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Steel 36NiCrMo16 +QT-40 (+QT)

Heat-treated state · default condition

EN 36NiCrMo16

Standard stocked condition for bar and small forgings; the usual specification reference for this grade.

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Values for the +QT-40 condition

Other 36NiCrMo16 tempers and conditions

36NiCrMo16 is listed in 9 conditions; see the grade overview at 36NiCrMo16.

Compare all 9 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Pick for machining, deep drilling or cold straightening of bar before final quench and temper.5208001621 HRC—
+QT
Heavy forgings and thick shafts — the section size where this grade's nickel content really pays off versus 34CrNiMo6.8601,1001335 HRC—
+QT
Medium-section shafts and gear blanks where 900 MPa minimum yield with better toughness is wanted.9601,2001238 HRC—
Normalized
Rarely supplied as a delivery condition — the 4 % Ni gives air-hardening, so a normalise leaves a hard martensitic/bainitic structure needing tempering.1,0501,450946 HRC5.4 % IACS
+QT then gas/plasma nitrided
Use where a wear- and fatigue-resistant surface is needed on a tough high-strength core (gears, spindles, hydraulic rods).1,0501,2501158 HRC5.7 % IACS
+QT-40DefaultThis page
+QT
Standard stocked condition for bar and small forgings; the usual specification reference for this grade.1,1201,3301142 HRC—
+SH / peeled-turned bar in +QT condition
Q&T bar supplied peeled and straightened to close tolerance with a decarb-free surface for direct machining.1,1201,3301142 HRC5.7 % IACS
+QT
Small-diameter bar for highly stressed bolts, pins and shafts at the top strength class.1,1501,3501043 HRC—
Q&T low-temper
Choose for ultra-high-strength aerospace/landing-gear-type parts; toughness and hydrogen sensitivity become the design drivers.1,4001,600948 HRC—

What is 36NiCrMo16 +QT-40?

36NiCrMo16 +QT-40 is 36NiCrMo16 heat treated to +QT-40 — standard stocked condition for bar and small forgings; the usual specification reference for this grade. 36NiCrMo16 +QT-40 has a yield strength of 1,120 MPa (162 ksi) and a tensile strength of 1,330 MPa (193 ksi) — stronger than 93% of steel grades. Elongation at break is 11% and the elastic modulus is 205 GPa (29.7 Msi). 36NiCrMo16 +QT-40 has a density of 7.85 g/cm³ (0.284 lb/in³), heavier than 56% of steel grades. It melts at 1,420°C (2,588 °F).

Advantages

  • High strength — 1,120 MPa (162 ksi), better than 93% of steel grades
  • Polishes to a fine finish — 70/100, better than 87% of steel grades

Limitations

  • Limited ductility — 11%, worse than 89% of steel grades
  • Difficult to machine — 30/100, worse than 89% of steel grades
  • Limited formability — 15/100, worse than 87% of steel grades
  • Difficult to weld — 20/100, worse than 84% of steel grades
  • High embodied carbon — 2.5 kg CO₂/kg, worse than 82% of steel grades

36NiCrMo16 +QT-40 properties

Typical room-temperature values for 36NiCrMo16 +QT-40; 13 are specific to this condition. Other listed values are 36NiCrMo16 reference data and may not represent this condition. Bars are the position among steel grades.

Physical3

36NiCrMo16 +QT-40 has a density of 7.85 g/cm³ (0.284 lb/in³), heavier than 56% of steel grades. It melts at 1,420°C (2,588 °F).

Density7.85 g/cm³0.28 lb/in³
Melting Point (Solidus)1,420°C2,588 °F
Liquidus Temperature1,480°C2,696 °F

Mechanical16

36NiCrMo16 +QT-40 has a yield strength of 1,120 MPa (162 ksi) and a tensile strength of 1,330 MPa (193 ksi) — stronger than 93% of steel grades. Elongation at break is 11% and the elastic modulus is 205 GPa (29.7 Msi).

Elastic (Young's) Modulus205 GPa29.7 Msi
Shear Modulus80 GPa11.6 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)1,330 MPa193 ksi
Yield Strength (0.2% offset)1,120 MPa162 ksi
Elongation at Break11%
Reduction in Area48%
Compressive Strength1,150 MPa167 ksi
Shear Strength800 MPa116 ksi
Fatigue Strength (Endurance Limit)600 MPa87 ksi
Fracture Toughness (K_IC)95 MPa·√m86.5 ksi·√in
Charpy V-Notch Impact (RT)45 J33.2 ft·lbf
Hardness, Brinell400 HB
Hardness, Rockwell C42 HRC
Hardness, Vickers420 HV

Thermal6

36NiCrMo16 +QT-40 is rated for continuous service to 350°C (662 °F). It conducts heat at 34 W/m·K (19.6 BTU/hr·ft·°F), worse than 77% of steel grades. Thermal expansion is 11.8 µm/m·K (6.56 µin/in·°F).

Thermal Conductivity34 W/m·K19.6 BTU/hr·ft·°F
Specific Heat Capacity470 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)11.8 µm/m·K6.6 µin/in·°F
Latent Heat of Fusion250 J/g107 BTU/lb
Max Service Temperature (continuous)350°C662 °F
Min Service Temperature-80°C-112 °F

Electrical3

36NiCrMo16 +QT-40 conducts electricity at 5.7 % IACS, worse than 80% of steel grades.

Electrical Conductivity5.7 % IACS
Electrical Resistivity3×10⁻⁷ Ω·m11.8 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is not recommended (13/100), better than 66% of steel grades.

Galvanic Potential (seawater, vs SCE)-0.6 V
Corrosion ResistanceNot recommended13/100
Chemical Resistance SummaryNo inherent corrosion resistance: rusts in humid air and seawater, attacked by acids; requires oil, phosphate, Zn-Ni/Cd plating or paint. Susceptible to hydrogen embrittlement above ~1200 MPa — bake after plating.

Sustainability4

Producing a kilogram of 36NiCrMo16 +QT-40 takes about 34 MJ of energy and emits 2.5 kg of CO₂ — more than 82% of steel grades. Typical recycled content is 35%.

Embodied Energy (primary production)34 MJ/kg14,617 BTU/lb
Embodied Carbon (primary production)2.5 kg CO₂/kg
Embodied Water60 L/kg7.2 gal/lb
Typical Recycled Content35%

Manufacturability8

36NiCrMo16 +QT-40's machinability is poor (30/100, worse than 89% of steel grades); weldability poor (20/100); formability poor (15/100).

MachinabilityPoor30/100
Machinability Rating (AISI 1212 = 100 %)35%
WeldabilityPoor20/100
Formability (cold)Poor15/100
CastabilityPoor30/100
Brazeability / SolderabilityFair40/100
PolishabilityVery good70/100
Anodizing Responsen/a — ferrous alloy; use Zn-Ni, hard chrome, phosphate or nitriding instead

Common Calculations5

Specific Strength (UTS / density)calculated169 kN·m/kg
Specific Stiffness (E / density)calculated26.1 MN·m/kg
Modulus of Resiliencecalculated3,060 kJ/m³
Thermal Diffusivitycalculated9.2 mm²/s
Thermal Shock Resistance Indexcalculated19

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with 36NiCrMo16 +QT-40

Is 36NiCrMo16 easy to machine?

Machine in the +A condition (≈235 HB) where possible; in +QT at 40+ HRC use rigid setups, coated carbide or CBN, low speed and heavy positive feed to stay under the work-hardened layer.

Can 36NiCrMo16 be welded?

Poor weldability (CEV ≈ 1.2): avoid if possible, otherwise preheat 250–350 °C, low-hydrogen consumables, immediate post-weld temper below the part's tempering temperature.

Can 36NiCrMo16 be formed, bent or molded?

Hot forge 1100–850 °C then slow-cool/anneal to prevent air-hardening cracks; no meaningful cold forming in the hardened state — straighten warm or after tempering.

What surface finishes work on 36NiCrMo16?

Not anodizable; protect with phosphate + oil, Zn-Ni or Cd plating (bake 190 °C ≥ 8 h to de-embrittle), hard chrome or nitriding for wear surfaces; takes a fine polish for die and mould applications.

36NiCrMo16 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
C0.32 – 0.390.36
Si≤ 0.40.25
Mn0.3 – 0.60.45
P≤ 0.030.01
S≤0.035 for base grade; ≤0.005 for +S-controlled / vacuum-degassed variants≤ 0.040.01
Cr1.6 – 21.8
Mo0.25 – 0.450.35
Nisource of the very high hardenability3.6 – 4.13.85
Febalance—

36NiCrMo16 +QT-40 — frequently asked

What is 36NiCrMo16 +QT-40 used for?

36NiCrMo16 +QT-40 is typically used for large forged shafts, heavy machinery components and high-strength structural forgings. In short: through-hardens thick sections; highest strength Ni-Cr-Mo grade; very poor weldability.

What is the yield strength of 36NiCrMo16 +QT-40?

36NiCrMo16 +QT-40 has a typical yield strength of 1,120 MPa (162 ksi) and a tensile strength of 1,330 MPa (193 ksi) — stronger than 93% of steel grades. Strength varies by condition: see the 9 listed tempers.

Is 36NiCrMo16 +QT-40 easy to machine?

Not especially — machinability is rated poor (30/100, worse than 89% of steel grades). Machine in the +A condition (≈235 HB) where possible; in +QT at 40+ HRC use rigid setups, coated carbide or CBN, low speed and heavy positive feed to stay under the work-hardened layer.

Can 36NiCrMo16 +QT-40 be welded?

Not readily — weldability is rated poor (20/100). Poor weldability (CEV ≈ 1.2): avoid if possible, otherwise preheat 250–350 °C, low-hydrogen consumables, immediate post-weld temper below the part's tempering temperature.

What surface finishes work on 36NiCrMo16 +QT-40?

Not anodizable; protect with phosphate + oil, Zn-Ni or Cd plating (bake 190 °C ≥ 8 h to de-embrittle), hard chrome or nitriding for wear surfaces; takes a fine polish for die and mould applications.

Can 36NiCrMo16 +QT-40 be formed, bent or molded?

Hot forge 1100–850 °C then slow-cool/anneal to prevent air-hardening cracks; no meaningful cold forming in the hardened state — straighten warm or after tempering.

What is the maximum service temperature of 36NiCrMo16 +QT-40?

36NiCrMo16 +QT-40 is rated for continuous use to about 350°C (662 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 36NiCrMo16 +QT-40 and 36NiCrMo16 QT-1600?

+QT-40 is the default condition — standard stocked condition for bar and small forgings; the usual specification reference for this grade. QT-1600: choose for ultra-high-strength aerospace/landing-gear-type parts; toughness and hydrogen sensitivity become the design drivers. Yield strength is 1,120 MPa in +QT-40 versus 1,400 MPa in QT-1600.

Sources

  1. EN 10083-3 Steels for quenching and tempering — Alloy steels — CEN (2006)
  2. EN 10250-3 Open die steel forgings — Alloy special steels — CEN (1999)
  3. EN 10027-2 / Werkstoff 1.6773 designation system — CEN (2015)
  4. ASM Handbook Vol.1 — Properties and Selection: Irons, Steels and High-Performance Alloys — ASM International (1990)
  5. ASM Handbook Vol.19 — Fatigue and Fracture — ASM International (1996)
  6. Ni-Cr-Mo through-hardening steel bar datasheets (1.6773 / 35NCD16 class) — European special steel producers (2023)
  7. GB/T 3077 (34CrNi3Mo comparable grade) — SAC (2015)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.