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AISI 4140 Chromium-Molybdenum Steel

Alloy Steel

Basic Information

Category: Alloy Steel
Material Type: alloy
Alternative Names:
4140AISI 414042CrMo4
Tags:
heat-treatablehigh-strengthmachinable

Composition & Structure

Composition: Fe-0.40C-1Cr-0.25Mo-0.85Mn
Microstructure: Tempered martensite

Description

Chromium-molybdenum steel with excellent hardenability and strength. Used in high-stress applications.

Mechanical Properties

Hardness: 197 HB
Hardness (HB): 197 HB
Hardness Category: medium
Tensile Strength: 655 MPa
Yield Strength: 415 MPa

Physical Properties

Density: 7.85 g/cm³
Melting Point: 1416 °C

Material Characteristics

Work Hardening: No
Magnetic: Yes
Corrosion Resistance: low

General Preparation Notes

AISI 4140 Chromium-Molybdenum Steel is a medium-hard (197 HB) alloy steel (0.40% C, 1% Cr, 0.25% Mo) with a tempered martensite microstructure when quenched and tempered. One of the most commonly used alloy steels in aerospace, automotive, and oil & gas applications. The chromium and molybdenum additions provide excellent hardenability and strength. The medium hardness allows for standard preparation procedures with moderate pressure. The tempered martensite structure will reveal clearly with standard alloy steel etchants. The material is typically quenched and tempered, so the microstructure will show tempered martensite with possible carbides. Commonly used in shafts, gears, bolts, and high-stress applications due to excellent hardenability and strength.

Sectioning

Use abrasive cut-off wheel designed for alloy steel (Al₂O₃ or SiC abrasive). Standard cut-off wheel (1.0-1.5 mm thickness) is appropriate. Use adequate coolant flow to prevent overheating - excessive heat can affect the tempered martensite structure. Cutting speed: 200-300 RPM for most cut-off saws. Apply steady, moderate pressure - the medium-hard material allows for reasonable feed rates. 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 tempered martensite structure. 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 (3000-4000 psi for phenolic). Use phenolic or epoxy-phenolic resins designed for medium-hard materials. Ensure proper cooling under pressure to minimize shrinkage and maintain edge retention. For aerospace, automotive, and oil & gas applications, ensure the mounting material is compatible with the intended use environment.

Grinding

The medium hardness (197 HB) of AISI 4140 allows for standard grinding procedures. Use standard SiC grinding papers with adequate water lubrication. Disc speed: 200-300 RPM. Apply moderate pressure (25-35 N per 30 mm sample) - the medium-hard material can tolerate reasonable pressure. Use sharp, fresh grinding papers to minimize deformation.

Grinding sequence:
  • 120 grit: Remove sectioning damage (30-60 seconds). Use moderate pressure to remove heat-affected zone.
  • 240 grit: Remove previous scratches (30-60 seconds). Ensure complete scratch removal.
  • 320 grit: Further refinement (30-60 seconds). Continue scratch removal.
  • 400 grit: Refinement (30-60 seconds). Prepare for polishing.
  • 600 grit: Final grinding step (30-60 seconds). Ensure all scratches are removed before polishing.
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.
Recommended Sequence:
120240320400600

Polishing

The medium hardness allows for standard polishing procedures. Use diamond polishing with appropriate polishing pads for each stage. Apply moderate pressure throughout. The tempered martensite structure should be preserved during polishing.

Diamond polishing sequence:
  • 6μm diamond: 3-4 minutes on a medium-hard synthetic pad (e.g., TEXPAN) with moderate pressure (25-35 N per 30 mm sample). Start with 6μm for medium-hard materials. Standard synthetic pads work well for this hardness level.
  • 3μm diamond: 3-4 minutes on a medium-hard synthetic pad (e.g., TEXPAN) or non-woven intermediate pad with moderate pressure. Continue removing scratches from previous step.
  • 1μm diamond: 2-3 minutes on a low-napped pad designed for fine polishing (e.g., GOLD PAD) with lighter pressure (20-30 N). These pads provide consistent material removal and flatness control.
Final polishing:
  • 0.05μm colloidal silica: 1-2 minutes on a high-napped final polishing pad (e.g., MICROPAD) with light pressure. High-napped pads are recommended for colloidal silica and produce a mirror finish. 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 medium hardness means standard polishing times work well - ensure complete scratch removal at each step. Monitor for any carbides that may require additional polishing time. The tempered martensite structure should be clearly visible after proper polishing.
Recommended Sequence:
6μm diamond3μm diamond1μm diamond0.05μm colloidal silica

Etching

AISI 4140 Chromium-Molybdenum Steel responds well to standard alloy steel etchants. The tempered martensite structure will reveal clearly with appropriate etchants. The chromium and molybdenum additions may require slightly longer etching times than plain carbon steels. Two primary etchants are recommended:

2% Nital (Chemical Etching) - Primary choice for alloy steels:
  • Composition: 2ml HNO₃ (concentrated), 98ml ethanol
  • Preparation: Add nitric acid to ethanol slowly with stirring. Prepare fresh for best results. Solution is stable for several days if stored properly.
  • Application: Immerse sample or swab for 5-15 seconds. Standard etchant for alloy steels. The chromium and molybdenum content may require slightly longer etching times than plain carbon steels.
  • Reveals: Tempered martensite structure, prior austenite grain boundaries, and any carbides clearly. Excellent for general microstructure examination. Good contrast for tempered martensite structure.
  • Rinse: Immediately with water, then ethanol. Dry with compressed air or warm air to avoid staining.
  • Note: Prepare fresh when needed. Shelf life: several days. Use in fume hood. The alloy content may require slightly longer etching times than plain carbon steels.
4% Picral (Chemical Etching) - For revealing carbides and fine structure:
  • Composition: 4g picric acid, 100ml ethanol
  • Preparation: Dissolve picric acid in ethanol with stirring. Prepare fresh for best results. Solution is stable for several weeks if stored properly.
  • Application: Immerse sample or swab for 10-60 seconds. Excellent for revealing carbides without attacking the matrix. Particularly useful when examining carbide distribution in tempered martensite.
  • Reveals: Carbides clearly with excellent contrast. Less aggressive on the matrix than nital. Good for revealing fine carbide distribution in tempered martensite.
  • Rinse: Immediately with water, then ethanol. Dry with compressed air.
  • Note: Prepare fresh when needed. Shelf life: several weeks if stored properly. Use in fume hood. Picric acid is explosive when dry - keep moist and handle with care.
Etching Strategy:
  • Start with 2% nital for general microstructure examination - it provides good contrast and reveals tempered martensite structure clearly
  • Use 4% picral if you need to examine carbide distribution in detail or when nital is too aggressive
  • Etching time may vary with tempering condition - higher tempering temperatures result in coarser carbides and different etching response
  • The chromium and molybdenum additions provide excellent hardenability - ensure material is properly quenched and tempered
  • 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
  • For aerospace applications, ensure proper surface preparation to reveal any service-related changes or fatigue damage
  • For automotive applications, ensure proper surface preparation to reveal any microstructural changes from service or processing
  • For oil & gas applications, ensure proper surface preparation to reveal any service-related changes or corrosion
  • The tempered martensite structure should reveal prior austenite grain boundaries with proper etching
  • Carbides may be present depending on tempering temperature - higher tempering temperatures result in more and coarser carbides
  • The chromium and molybdenum additions may result in slightly different etching characteristics compared to plain carbon steels
Safety: Both etchants require proper PPE and fume hood. Nital produces toxic fumes. Picral contains picric acid which is explosive when dry - keep moist and handle with extreme care.
Common Etchants:
2% Nital4% Picral

Heat Treatment

Quenched and tempered

Temperature Parameters

Annealing Temperature: 845 °C

No standards information available.

Applications

  • Aerospace
  • Automotive
  • Oil and gas

Typical Uses

  • Shafts
  • Gears
  • Bolts