but complex shaped substrates cannot be coated uniformly

Engineering Contradiction:
Improvecoating homogeneityVSAvoidapplicability to complex shapes
Core Design Contradiction:
Manufacturing precisionVSAdaptability or versatility

Solution Approach 1:

The patent segments the coating process into distinct layers (nickel deposition layer, intermediate reaction layer, outer nickel aluminide layer) that can form independently on complex geometries, allowing uniform coverage of intricate shapes

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces an intermediate nickel deposition layer as a mediator between the substrate and the aluminum foil, facilitating controlled reaction and ensuring uniform coating distribution on complex surfaces

Inventive Principle:
Principle #24Intermediary (Mediator)

4Manufacturing precision

If high pressure is applied during coating process, then coating density is improved, but equipment complexity and operational difficulty increase

Engineering Contradiction:
Improvecoating densityVSAvoidpressure control equipment
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent replaces mechanical pressure application with controlled thermal diffusion and chemical reaction processes, achieving dense coating formation through atomic diffusion rather than external pressure

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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

This method enables the creation of a stable, uncracked nickel aluminide coating that provides improved oxidation resistance and can be applied to complex shapes without the need for high pressures or temperature gradients, while maintaining the substrate's integrity and allowing for local repairs.

Implementation Method 1

subjecting the assembly to heat treatment at a temperature below the melting temperature of aluminium, that is to say below 660.30° C., and under reduced pressure in order to cause a reaction between the aluminium and the nickel

Methodology Applied
Scientific EffectHeat treatment: Heat Treatment

Implementation Method 2

cause a reaction between the aluminium and the nickel and thus form a layer of nickel aluminide

Methodology Applied
Scientific EffectDiffusion: Diffusion

Data Source

PatentUS10549378B2Method for producing a nickel aluminide coating on a metal substrate, and part having one such coating
Publication Date: 2020.02.04 OFFICE NAT DETUDES & DE RECH AEROSPATIALES
  • US10549378B2 patent drawing
  • US10549378B2 patent drawing

AI summary

The invention relates to a method for producing a nickel aluminide coating on a metal substrate. The method includes the following steps: a) coating the substrate with a nickel deposit; b) applying an aluminum sheet onto the nickel deposit from step a) so as to form an assembly made up of the substrate coated with the nickel deposit and the aluminum sheet; and c) subjecting said assembly to heat treatment at a temperature that is lower than the melting point of aluminum, and at a low pressure so as to induce a reaction between the aluminum and the nickel and thus form a β-NiAl nickel aluminide layer mounted on a nickel layer. The invention is particularly of use for protecting the materials used in turbines of aircraft engines.