Al-Co-Cr-Fe-Ni-Si Alloy Cladding for Wear and Corrosion Resistance

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Solution Overview

Problem

Current metal bonding layers in nickel-based superalloys for engine turbines face issues with thermal barrier coating peeling due to thermally grown oxide thickness and corrosion from high halogen-free glass fiber plastics, leading to wear and corrosion of injection components.

Innovation Solution

An aluminum-cobalt-chromium-iron-nickel-silicon alloy powder with specific atomic percentages is produced using inert gas spray atomization and cladded onto substrates via thermal spray technology, forming a high-temperature, wear-resistant, and corrosion-resistant layer that reduces reaction rates and improves bonding strength.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a metal bonding layer is used between nickel-based superalloy and ceramic thermal barrier layer, then bonding strength is improved, but thermally grown oxide thickness increases causing thermal barrier coating to peel off

Engineering Contradiction:
Improvebonding strengthVSAvoidcoating stability
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent modifies the chemical composition parameters of the bonding layer by incorporating specific elements (Al, Si, Ti, B) in controlled amounts to optimize both bonding strength and oxidation resistance, preventing TGO overgrowth while maintaining interface stability

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The bonding layer is designed as a composite material system combining nickel-based superalloy with specific alloying elements (Al, Si, Ti, B) to achieve multiple functions: strong bonding to both substrate and ceramic, controlled oxidation resistance, and thermal barrier properties

Inventive Principle:
Principle #40Composite materials

2Reliability

If halogen-free high glass fiber plastic parts are produced with inorganic flame retardants, then fire safety is improved, but injection components suffer severe corrosion

Engineering Contradiction:
Improvefire safetyVSAvoidcorrosion
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The alloy cladding layer acts as an intermediary protective barrier between the injection component and the corrosive halogen-free plastic environment, preventing direct contact and chemical interaction while allowing the plastic to maintain its fire safety properties

Inventive Principle:
Principle #24Intermediary (Mediator)

3Strength

If glass fiber is added to plastic parts to improve strength, then mechanical strength is improved, but injection components suffer severe wear

Engineering Contradiction:
Improveplastic part strengthVSAvoidwear
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

The alloy cladding layer serves as a protective intermediary layer that prevents direct contact between the injection component and glass fibers in the plastic, thereby preventing wear while allowing the plastic parts to maintain their enhanced mechanical strength

Inventive Principle:
Principle #24Intermediary (Mediator)

4Reliability

If aluminum content in the alloy is increased to improve oxidation resistance, then high-temperature oxidation resistance is improved, but hot cracking tendency increases

Engineering Contradiction:
Improveoxidation resistanceVSAvoidcracking resistance
Core Design Contradiction:
ReliabilityVSStability of the object's composition

Solution Approach 1:

The patent optimizes the aluminum content within a specific range (3-13 at%) rather than maximizing it, and balances it with other alloying elements (Si, Ti, B) to achieve both oxidation resistance and hot cracking resistance through controlled compositional parameters

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 resulting alloy cladding exhibits enhanced high-temperature hardness, wear resistance, and corrosion resistance, extending the service life of injection components and maintaining high bonding strength with substrates.

Implementation Method 1

cladded onto substrates via thermal spray technology

Methodology Applied
Scientific EffectThermal spray: Plasma Spray

Data Source

PatentUS11104981B2Aluminum-cobalt-chromium-iron-nickel-silicon alloy, powder and cladding thereof
Publication Date: 2021.08.31 IND TECH RES INST
  • US11104981B2 patent drawing
  • US11104981B2 patent drawing
  • US11104981B2 patent drawing

AI summary

An aluminum-cobalt-chromium-iron-nickel-silicon alloy has atomic percentages of 4-12 at % aluminum, 15-25 at % cobalt, 25-35 at % chromium, 4-8 at % iron, 15-25 at % nickel, 10-25 at % silicon, wherein the atomic percentage of aluminum plus silicon is between 18-32 at %. The disclosure applies the alloy design to develop a low-aluminum Al—Co—Cr—Fe—Ni—Si alloy composition, and has high-temperature hardness, high wear resistance, corrosion resistance and high temperature oxidation resistance.