Thermal Barrier Coating Patterns for Engine Component Thermal Management

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Solution Overview

Problem

Internal combustion engine components face damage due to frictional wear and excessive heat, which can cause structural integrity degradation and failure, particularly from differential heat across components leading to uneven expansion and contraction.

Innovation Solution

Applying a thermal barrier coating with varying thickness and patterns to engine components to reduce temperature differences between areas, using materials like Zirconia or NiCrAlY, which acts as a thermal insulator to minimize heat transfer and prevent structural defects.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a thermal barrier coating is applied to engine components, then the component's resistance to excessive heat and differential heat damage is improved, but the device complexity and manufacturing complexity increase

Engineering Contradiction:
Improvecomponent structural integrityVSAvoidcoating application complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent applies thermal barrier coatings with varying thicknesses to different areas of the engine component surface. Specifically, the coating thickness is adjusted based on the local thermal characteristics and differential heat exposure of each region, allowing the component to better withstand thermal stresses while maintaining manufacturing feasibility through a targeted rather than uniform approach

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent employs composite material structures by combining the base engine component material with thermal barrier coating materials. This composite approach allows the component to leverage the thermal resistance properties of the coating materials (such as ceramics or ceramic-matrix composites) while maintaining the structural integrity and mechanical properties of the base metal component

Inventive Principle:
Principle #40Composite materials

2Object-affected harmful factors

If the coating thickness is increased to better insulate high-heat areas, then the temperature difference protection is improved, but the manufacturing precision and coating uniformity become more difficult to control

Engineering Contradiction:
Improvedifferential heat damageVSAvoidcoating thickness uniformity
Core Design Contradiction:
Object-affected harmful factorsVSManufacturing precision

Solution Approach 1:

The patent specifies different coating thickness ranges for different areas of the component surface. High-heat exposure areas receive thicker coatings (e.g., 0.5-2.0 mm) for better thermal insulation, while lower-heat areas receive thinner coatings (e.g., 0.1-0.5 mm). This local quality approach optimizes thermal protection where needed while maintaining manufacturing precision and avoiding excessive thickness that would be difficult to control uniformly across the entire component

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent controls the coating thickness as a key parameter, specifying precise thickness ranges for different regions. By carefully controlling this parameter within defined limits, the patent achieves optimal balance between thermal insulation performance and manufacturing feasibility, preventing both under-protection and over-engineering that would compromise manufacturing precision

Inventive Principle:
Principle #35Parameter changes

3Duration of action of stationary object

If thermal barrier coating is applied to reduce temperature differences, then the component lifespan is extended, but the cost and manufacturing time increase

Engineering Contradiction:
Improvecomponent lifespanVSAvoidcoating application ease
Core Design Contradiction:
Duration of action of stationary objectVSEase of manufacture

Solution Approach 1:

The patent applies thermal barrier coatings selectively to specific high-heat exposure areas rather than uniformly across the entire component surface. This targeted approach extends component lifespan in critical regions while reducing overall material usage, manufacturing time, and cost compared to full-surface coating, making the process more economically viable

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent applies thermal barrier coating to the extent necessary for protection - covering only the areas that require thermal protection rather than the entire component. This partial action approach provides sufficient protection to extend component lifespan while avoiding the excessive manufacturing effort and cost that would result from complete surface coating

Inventive Principle:
Principle #16Partial or excessive action

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 thermal barrier coating reduces temperature differences, minimizing stress fractures and extending the lifespan of engine components by maintaining structural integrity and reducing fatigue.

Implementation Method 1

a first coating of a thermal barrier coating applied to the first area, the first coating configured to reduce a rate of heat transfer into and out of the first area

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Data Source

PatentUS11933204B2Systems and methods for thermal barrier coatings to modify engine component thermal characteristics
Publication Date: 2024.03.19 CATERPILLAR INC
  • US11933204B2 patent drawing
  • US11933204B2 patent drawing
  • US11933204B2 patent drawing

AI summary

An engine component comprises one or more thermal barrier coatings applied to one or more areas of the engine component. The thermal barrier coatings reduce the temperature rate of change of the areas to which the thermal barrier coating is applied. Reducing the temperature rate of change can help reduce lattice structure damage caused by different temperatures in different areas of the engine component. The thermal barrier coating can be applied as a monolithic layer on a surface of the engine component or can be applied in different areas using patterns. The patterns allow for the tuning of the performance characteristics (temperature rate of change) of the areas of the engine component and can help reduce defect propagation, such as cracks, in the thermal barrier coating from one area of the thermal barrier coating to other areas of the thermal barrier coating.