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Machining of CrNiCo alloys (chromium-nickel-cobalt)


The machining of CrNiCo alloys is particularly challenging due to their unique physical properties. The main factors that determine the machinability of these alloys are

Work hardening: CrNiCo alloys have a strong tendency to work harden during machining, which means that the material becomes harder as a result of the cutting process. This makes subsequent cuts more difficult and accelerates tool wear.

Heat generation and low thermal conductivity: Due to high strength and plastic deformation, an excessive amount of heat is generated in the cutting zone. CrNiCo alloys conduct heat poorly, which leads to localized temperature increases. The heat is concentrated at the tool-workpiece interface, which impairs both the service life of the tool and the workpiece quality.

Tool material and wear: The combination of high hardness, toughness and heat bonding in CrNiCo alloys leads to rapid tool wear and possible tool failure. The choice of cutting material (e.g. coated carbides or ceramics) is critical and may require frequent tool changes.

Cutting forces: The strength and toughness of these alloys require high cutting forces. Stable machine structures and powerful spindles are required to ensure dimensional accuracy and surface quality.

Cutting parameters and cooling lubricant: Optimization of cutting speeds, feed rates and cutting depths is essential. Lower speeds and higher feeds are often recommended. The use of optimally adjusted high-pressure coolant is crucial for heat dissipation and chip removal.

Surface quality and tool adhesion: The tendency of CrNiCo alloys to adhere to the tool (built-up edge formation) worsens the surface quality and also increases tool wear, especially with inadequate cooling or unsuitable tool geometries.

Summary: Careful planning, suitable tool selection, optimum cutting parameters and efficient coolant supply are essential for the successful machining of CrNiCo alloys.



Problem
Consequences
Solutions
Work hardening
Subsequent cuts hit much harder material

Sharp tools, higher cutting depth

  • Internal turning: Swiss-MicroTurn
  • Milling: Maykestag Speedcut 4.0 blue
Heat development
More tool wear, distortion

High-pressure cooling, lower cutting speed

  • Internal turning: Swiss-MicroTurn MTHA "SK"
  • Albrecht: APC + Coolant 2.0 sleeve
High tool wear
Frequent tool changes, increased costs

Carbide, CBN or ceramic tools, coating

  • Internal turning: Swiss-MicroTurn CBN or ALTISIN coating
  • Knurling: faceted and DVA-coated Swiss-Knurl roller
  • Drilling/milling: Swiss-Drill ISDTTD204 Maykestag Speedcut 4.0 blue
High cutting forces
Piece/tool distortion, poor surface finish

Stable clamping, strong machines

  • Drilling/milling: Albrecht APC
  • Internal turning: Swiss-MicroTurn MTHA
Low thermal conductivity
Local overheating, surface changes

Coolant management, moderate Vc.

  • TiAlN, ALTISIN coatings
  • Drilling with internal cooling: Swiss-Drill ISDTTD204
  • Internal turning: Swiss-MicroTurn CBN
Material adhesion
Poor surface finish, tool life decreases

High-quality tools with the correct geometry such as

  • Ifanger Swiss-MicroTurn, Swiss-Drill, Swiss-Knurl
  • Maykestag
  • Tungaloy-NTK


Brand nameChemical compositionDIN designationAlloy type
Nimonic 75Ni (Bal), 18–21 Cr, 0.2–0.6 Ti, <5 Fe2.4951 / NiCr20Ti / DIN 17742NiCr (super alloy)
Nimonic 80ANi (Bal), 18–21 Cr, 1.8–2.7 Ti, 1.0–1.8 Al2.4952 / NiCr20TiAl / DIN 17742NiCr-Ti-Al (super alloy )
Nimonic 90Ni (Bal), 18–21 Cr, 16–21 Co, 2 Ti, 1 AlDIN 17742 / EN 10095NiCrCo (super alloy )
Phynox40 Co, 20 Cr, 15 Ni, 7 Mo, Fe Rest2.4711 / CoCr20Ni15Mo7 / ASTM F1058 / ISO 5832-7CoCrNi (Fe based)
Elgiloy40 Co, 20 Cr, 15 Ni, 7 Mo, Fe Rest2.4711 / ASTM F1058 / ISO 5832-7CoCrNi (Fe based)
MP35N35 Ni, 35 Co, 20 Cr, 10 MoASTM F562 / ISO 5832-6 / (kein DIN)NiCoCr
Haynes 18839 Co, 22 Cr, 22 Ni, 14 W2.4683 / ASTM B422CoCrNi
Haynes HR-12037 Ni, 25 Cr, 3 Co, 33 Fe, 2.5 Mo, 2.5 W2.4854 / NiFe33Cr25CoNiCrFe
Inconel 600Ni 72 min, 14–17 Cr, 6–10 Fe2.4816 / NiCr15Fe / DIN 17752 / UNS N06600NiCr
Inconel 625Ni 58 min, 20–23 Cr, 8–10 Mo, 3.15–4.15 Nb2.4856 / NiCr22Mo9Nb / DIN 17744 / UNS N06625NiCrMo-Nb
Inconel 718Ni 50–55, 17–21 Cr, 4.75–5.5 Nb, 2.8–3.3 Mo, Fe Bal2.4668 / NiCr19NbMo / DIN 17744 / UNS N07718NiCrFe-Nb-Mo
Hastelloy B-2Ni 65, 26–30 Mo, <3 Fe, <1 Cr2.4617 / NiMo28 / DIN 17744 / UNS N10665NiMo
Hastelloy C-4Ni Bal, 14.5–17.5 Cr, 14–17 Mo, 3 W2.4610 / NiCr16Mo16 / DIN 17744 / UNS N06455NiCrMo
Hastelloy C-276Ni 57 min, 14.5–16.5 Cr, 15–17 Mo, 3.7–5.3 W2.4819 / NiMo16Cr15W / DIN 17744 / UNS N10276NiCrMo
Monel 400Ni 63 min, 28–34 Cu, 1–2.5 Fe2.4360 / NiCu30Fe / DIN 17743 / UNS N04400NiCu
Monel K-500Ni 63 min, 27–33 Cu, 2.3–3.15 Al, 0.35–0.85 Ti2.4375 / NiCu30Al / DIN 17743 / UNS N05500NiCu (hardened)
Nickel 200Ni >99 (99.0–99.6), <0.4 Fe, <0.25 Cu2.4066 / Ni99.6 / DIN 17740 / UNS N02200Ni (pure)
Nickel 201Ni >99 (99.0 min), <0.02 C (LC), <0.4 Fe2.4068 / LC-Ni99.2 / DIN 17740 / UNS N02201Ni (pure, LC)
Incoloy 800Ni 30–35, 19–23 Cr, Fe 39.5 min, 0.15–0.6 Ti/Al2.4876 / NiCr21Fe / DIN 17743 / UNS N08800NiCrFe
Incoloy 825Ni 38–46, 19.5–23.5 Cr, 2.5–3.5 Mo, 1.5–3 Cu, Fe Bal2.4858 / NiCr21Mo / DIN 17744 / UNS N08825NiCrFe-Mo-Cu