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Carbon Fiber Reinforced Polymer (CFRP)

Composite

Basic Information

Category: Composite
Material Type: composite
Alternative Names:
CFRPCarbon Fiber CompositeCarbon Fiber Epoxy
Tags:
polymer-compositecarbon-fiberaerospace

Composition & Structure

Composition: 60% carbon fiber, 40% epoxy matrix
Microstructure: Unidirectional or woven carbon fibers in epoxy matrix

Description

High-strength carbon fiber composite with excellent strength-to-weight ratio. Used extensively in aerospace and high-performance applications.

Mechanical Properties

Hardness: 60-80 HRC (fiber)
Hardness (HRC): 60 HRC
Hardness Category: hard
Tensile Strength: 1500 MPa

Physical Properties

Density: 1.6 g/cm³

Material Characteristics

Work Hardening: No
Magnetic: No
Corrosion Resistance: high

Sectioning

Use abrasive cut-off wheel with adequate coolant flow. Standard cut-off wheel (1.0-1.5 mm thickness) is appropriate. Use adequate coolant flow to prevent overheating. Cutting speed: 200-300 RPM for most cut-off saws. Apply steady, moderate pressure. Avoid forcing the cut which can cause wheel wear and sample damage. Leave adequate allowance (~2-3 mm) for grinding away the heat-affected zone from cutting.

Mounting

Cold mounting with epoxy resin is preferred to avoid heat that could affect the microstructure. Use a low-shrinkage epoxy resin for best edge retention. Ensure complete cure before grinding to prevent edge rounding and maintain sample integrity.

Hot compression mounting is acceptable if the part tolerates ~150-180°C and moderate pressure (2000-3000 psi for phenolic). Use phenolic or epoxy-phenolic resins. Ensure proper cooling under pressure to minimize shrinkage.

Grinding

The hardness (60-80 HRC (fiber)) of Carbon Fiber Reinforced Polymer (CFRP) requires careful grinding. Use standard SiC grinding papers with adequate water lubrication. Disc speed: 200-300 RPM. Apply light to moderate pressure (30-40 N per 30 mm sample) - the hard material may require longer grinding times. Use sharp, fresh grinding papers to minimize deformation.

Grinding sequence:
  • 240 grit: Remove sectioning damage (40-90 seconds). Use moderate pressure to remove heat-affected zone.
  • 320 grit: Remove previous scratches (40-90 seconds). Ensure complete scratch removal.
  • 400 grit: Remove previous scratches (40-90 seconds). Ensure complete scratch removal.
  • 600 grit: Remove previous scratches (40-90 seconds). Ensure complete scratch removal.
Always rotate the specimen holder 90° between steps to ensure complete scratch removal. Use complementary rotation (platen and holder same direction, different speeds) rather than contra-rotation to minimize deformation. Adequate water lubrication is critical - avoid drying during grinding which can cause smearing.
Recommended Sequence:
240320400600

Polishing

The hardness requires careful polishing. Use diamond polishing with appropriate polishing pads for each stage. Apply light to moderate pressure throughout to prevent deformation.

Diamond polishing sequence:
  • 6μm diamond: 2-4 minutes on a medium-hard synthetic pad (e.g., TEXPAN) with light to moderate pressure (30-40 N per 30 mm sample). Start with 6μm to minimize damage. The hard material may require longer polishing times.
  • 1μm diamond: 2-4 minutes on a medium-hard synthetic pad (e.g., TEXPAN) with light pressure (25-35 N). Continue removing scratches from previous step.
  • 0.25μm diamond: 2-3 minutes on a medium-hard synthetic pad with lighter pressure (25-35 N). These pads provide gentle material removal.
  • 0.05μm colloidal silica: 1-2 minutes on a high-napped final polishing pad (e.g., MICROPAD) with very light pressure. This removes any remaining fine scratches and prepares the surface for etching. Monitor for relief - reduce polishing time if excessive relief develops.
Use appropriate polishing lubricants. The hard material means polishing times should be sufficient but not excessive - avoid over-polishing which can cause relief and affect grain boundary revelation. Monitor the surface frequently under the microscope to check for smearing or excessive relief.
Recommended Sequence:
6μm diamond1μm diamond0.25μm diamond

Etching

Carbon Fiber Reinforced Polymer (CFRP) responds well to standard etchants for composite materials. The unidirectional or woven carbon fibers in epoxy matrix will reveal clearly with appropriate etchants. No Etching (Chemical Etching) - Standard etchant for this material:
  • Application: Follow standard procedures for No Etching.
  • Reveals: Grain boundaries and microstructure clearly.
  • Rinse: Immediately with water, then ethanol. Dry with compressed air.
  • Note: Use appropriate safety measures. Consult material-specific guidelines.
Polarized Light (Chemical Etching) - Standard etchant for this material:
  • Application: Follow standard procedures for Polarized Light.
  • Reveals: Grain boundaries and microstructure clearly.
  • Rinse: Immediately with water, then ethanol. Dry with compressed air.
  • Note: Use appropriate safety measures. Consult material-specific guidelines.
Etching Strategy:
  • Start with No Etching for general microstructure examination
  • Always clean and degrease before etching
  • Use short initial etch times (a few seconds), check under the microscope, repeat if needed
  • Check etching progress frequently - over-etching can obscure fine details
Safety: All etchants require proper PPE (gloves, safety glasses, lab coat), proper fume hood, and appropriate safety measures. Handle with care.
Common Etchants:
No EtchingPolarized Light

Heat Treatment

Cured at 120-180°C

No standards information available.

Applications

  • Aerospace
  • Automotive
  • Sports equipment

Typical Uses

  • Aircraft structures
  • Racing car bodies
  • Bicycle frames