Abrasive Blade Tip Coating With Multi-Grit Wear Retention

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Solution Overview

Problem

Turbomachinery components experience rapid depletion of abrasive blade tip coatings due to varying radial interaction rates during engine operation, leading to unwanted contact between base material and abradable seals, causing damage and inefficiency.

Innovation Solution

A composite abrasive coating is applied to turbine engine components, comprising a strike layer, base layer, tack layer, and an overplate layer with varying grit particle sizes, where larger grit particles are embedded and smaller grit particles are interspersed within a matrix, forming channels for debris removal.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a conventional abrasive coating is applied to blade tips, then cutting capability is provided during initial operation, but the coating depletes rapidly during high radial interaction conditions (e.g., bird strike), causing unwanted contact between base material and abradable seal

Engineering Contradiction:
Improvecoating retentionVSAvoidcoating service life
Core Design Contradiction:
ReliabilityVSDuration of action of moving object

Solution Approach 1:

The abrasive coating is segmented into multiple functional layers: a strike layer for initial cutting, a base layer for support, a tack layer for particle adhesion, and an overplate layer for protection and debris management. This segmentation allows each layer to perform its specific function optimally, preventing rapid depletion while maintaining cutting capability throughout the coating's service life.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The coating uses a composite structure combining different materials with complementary properties: metallic matrix materials (nickel, cobalt, or MCrAlY) provide toughness and adhesion, while abrasive particles (cubic boron nitride, silicon carbide, aluminum oxide, or diamond) provide cutting capability. This composite approach ensures the coating maintains both hardness for cutting and toughness for retention under varying radial interaction conditions.

Inventive Principle:
Principle #40Composite materials

2Strength

If the abrasive coating is made harder to maintain cutting capability, then wear resistance improves, but the coating becomes more susceptible to rapid depletion during high radial interaction events

Engineering Contradiction:
Improvecutting capabilityVSAvoidcoating retention under transient conditions
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

Different regions of the coating have different properties optimized for their specific functions: the strike layer contains high concentrations of abrasive particles for maximum cutting capability, while the overplate layer provides a tougher, more protective surface that resists rapid depletion during transient high-radial-interaction events. The tack layer provides localized adhesion to ensure particle retention at the interface with the abradable seal.

Inventive Principle:
Principle #3Local quality

3Ease of manufacture

If the coating structure is simplified to improve manufacturing, then ease of application increases, but the ability to maintain cutting capability over multiple operating cycles deteriorates

Engineering Contradiction:
Improvecoating application simplicityVSAvoidservice life over operating cycles
Core Design Contradiction:
Ease of manufactureVSDuration of action of moving object

Solution Approach 1:

The multi-layer coating structure ensures continuous cutting capability throughout the service life by providing a strike layer for initial cutting action, followed by the base and tack layers that maintain particle adhesion, and the overplate layer that protects against depletion. This continuous structure allows the coating to maintain its cutting function across multiple operating cycles without requiring simplification.

Inventive Principle:
Principle #20Continuity of useful action

4Strength

If larger abrasive particles are used to enhance cutting capability, then wear resistance improves, but the coating becomes more prone to depletion during high radial interaction rates

Engineering Contradiction:
Improveabrasive cutting capabilityVSAvoidabrasive particle depletion
Core Design Contradiction:
StrengthVSLoss of substance

Solution Approach 1:

Smaller abrasive particles are embedded within and surrounded by the matrix material and larger abrasive particles, creating a nested structure where smaller particles fill the spaces between larger particles. This nesting maximizes the total abrasive content while ensuring proper distribution and retention, allowing the coating to maintain cutting capability without excessive depletion during high radial interaction events.

Inventive Principle:
Principle #7Nested doll (Nesting)

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 coating enhances wear resistance and retention of abrasive particles, maintaining cutting capability over multiple operating cycles, reducing the need for recoating and minimizing damage to abradable seals.

Implementation Method 1

the matrix material bonds to and partially surrounds the first grit particles

Methodology Applied
Scientific EffectAdhesion: Adhesive

Implementation Method 2

the blade tips act as an abrading component and the seal can be provided as an abradable seal. Generally, the blade tip is harder and more abrasive than the seal. Thus, the blade tips will abrade or cut into the abradable seal

Methodology Applied
Scientific EffectAbrasion: Abrasion

Data Source

PatentUS12473834B2Wear resistant coating, method of manufacture thereof and articles comprising the same
Publication Date: 2025.11.18 RTX CORP
  • US12473834B2 patent drawing
  • US12473834B2 patent drawing
  • US12473834B2 patent drawing

AI summary

An abrasive coating for a substrate comprises a strike layer is formed on a substrate top surface; a base layer is coupled to the strike layer; a tack layer is coupled to the base layer, wherein the tack layer is configured to adhere first grit particles to the base layer; a plurality of first grit particles are adapted to be coupled to the tack layer, a plurality of second grit particles are placed between each of the plurality of first grit particles, the second grit particles having a nominal size smaller than the first grit particles; and an overplate layer comprising a matrix material is bonded to the tack layer; the matrix material envelops the second grit particles and bonds and partially surrounds the first grit particles, wherein the first grit particles extend above the overplate layer.