Turbomachine Blade Reinforcement via Superplastic Wire Preform
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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
Engineering 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
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.
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.
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
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.
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.
3Manufacturing precision
If extensive machining operations are performed on metal reinforcement, then required geometric requirements are met, but production time and material costs increase
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.
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.
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
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
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
Implementation Method 4
an insert having properties allowing superplastic forming and diffusion welding
Data Source
Figure 1~3
Figure 4a~4c
Figure 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.