Ceramic Coatings for C/C Thermal Protection via Selective Laser Heating

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Solution Overview

Problem

Traditional processes for forming carbon-carbon (C/C) composites for thermal protection systems are expensive, time-consuming, and prone to defects due to high-temperature heat treatments, making them impractical for large-scale or time-sensitive projects.

Innovation Solution

A method involving selective laser heating (SLH) of preceramic polymer-coated carbon-carbon composites to form ceramic coatings, using polymers like SiC and HfC, with optional metal carbide coatings, to create anti-ablative thermal protection systems with controlled thermal expansion and improved mechanical properties.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If traditional high-temperature heat treatment processes are used to form C/C composites, then the crystal structure is refined and high temperature stability is improved, but the production time increases to months and defects such as pores and cracks develop

Engineering Contradiction:
Improvehigh temperature stabilityVSAvoidproduction time
Core Design Contradiction:
Stability of the object's compositionVSLoss of time

Solution Approach 1:

The patent changes the heating parameters from traditional slow heat treatment (1,000-1,500°C for months) to selective laser heating at higher temperatures (1,500-2,750°C) applied locally and rapidly. This parameter change achieves the same crystal structure refinement (graphitization) in a fraction of the time while maintaining high temperature stability.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent replaces the traditional thermal field heating method with a selective laser heating method. The laser provides concentrated energy that can rapidly heat specific regions to the required temperatures for graphitization without the need for prolonged furnace heating, thus reducing production time while maintaining material stability.

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

2Stability of the object's composition

If traditional bulk high-temperature heat treatment is applied to C/C composites, then the crystal structure is refined, but mechanically compromised porous and brittle structures form due to rapid heating

Engineering Contradiction:
Improvecrystal structure refinementVSAvoidmechanical characteristics
Core Design Contradiction:
Stability of the object's compositionVSReliability

Solution Approach 1:

The patent applies selective laser heating to create localized high-temperature zones for graphitization while leaving the bulk material at lower temperatures. This local quality approach allows crystal structure refinement in specific regions without subjecting the entire part to rapid heating that causes porosity and brittleness, thereby improving mechanical characteristics.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent segments the heating process into selective laser heating zones rather than applying uniform bulk heating. By dividing the heating into controlled local regions, the process achieves crystal refinement without the harmful effects of rapid bulk heating, preventing the formation of porous and brittle structures.

Inventive Principle:
Principle #1Segmentation

3Temperature

If traditional C/C composite manufacturing processes are used, then thermal protection is achieved, but the cost increases due to repeated high-temperature heating cycles and specialized capital equipment

Engineering Contradiction:
Improvethermal protectionVSAvoidmanufacturing cost
Core Design Contradiction:
TemperatureVSEase of manufacture

Solution Approach 1:

The patent replaces expensive specialized capital equipment and repeated high-temperature heating cycles with selective laser heating technology. The laser system can be integrated into existing manufacturing lines and requires less specialized equipment, thereby reducing manufacturing costs while maintaining thermal protection capabilities.

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

Solution Approach 2:

The selective laser heating process uses the laser energy itself to directly create the thermal conditions needed for graphitization, eliminating the need for separate heating cycles and specialized equipment. This self-service approach reduces both equipment requirements and manufacturing costs while achieving the same thermal protection.

Inventive Principle:
Principle #25Self-service

4Temperature

If conventional C/C composite processes are used for large scale projects, then thermal protection systems can be manufactured, but the process becomes impractical due to extended production time and high costs

Engineering Contradiction:
Improvethermal protectionVSAvoidproduction speed
Core Design Contradiction:
TemperatureVSProductivity

Solution Approach 1:

The patent changes the heating parameters from slow, prolonged heat treatment to rapid selective laser heating. This parameter change enables production speeds suitable for large-scale projects with tight deadlines, reducing production time from months to a fraction of that time while maintaining thermal protection quality.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The selective laser heating process allows for continuous processing without the need for repeated heating cycles and cooling periods required by traditional methods. This continuous action significantly increases productivity and makes the process practical for large-scale projects with time-sensitive delivery requirements.

Inventive Principle:
Principle #20Continuity of useful 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

The method reduces production time and costs while enhancing the durability and resistance to oxidation of C/C composites, providing effective thermal protection with minimal defects and improved mechanical characteristics.

Implementation Method 1

selective laser heating (SLH) of preceramic polymer-coated carbon-carbon composites to form ceramic coatings

Methodology Applied
Scientific EffectLaser heating: Laser

Implementation Method 2

with optional metal carbide coatings, to create anti-ablative thermal protection systems with controlled thermal expansion

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Implementation Method 3

selective laser heating (SLH) of preceramic polymer-coated carbon-carbon composites to form ceramic coatings

Methodology Applied
Scientific EffectPhase change: Phase Change

Implementation Method 4

enhancing the durability and resistance to oxidation of C/C composites, providing effective thermal protection

Methodology Applied
Scientific EffectOxidation resistance: Oxidation

Data Source

PatentUS20250368793A1Thermal protection systems having ceramic coatings optionally with metal carbide coatings
Publication Date: 2025.12.04 BATTELLE MEMORIAL INST
  • US20250368793A1 patent drawing
  • US20250368793A1 patent drawing
  • US20250368793A1 patent drawing

AI summary

The present disclosure relates to the formation of thermal protection systems based on the formation of ceramic coatings. Such ceramic coatings may be derived from polymeric resins and may be applied over carbon-carbon (C/C) composites. The ceramic coatings may optionally contain a metal carbide coating.