Airfoil Edge ECM Using Dielectric Shields Instead of Complex Cathodes

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Solution Overview

Problem

Traditional precision electro-chemical machining methods are ineffective in forming complex, small-sized leading and trailing edges of airfoils, such as those found in gas turbine engines, due to high costs and long lead times associated with complex tooling.

Innovation Solution

The method involves using non-conductive shields, such as plastic, placed between the workpiece and electrode to concentrate current distribution on the edges, allowing for precise formation of leading and trailing edges through electro-chemical machining.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If traditional precision ECM methods use complex cathode shapes to form complex airfoil edges, then manufacturing precision is improved, but device complexity and cost increase significantly

Engineering Contradiction:
Improveedge formation precisionVSAvoidcathode complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

A simple planar cathode is used in conjunction with a dielectric shield positioned between the cathode and workpiece. The shield acts as an intermediary that concentrates and directs the electrical discharge current to the specific edge regions requiring machining, eliminating the need for complex cathode geometries while achieving precise edge formation

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The dielectric shield creates localized regions of high current density at the leading and trailing edges of the airfoil by positioning it between the planar cathode and workpiece. This concentrates the machining action precisely where needed (local quality) while the cathode itself remains simple and uniform

Inventive Principle:
Principle #3Local quality

2Manufacturing precision

If traditional precision ECM methods use complex cathode tooling to form small-sized edges, then manufacturing precision is improved, but lead time increases

Engineering Contradiction:
Improvesmall edge formation precisionVSAvoidtooling lead time
Core Design Contradiction:
Manufacturing precisionVSLoss of time

Solution Approach 1:

The dielectric shield serves as a temporary, easily fabricable intermediary component that directs current to small edge regions. Unlike complex permanent cathode tooling, the shield can be quickly manufactured or adjusted, significantly reducing tooling lead time while maintaining precision for small-sized edges

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The machining process is segmented into two stages: first using a simple planar cathode to create the general airfoil shape, then using the dielectric shield to precisely form the small leading and trailing edges. This segmentation allows each stage to use appropriately simple tooling, reducing overall lead time

Inventive Principle:
Principle #1Segmentation

3Productivity

If traditional ECM methods are used for airfoil manufacturing, then productivity is maintained, but manufacturing precision for edges deteriorates

Engineering Contradiction:
Improveairfoil manufacturing productivityVSAvoidedge formation precision
Core Design Contradiction:
ProductivityVSManufacturing precision

Solution Approach 1:

The dielectric shield is introduced as an intermediary that enhances edge formation precision without significantly impacting productivity. The shield can be easily positioned and removed, allowing the process to maintain high productivity while achieving superior edge precision that traditional ECM cannot deliver

Inventive Principle:
Principle #24Intermediary (Mediator)

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

This approach enables the efficient and cost-effective formation of complex airfoil edges by deflecting current to specific areas, reducing tooling complexity and lead times while maintaining precision.

Implementation Method 1

One popular method of manufacturing airfoils is electro-chemical machining (ECM). In a common ECM system, a conductive workpiece is machined to form the airfoil. A voltage is connected to the workpiece and to an electrode (cathode). The workpiece is in a chamber with an electrolytic fluid.

Methodology Applied
Scientific EffectElectro-chemical machining: Electrolysis

Implementation Method 2

providing a shield in a current distribution path between a workpiece and an electrode, with the shield concentrating current distribution upon an end of the workpiece

Methodology Applied
Scientific EffectCurrent concentration: Electrical Resistance

Data Source

PatentEP4101950A1Method for creating airfoil leading and trailing edges
Publication Date: 2022.12.14 RTX CORP
  • EP4101950A1 patent drawingFigure 1~2A
  • EP4101950A1 patent drawingFigure 2B~3
  • EP4101950A1 patent drawing

AI summary

A method of forming a component using electro-chemical machining includes the steps of providing a shield in a current distribution path between a workpiece and an electrode, with the shield concentrating current distribution upon an end of the workpiece.