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High-Temperature Carbon Composites

Utilizing Carbon/Carbon (C/C) composites to solve structural challenges in high-temperature environments where traditional graphite fails due to brittleness.

Target Buyer:Engineers pushing the limits of high-temperature fixturing.
Carbon carbon composite tray for high-temperature load bearing 1

Solution Highlights

  • Exceptional strength-to-weight
  • Thermal shock immunity
  • Longer lifespan than graphite

Common Use Cases

  • Heavy Load Sintering
  • Aerospace Processing

Implementation Focus

  • Load calculations
  • Fiber orientation (2D vs 3D)

Application Evaluation Matrix

Evaluation MetricTypical RangeBuyer Relevance
Flexural Strength> 120 MPaCarries heavy loads without sagging.
Fiber Architecture2D or 3D C/C composite by load directionFiber orientation controls strength, thread retention, and long-term deformation.
Operating AtmosphereVacuum or inert gas; oxidation protection if requiredC/C composite strength is excellent at temperature, but oxygen exposure must be managed.
Load CaseStatic load, fixture spacing, and thermal-cycle countTray sag, bolt shear, and creep risk depend on the real support condition.

Application Selection Logic

Decision FactorSelection LogicBuyer Check
Load at temperatureChoose C/C composite when graphite is too brittle or molybdenum adds too much thermal mass.Provide load, support spacing, furnace temperature, and cycle count.
Fiber architecture2D C/C can fit plates and trays; 3D architecture is preferred for multi-directional stress and threads.Clarify bending direction, thread engagement, and any fastener preload.
Oxidation boundaryC/C composite is strongest in vacuum or inert environments; oxygen exposure needs protection.Share atmosphere, leak risk, cleaning practice, and cooldown handling.

Application Delivery and QC Flow

StageDelivery / QC CheckpointBuyer Evidence
1. Load-case reviewDefine temperature, support spacing, fastener preload, tray load, and cycle count.Application sketch, fixture drawing, load estimate, and atmosphere notes.
2. Fiber architectureChoose 2D or 3D C/C blank according to bending, shear, and thread loads.Material route with density and architecture recommendation.
3. Densification and machiningProcess C/C blank, then machine threads, holes, plates, and tray geometry.Dimensional report for load-bearing and assembly-critical features.
4. Strength-risk checkReview delamination, thread stripping, sag, and edge damage before shipping.Visual inspection plus agreed mechanical evidence if required.
5. Handling and packingPrevent abrasion and impact on lightweight C/C fixtures during export.Packing photos and handling notes for furnace maintenance teams.

RFQ Preparation Checklist

  1. Load requirements
  2. Operating temperature
  3. Dimensions

Risk and Mitigation

  • Oxidation: Available with oxidation-resistant coatings for specific atmospheres.

Recommended Products

Carbon carbon composite tray for high-temperature load bearing 2
Carbon carbon composite tray for high-temperature load bearing 2
Carbon carbon composite tray for high-temperature load bearing 3
Carbon carbon composite tray for high-temperature load bearing 3
Carbon carbon composite tray for high-temperature load bearing 4
Carbon carbon composite tray for high-temperature load bearing 4
C/C composite fastener for high-temperature furnace fixture 1
C/C composite fastener for high-temperature furnace fixture 1
C/C composite fastener for high-temperature furnace fixture 2
C/C composite fastener for high-temperature furnace fixture 2
C/C composite fastener for high-temperature furnace fixture 3
C/C composite fastener for high-temperature furnace fixture 3

Buyer FAQ

Is C/C more expensive than graphite?

Initial cost is usually higher, but total cost can improve when the application benefits from longer service life and reduced maintenance.

When is C/C composite a better choice than graphite?

Choose C/C composite when the part carries load, sees repeated thermal shock, needs threaded strength, or fails because graphite is too brittle.

What information is needed for C/C tray or fastener design?

Provide load, support spacing, maximum temperature, atmosphere, cycle count, thread standard, and the current failure mode if replacing another material.

Can C/C composite be used in oxidizing atmospheres?

C/C composite performs best in vacuum or inert gas. If oxygen exposure is expected, the application needs oxidation-risk review and possible protective treatment.

Related Resources

From Application Review to RFQ

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