Airfoil Masking System for Coating Precision

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Solution Overview

Problem

In gas turbine engines, precise control of working fluid flow across airfoil tip sections is challenging due to flow losses, clearance, temperature, and efficiency concerns, which are exacerbated by the need for accurate and efficient coating systems that are resistant to abrasion and thermal erosion.

Innovation Solution

A masking system for airfoils featuring locator and mask sections that conform to convex and concave surfaces, utilizing locator pins and retainer tabs to position and retain mask sections along the airfoil edges, ensuring accurate coverage and protection during coating processes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional coating systems are used on airfoil surfaces, then thermal and erosion resistance is improved, but coating accuracy and precision deteriorate due to difficulty in masking complex airfoil geometries

Engineering Contradiction:
Improvethermal and erosion resistanceVSAvoidcoating accuracy
Core Design Contradiction:
ReliabilityVSManufacturing precision

Solution Approach 1:

The mask is divided into multiple sections (first mask section for convex surface, second mask section for concave surface) that can be independently positioned and secured. Each mask section has dedicated positioning features (locator pins, retainer tabs) that enable precise placement on specific geometric features of the airfoil, thereby achieving accurate coating application on complex surfaces.

Inventive Principle:
Principle #1Segmentation

2Manufacturing precision

If complex masking systems are designed to achieve precise coating coverage, then coating accuracy is improved, but device complexity and processing time increase

Engineering Contradiction:
Improvecoating accuracyVSAvoidmasking system complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The positioning features (locator pins, retainer tabs) and masking surfaces are integrated into a unified mask structure that simultaneously addresses both positioning accuracy and coating coverage. The mask sections combine multiple functions (positioning, retaining, and masking) in single components, reducing the number of separate elements needed while maintaining precision.

Inventive Principle:
Principle #5Merging (Combining)

3Ease of manufacture

If conventional masking methods are used, then ease of manufacture is maintained, but processing time and scrap rates increase due to reworking

Engineering Contradiction:
Improvemasking system manufacturabilityVSAvoidprocessing time
Core Design Contradiction:
Ease of manufactureVSProductivity

Solution Approach 1:

The mask sections are pre-positioned using locator pins that engage with predetermined locations on the airfoil, and pre-secured using retainer tabs that engage with corresponding features. This preliminary positioning and securing action ensures accurate coating coverage from the first attempt, eliminating the need for reworking and reducing scrap rates.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS9121091B2Turbine airfoil mask
Publication Date: 2015.09.01 RTX CORP
  • US9121091B2 patent drawing
  • US9121091B2 patent drawing
  • US9121091B2 patent drawing

AI summary

A masking system for an airfoil comprises a locator for positioning along the trailing edge of the airfoil, and first and second mask sections. The first mask section has a trailing edge portion with locator pins for cooperating with a positioning tab on the locator to position the first mask section along the trailing edge of the airfoil, and a leading edge portion for extending around the leading edge of the airfoil to locate the first mask section along the convex surface. The second mask section has a retainer portion for cooperating with a retainer process on the first mask section to retain the second mask along the leading edge of the airfoil, and a flange portion for extending between the locator pins to locate the second mask along the concave surface.