Turbomachine Blade Reinforcement via Superplastic Wire Preform

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

The production of metal reinforcements for turbine engine blades, particularly those with complex geometric shapes, is costly and time-consuming due to the need for complex tools and numerous rework operations, which complicates the manufacturing process and increases material costs.

Innovation Solution

A method involving the creation of a three-dimensional metal structure using an insert and metal wires that can be superplastically formed and diffusion welded, followed by hot pressing to produce a compact, porosity-free metal part, simplifying the manufacturing process and reducing costs by eliminating the need for extensive machining.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If metal reinforcement is produced by milling from a block of material, then the part achieves required geometric precision and strength, but production costs increase and manufacturing time extends

Engineering Contradiction:
Improvegeometric precisionVSAvoidproduction cost
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The patent applies preliminary action by creating a preform structure before final forming. Metal wires are arranged in a three-dimensional configuration matching the desired reinforcement geometry, and an insert is positioned within the wire assembly before hot pressing. This pre-arranged structure reduces the complexity of subsequent machining operations while ensuring geometric precision is achieved during the forming process itself.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent utilizes parameter changes by transforming the physical state of metal wires through hot pressing at elevated temperatures and pressures. The metal wires transition from a loose three-dimensional arrangement to a densely packed, sintered structure with properties approaching those of forged material. This parameter change enables the production of complex geometries without extensive machining, reducing both cost and manufacturing time while maintaining geometric precision.

Inventive Principle:
Principle #35Parameter changes

2Manufacturing precision

If complex tools and numerous rework operations are used for producing metal reinforcements, then required geometric accuracy is achieved, but device complexity and manufacturing time increase

Engineering Contradiction:
Improvegeometric accuracyVSAvoidtool complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent applies preliminary action by pre-assembling the metal reinforcement structure in its near-final configuration before hot pressing. The three-dimensional arrangement of metal wires and insert is constructed to match the target geometry, eliminating the need for complex post-forming tools and rework operations. This preliminary structuring ensures geometric accuracy is built-in rather than achieved through multiple machining steps.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent extracts the geometric complexity from the manufacturing process by directly forming the reinforcement in its final shape through hot pressing of the prearranged wire structure. This eliminates the need for separate complex machining tools and multiple rework operations that would otherwise be required to achieve the same geometric accuracy, thereby reducing device complexity.

Inventive Principle:
Principle #2Taking out (Extraction)

3Manufacturing precision

If extensive machining operations are performed on metal reinforcement, then required geometric requirements are met, but production time and material costs increase

Engineering Contradiction:
Improvegeometric requirementsVSAvoidproduction time
Core Design Contradiction:
Manufacturing precisionVSLoss of time

Solution Approach 1:

The patent utilizes parameter changes by applying heat and pressure during hot pressing to transform the metal wire structure into a dense, mechanically sound component with the desired geometry. This thermal-mechanical processing achieves geometric requirements directly during forming, eliminating the need for extensive subsequent machining operations and significantly reducing production time while meeting geometric specifications.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent applies preliminary action by pre-configuring the metal wires and insert in their final geometric arrangement before hot pressing. This preliminary structuring ensures that the reinforcement achieves required geometric requirements directly from the forming process, minimizing or eliminating the need for time-consuming machining operations afterward.

Inventive Principle:
Principle #10Preliminary 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

This method significantly reduces production costs and time while allowing for the creation of metal parts with complex geometries, such as turbine engine blade reinforcements, by simplifying the manufacturing process and ensuring parts meet strict mass and geometric requirements.

Implementation Method 1

a step of producing a three-dimensional metal structure consisting of an insert having properties allowing superplastic forming and diffusion welding and by a plurality of metal wires, each metal wire of said plurality encircling the periphery of said insert

Methodology Applied
Scientific EffectDiffusion welding: Diffusion Welding

Implementation Method 2

The hot pressing process is an isostatic pressing or compacting process (HIP for Hot Isostatic Pressing in English) making it possible to obtain a compact and porosity-free part by the combination of plastic deformation, creep and diffusion welding

Methodology Applied
Scientific EffectPlastic deformation: Plasticity

Implementation Method 3

The hot pressing process is an isostatic pressing or compacting process (HIP for Hot Isostatic Pressing in English) making it possible to obtain a compact and porosity-free part by the combination of plastic deformation, creep and diffusion welding

Methodology Applied
Scientific EffectCreep: Creep

Implementation Method 4

an insert having properties allowing superplastic forming and diffusion welding

Methodology Applied
Scientific EffectSuperplasticity: Superplasticity

Data Source

PatentEP2681004B1Method for producing a metal component such as a turbomachine blade edge reinforcement piece
Publication Date: 2018.11.28 SAFRAN AIRCRAFT ENGINES SAS
  • EP2681004B1 patent drawingFigure 1~3
  • EP2681004B1 patent drawingFigure 4a~4c
  • EP2681004B1 patent drawingFigure 5~6

AI summary

The present invention relates to a method for producing a metal component such as a metal turbomachine blade reinforcement, comprising, in succession: a step of producing a three-dimensional metal structure (310) consisting of an insert (301) that has properties allowing superplastic forming and diffusion welding and consisting of a plurality of metal wires (302) surrounding the periphery of said insert (301), said metal structure (310) forming a preform of said metal component (30); a step of positioning said metal structure (310) in a forming tool; and a step of hot-pressing said three-dimensional metal structure (310), causing the agglomeration of said metal structure (310) so as to obtain said compact metal component.