Ceramic Turbine Part With Density Gradient Structure
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Solution Overview
Problem
Current manufacturing techniques for turbine engine parts, especially ceramic materials, face challenges in withstanding high temperatures, mechanical stress, and efficient cooling, particularly in the root region of rotating parts like turbine rotor blades, where defects and thermal gradients can lead to structural weaknesses and residual stress.
Innovation Solution
A ceramic part with a density gradient structure, featuring a low-porosity base and a high-porosity core, manufactured using powder sintering with a laser or electron beam, allowing for reduced mechanical stress and integrated fluid channels for cooling without extensive machining.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Strength
If monolithic ceramic material is used throughout the part, then structural strength is maintained, but mechanical stress and weight increase in regions where it is not needed
Solution Approach 1:
The patent applies local quality by creating a density gradient within the ceramic part, where the base region has high density (low porosity) for structural strength, while the wall regions have progressively lower density (higher porosity) to reduce weight. This is achieved through controlled powder deposition and selective sintering, resulting in a part where material properties are optimized for each specific location's functional requirements.
2Reliability
If dense ceramic material is used throughout, then defect probability is reduced, but manufacturing complexity and machining requirements increase
Solution Approach 1:
The patent intentionally incorporates controlled porosity in the wall regions of the ceramic part. This porous structure reduces the volume of material that could contain critical defects, thereby improving reliability. The porous walls also eliminate the need for extensive machining to create cooling channels, as the porosity itself can serve as fluid circulation pathways, significantly simplifying manufacturing.
3Ease of manufacture
If uniform density is maintained throughout the part, then manufacturing simplicity is preserved, but cooling efficiency and stress distribution deteriorate
Solution Approach 1:
The patent implements local quality through a density gradient where the base remains dense for structural support while the walls have controlled porosity for cooling. The porous structure in the walls creates natural pathways for cooling fluid circulation, improving heat dissipation without requiring complex machined channels. This gradient structure is achieved through controlled powder deposition and selective sintering processes.
4Weight of moving object
If high porosity is used to reduce weight, then stress reduction is achieved, but structural integrity and defect resistance worsen
Solution Approach 1:
The patent resolves this contradiction by applying local quality through spatially varying porosity. The base region maintains high density (low porosity) to provide structural integrity and resistance to critical defects, while the wall regions have controlled porosity to reduce weight. The gradual transition from dense base to porous walls ensures that structural strength is maintained where needed while achieving weight reduction in less critical regions.
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
The density gradient structure reduces mechanical stress and the likelihood of critical defects, while the porous nature enables efficient cooling without machining, enhancing the structural integrity and performance of turbine engine components.
Implementation Method 1
the material is in the form of a powder that is heated under the action of a laser beam or electron beam
Implementation Method 2
the material is in the form of a powder that is heated under the action of a laser beam or electron beam
Implementation Method 3
powder sintering, which is a method for directly producing mechanical parts or other objects from powders
Data Source
AI summary
A part made of a ceramic material, including a portion forming a base and a portion forming a wall, wherein the base consists of a low-porosity ceramic material and the wall is obtained by powder sintering and includes an envelope and a core, the core being within the envelope, the porosity of the core being higher than that of the base and increasing the further it is from the base.

