Silicon Carbide Fabrication via Carbon Foam Infiltration

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing methods for fabricating silicon carbide structures for nuclear reactor applications face challenges in achieving desired geometries and dimensions due to the high strength and difficulty in machining these materials.

Innovation Solution

The technology involves using preformed carbon foam structures and a slurry mixture of silicon particles coated with silicon dioxide to penetrate and fill the pores of the carbon foam. Heat is applied to convert the carbon foam into silicon carbide, maintaining the original geometry and dimensions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If traditional machining methods are used to fabricate silicon carbide structures, then the material strength and integrity are maintained, but the manufacturing complexity and difficulty increase significantly

Engineering Contradiction:
Improvematerial strengthVSAvoidmanufacturing difficulty
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The patent applies preliminary action by first creating a foam structure with the desired final geometry and dimensions, then filling it with slurry mixture before conversion. This allows the complex geometric shaping to be done in the foam stage (which is easier to form) rather than in the final silicon carbide material, thereby maintaining material strength while greatly simplifying manufacturing.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent replaces mechanical machining operations with a chemical conversion process. Instead of mechanically cutting or shaping silicon carbide (which is extremely difficult due to its hardness), the invention uses slurry infiltration followed by thermal conversion of foam to silicon carbide, substituting mechanical fabrication with chemical and thermal processes that achieve the same geometric result without the machining difficulty.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Manufacturing precision

If silicon carbide structures are machined to achieve precise geometries, then the final dimensional accuracy is obtained, but the manufacturing time and cost increase

Engineering Contradiction:
Improvegeometric precisionVSAvoidmanufacturing efficiency
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The desired geometric precision is achieved in advance by forming the foam structure to the exact final dimensions before conversion. The foam acts as a sacrificial template that defines the precise geometry, eliminating the need for subsequent precision machining of the silicon carbide material itself, thereby greatly improving manufacturing efficiency while maintaining geometric precision.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent uses the foam structure as a copy or template of the desired final geometry. The foam is formed to match the exact dimensions and shape needed, then serves as a mold for the silicon carbide conversion process, copying the geometric precision from the foam template to the final silicon carbide structure without requiring direct machining of the hard material.

Inventive Principle:
Principle #26Copying

3Reliability

If dense silicon carbide structures are produced directly, then the structural integrity for nuclear applications is achieved, but the fabrication complexity increases

Engineering Contradiction:
Improvestructural integrityVSAvoidfabrication complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent uses porous foam material as an intermediate stage in the fabrication process. The foam's porous structure allows easy infiltration of slurry mixture, and after conversion to silicon carbide, the structure achieves the required density and integrity. This two-stage approach (foam formation then conversion) simplifies fabrication compared to attempting to directly form dense silicon carbide with complex geometries.

Inventive Principle:
Principle #31Porous materials

Solution Approach 2:

The process creates a composite situation during fabrication where foam and slurry mixture coexist temporarily. The foam provides the structural template while the slurry provides the silicon carbide precursors. This composite approach during manufacturing allows for simplified fabrication processes that ultimately produce the required dense, integrity-critical silicon carbide structure for nuclear applications.

Inventive Principle:
Principle #40Composite materials

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 allows for the efficient fabrication of silicon carbide structures with precise geometries and dimensions, overcoming the challenges of machining high-strength materials and ensuring the structural integrity required for nuclear reactor applications.

Implementation Method 1

directing a slurry mixture into the pre-formed carbon foam structure to cause the slurry mixture to penetrate into and fill in pores of the pre-formed carbon foam structure

Methodology Applied
Scientific EffectCapillary action: Capillary Action

Implementation Method 2

supplying heat to the vacuum chamber to cause the silicon particles coated with silicon dioxide exterior layers filled in the pre-formed carbon foam structure to react to become a silicon monoxide gas which fills the pre-formed carbon foam structure and further reacts with carbon in the pre-formed carbon foam structure to convert the carbon in the pre-formed carbon foam structure into silicon carbide

Methodology Applied
Scientific EffectChemical reaction: Chemical Bonding

Implementation Method 3

supplying heat to the vacuum chamber to cause the silicon particles coated with silicon dioxide exterior layers filled in the pre-formed carbon foam structure to react to become a silicon monoxide gas

Methodology Applied
Scientific EffectThermal decomposition: Pyrolysis

Data Source

PatentUS20250042821A1Fabrication of near net-shaped silicon carbide structures
Publication Date: 2025.02.06 GENERAL ATOMICS CO
  • US20250042821A1 patent drawing
  • US20250042821A1 patent drawing
  • US20250042821A1 patent drawing

AI summary

A method of manufacturing a target structure is provided. The method includes: obtaining a model structure of an initial material composition having a predetermined geometry and dimensions; applying a slurry mixture into the model structure; and processing the model structure with the slurry mixture inside the model structure to convert the initial material composition of the model structure into a final material composition to obtain the target structure with the final material composition and having a geometry and dimensions that are substantially similar to the predetermined geometry and dimensions of the model structure.