Gas Turbine Masking Shells for High-Temperature Coating Control

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Solution Overview

Problem

Existing masking systems for gas turbine components are either susceptible to damage at high temperatures or require lengthy and laborious fabrication processes, leading to improper coating application and potential damage to the components during high-temperature finishing processes.

Innovation Solution

The development of additively manufactured masking systems with overlapping shell halves and protrusions that securely retain and protect specific areas of gas turbine components, allowing for controlled coating distribution and application, using interlocking clips for secure attachment and customizable protrusions for precise coating control.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional masking systems are used, then they can be fabricated, but they are susceptible to damage at high temperatures and require lengthy fabrication processes

Engineering Contradiction:
Improvemasking system durabilityVSAvoidfabrication time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent changes the manufacturing parameter from traditional fabrication methods to additive manufacturing. This enables the masking system to be produced in a single continuous process without lengthy assembly operations, reducing fabrication time while maintaining high-temperature durability through the inherent properties of additively manufactured structures

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The masking system utilizes composite material structures created through additive manufacturing, combining materials that can withstand high temperatures while maintaining structural integrity. The multi-material capability of additive manufacturing allows integration of temperature-resistant materials directly into the masking system design

Inventive Principle:
Principle #40Composite materials

2Manufacturing precision

If masking systems are designed to protect specific areas, then coating application can be controlled, but the system complexity increases

Engineering Contradiction:
Improvecoating application precisionVSAvoidmasking system structure
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The masking system is segmented into multiple functional components including shell halves, protrusions, and mounting portions. Each segment can be independently designed and manufactured, then assembled to create the complete masking system. This segmentation allows for precise control of coating application areas while managing complexity through modular design

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The masking system incorporates adjustable and removable components, particularly the protrusions that can be positioned to control coating distribution. The dynamic capability of adjusting masking positions allows precise coating control without requiring overly complex fixed structures for every possible application scenario

Inventive Principle:
Principle #15Dynamics

3Manufacturing precision

If protrusions are added to control coating distribution, then coating precision is improved, but the risk of damage to the masking system increases

Engineering Contradiction:
Improvecoating distribution controlVSAvoidmasking system damage risk
Core Design Contradiction:
Manufacturing precisionVSObject-affected harmful factors

Solution Approach 1:

The protrusions are designed as removable and replaceable components rather than fixed permanent structures. This dynamic design allows the protrusions to be easily replaced if damaged or worn, maintaining coating distribution control precision while reducing the overall risk to the masking system through component replaceability

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The masking system incorporates protective features in the shell structure that cushion and protect the protrusions from damage during handling and the coating process. The robust shell design absorbs and distributes stresses that could otherwise damage the protrusions, maintaining their coating control functionality

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Data Source

PatentUS20250262640A1Masking Systems
Publication Date: 2025.08.21 CHROMALLOY GAS TURBINE LLC
  • US20250262640A1 patent drawing
  • US20250262640A1 patent drawing
  • US20250262640A1 patent drawing

AI summary

A masking system for selectively masking a component includes a first shell half and a second shell half. The second shell half is configured to be secured to the first shell half such that at least a portion of the first shell half overlaps the second shell half when the component is retained by the masking system. A protrusion extends from one of the first shell half and the second shell half. The protrusion is configured to cover an edge of the component.