Casting Core for Baffle Landings in Airfoil Investment Casting

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Solution Overview

Problem

High manufacturing tolerances in the formation of baffle landings for gas turbine engine airfoils lead to variability in the gap between baffles and airfoils, affecting cooling air effectiveness and installation complexity.

Innovation Solution

A method and casting core approach where the baffle landings are formed using a casting core instead of wax, reducing tolerances and variability, ensuring precise placement and improved cooling efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If wax is used to form baffle landings in investment casting, then the manufacturing process is simple and cost-effective, but the manufacturing precision and tolerance control deteriorate

Engineering Contradiction:
Improvemanufacturing process simplicityVSAvoidbaffle landing tolerance
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

The patent changes the material parameter from wax to ceramic slurry for forming baffle landings. Ceramic slurry allows for tighter tolerance control and more precise dimensional accuracy compared to wax, directly addressing the manufacturing precision issue while maintaining compatibility with the investment casting process

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent introduces a ceramic slurry intermediary layer that is applied to the wax pattern before shell formation. This intermediary layer provides the precise baffle landing geometry and tolerance control, while the wax pattern continues to serve its function as the basic pattern form, combining the advantages of both materials

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of manufacture

If traditional wax-based investment casting is used for baffle landings, then the production cost is low, but the cooling air effectiveness deteriorates due to gap variability

Engineering Contradiction:
Improveproduction costVSAvoidcooling air effectiveness
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent applies ceramic slurry (a fluid-like material) to the wax pattern using a spray or dip application method. This pneumatic/hydraulic application ensures uniform thickness and precise replication of the baffle landing geometry, reducing gap variability and improving cooling air effectiveness

Inventive Principle:
Principle #29Pneumatics and hydraulics

Solution Approach 2:

The patent changes the physical and chemical parameters of the pattern material from wax to ceramic slurry. Ceramic slurry provides better dimensional stability, lower shrinkage, and more consistent surface finish, all of which contribute to reduced gap variability and improved cooling effectiveness

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If wax is used to form baffle landings, then the manufacturing process is straightforward, but the installation complexity increases due to variability in baffle placement

Engineering Contradiction:
Improveprocess straightforwardnessVSAvoidinstallation complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The patent performs preliminary action by forming the baffle landings with precise geometry and tolerance during the casting process itself. The ceramic slurry is applied to the wax pattern before shell formation, ensuring that the baffle landings are pre-formed with accurate dimensions and positions, eliminating the need for post-casting adjustments during installation

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS11707779B2Method and casting core for forming a landing for welding a baffle inserted in an airfoil
Publication Date: 2023.07.25 RTX CORP
  • US11707779B2 patent drawing
  • US11707779B2 patent drawing
  • US11707779B2 patent drawing

AI summary

A method and casting core for forming a landing for welding a baffle inserted into an airfoil are disclosed, wherein the baffle landing of the blade or vane is formed in investment casting by the casting core rather than by wax, reducing tolerances and variability in the location of the baffle inserted into the cooling cavity of airfoil when the baffle is welded to the baffle landing.