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Sintered Iron (Fe-Cu PM)

Powder Metallurgy

Basic Information

Category: Powder Metallurgy
Material Type: alloy
Alternative Names:
FC-0208Fe-2CuSintered Iron-CopperPM IronIron PMPowder Metal Iron
Tags:
powder-metallurgysinteredporousautomotivegearsbearings

Composition & Structure

Composition: Fe-2Cu-0.8C (typical FC-0208)
Microstructure: Pearlite and ferrite with interconnected porosity (5-15%); copper phase at prior particle boundaries; possible free graphite

Description

Sintered iron-copper (Fe-2Cu) is the most common iron-based powder metallurgy material, widely used in automotive structural parts. The key preparation challenge is preserving the 5-15% interconnected porosity in its true morphology. Vacuum impregnation with epoxy before grinding is essential. The copper phase at prior particle boundaries and porosity distribution are critical quality features.

Mechanical Properties

Hardness: 60-90 HRB
Hardness (HB): 75-110 HB
Hardness (HV): 80-120 HV
Hardness Category: medium
Tensile Strength: 300-500 MPa
Yield Strength: 200-350 MPa

Physical Properties

Density: 6.4-7.2 g/cm³
Melting Point: 1538 °C

Material Characteristics

Work Hardening: No
Magnetic: Yes
Corrosion Resistance: low

General Preparation Notes

Sintered iron (Fe-Cu PM) is a moderately hard (60-90 HRB, 80-120 HV) powder metallurgy material with 5-15% interconnected porosity. The primary preparation challenge is preserving the porosity in its true morphology without smearing, filling with debris, or causing pullout at pore edges. Vacuum impregnation with epoxy before any grinding is essential. The microstructure consists of pearlite and ferrite (depending on carbon content) with copper phase visible at prior particle boundaries. Prior particle boundaries themselves are an important feature to preserve and reveal.

Sectioning

Use a standard abrasive cut-off wheel (alumina, bonded for steel) or a low-speed diamond saw with continuous coolant. Cutting speed: 200-300 RPM for cut-off saws. Apply moderate feed pressure. The porosity makes the material somewhat more fragile than wrought steel of the same composition, so avoid impact loading. For parts with oil impregnation (self-lubricating bearings), the oil may contaminate the coolant; use a dedicated coolant reservoir. Leave 2-3 mm allowance for grinding. Avoid crushing the pore structure with excessive clamping pressure.

Mounting

CRITICAL: Vacuum impregnation with low-viscosity castable epoxy is essential for PM samples. The epoxy infiltrates the interconnected porosity network, providing support for pore edges during subsequent grinding and polishing. Without vacuum impregnation, pore edges smear and distort, making porosity measurements inaccurate.

Mount the specimen in a standard mounting cup, apply a low-viscosity epoxy resin, and place in a vacuum chamber. Draw vacuum (25-29 inches Hg) for 2-5 minutes, then release vacuum to force epoxy into the pores. Repeat the vacuum cycle 2-3 times for thorough infiltration. Allow complete cure (8-12 hours for room-temperature epoxy). For oil-impregnated PM parts, degrease thoroughly with a solvent (acetone or ultrasonic cleaning in petroleum ether) before vacuum impregnation, as residual oil prevents epoxy penetration.

Grinding

After vacuum impregnation, standard grinding techniques apply. The epoxy-supported porosity allows normal pressure levels. Use SiC papers with water lubrication. Apply moderate pressure (25-35 N per 30 mm sample). Disc speed: 200-300 RPM. Complementary rotation. Monitor pore edges at each step; if smearing is occurring, the vacuum impregnation was incomplete and should be repeated.

Grinding sequence:
  • 240 grit: Remove sectioning damage (20-40 seconds). Moderate pressure.
  • 320 grit: Remove previous scratches (20-40 seconds). Rotate specimen 90 degrees.
  • 400 grit: Further refinement (20-30 seconds).
  • 600 grit: Final grinding step (20-30 seconds). Inspect pore edges under microscope to verify they are clean and sharp.
Rotate specimen 90 degrees between steps. Thorough ultrasonic cleaning between steps to remove debris from the pore/epoxy interfaces.
Recommended Sequence:
240320400600

Polishing

Use napless or low-nap cloths to prevent the cloth fibers from catching on pore edges and causing pullout or smearing.

Diamond polishing sequence:
  • 6 micrometer diamond: 2-4 minutes on a medium-hard synthetic pad with moderate pressure (25-30 N per 30 mm sample). Monitor for pore edge quality.
  • 3 micrometer diamond: 2-3 minutes on a medium-hard pad (20-28 N). Pores should appear as clean, sharp-edged voids filled with clear or faintly colored epoxy.
  • 1 micrometer diamond: 1-2 minutes on a napless pad (18-25 N).
Final polishing:
  • 0.05 micrometer colloidal silica: 1-2 minutes on a soft pad with moderate pressure. Avoid prolonged final polishing which can preferentially attack the softer ferrite phase and create relief at pore edges. The epoxy in the pores polishes at a different rate than the metal; brief final polish times minimize this differential.
After polishing, inspect under the microscope. Pores should be cleanly defined with smooth, sharp edges. If pore edges are rounded, smeared, or if debris is visible in pores, re-polishing or re-mounting with better vacuum impregnation is needed.
Recommended Sequence:
6μm diamond3μm diamond1μm diamond0.05μm colloidal silica

Etching

Sintered iron-copper responds to standard iron and steel etchants. The copper phase is best observed in the as-polished condition or with selective copper etchants.

2-5% Nital (Chemical Etching) - Primary choice:
  • Composition: 2-5 ml HNO3, 95-98 ml ethanol
  • Application: Immerse for 5-15 seconds. Start with 2% and increase concentration or time as needed.
  • Reveals: Pearlite lamellar structure, ferrite grain boundaries, prior particle boundaries, copper phase (remains unetched and appears bright orange-copper colored against the darker etched iron matrix). Porosity appears as dark voids (or epoxy-filled voids if vacuum impregnated).
  • Rinse: Ethanol, then dry with warm air.
4% Picral (Chemical Etching) - For pearlite resolution:
  • Composition: 4 g picric acid, 100 ml ethanol
  • Application: Immerse for 5-15 seconds.
  • Reveals: Pearlite lamellar structure with superior resolution compared to Nital. Does not reveal ferrite grain boundaries as clearly as Nital, but provides better contrast for carbon distribution analysis across the part cross-section.
  • Note: Picric acid is a shock-sensitive explosive when dry. Always keep wetted with >30% water. Handle with care.
For porosity quantification: Image analysis is typically performed on the as-polished (unetched) surface, where pores appear as dark features against the bright metal surface.
Common Etchants:
2-5% Nital4% Picral

Heat Treatment

Sintered, or sinter-hardened

ASTM Standards

  • ASTM B783
  • ASTM E8
  • MPIF Standard 35

Applications

  • Automotive gears
  • Self-lubricating bearings
  • Structural PM parts
  • Small engine components

Typical Uses

  • Transmission gears
  • Oil pump gears
  • Connecting rods
  • Bearing bushings
  • Cam lobes
  • Valve seat inserts