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Jiangyin Jiangnan Metal Co., Ltd. Open-die forgings · Seamless rolled rings · Made to drawing
6 free AISI 4150 engineering tools on this page: Designation lookup Tempering calculator Grade substitution Heat-treatment cycle Forging weight RFQ writer

Medium-carbon chromium–molybdenum steel · Open-die forgings

AISI 4150 Forgings (SAE 4150, UNS G41500, nearest 50CrMo4 / 1.7228)

Published 18 May 2016 · Last updated 13 September 2026 · Reviewed by the Jiangyin Jiangnan Metal metallurgical engineering team

Short answer: what is AISI 4150?

AISI 4150 is a medium-carbon chromium–molybdenum low-alloy steel, designated SAE 4150 and UNS G41500, containing 0.48–0.53% carbon, 0.75–1.00% manganese, 0.80–1.10% chromium and 0.15–0.25% molybdenum.

It is the higher-carbon member of the 41xx family, identical to AISI 4140 in alloy content but carrying about 0.10% more carbon. That carbon raises the maximum as-quenched hardness to roughly 58–60 HRC and lifts tempered strength by 100–200 MPa at any given tempering temperature, at the cost of toughness and weldability. In the annealed condition it has a tensile strength of 731 MPa and a hardness of 197 HB; quenched and tempered at 540 °C it reaches about 1,207 MPa and 375 HB.

Jiangyin Jiangnan Metal Co., Ltd. forges AISI 4150 to customer drawings as seamless rolled rings, forged shafts, gear and pinion shafts, discs, blocks, sleeves, bushings, hollow bars, flanges and round, square, flat and hex bar, supplied annealed, normalised or quenched and tempered and certified to EN 10204 3.1 as standard, 3.2 with third-party witness on request. The plant forges 100–6,000 mm diameters, lengths to 12,000 mm and single pieces from 10 kg to 15,000 kg. Written quotations are issued within 24 hours from sales@steelforgepieces.com or 0086-189-2135-9659. The factory is at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China.

UNS
G41500W.Nr. 1.7228 nearest
Carbon
0.48–0.53 wt %
Density
7.85 g/cm³0.284 lb/in³
Tensile, annealed
731 MPa106,000 psi
Tensile, Q&T 540 °C
1,207 MPa175,000 psi
Max as-quenched
58–60 HRCfully martensitic
Austenitise
830–860 °Coil quench
Forge from
1,100–1,200 °Cfinish above 900 °C

What AISI 4150 forged products can you buy?

Jiangyin Jiangnan Metal produces AISI 4150 by three routes, chosen by geometry and order size. Open-die forging covers shafts, blocks, discs and heavy sections. Seamless ring rolling produces rings and gear blanks, and is almost always cheaper than machining a ring out of a solid disc. Upset forging handles short, large-section hubs and flanges. On a 0.50% carbon steel the forging route also determines the grain flow, and grain flow is what makes a forged gear or drill collar outlast a machined one.

Rings and ring gears

Seamless rolled rings, forged rings, ring gears, gear wheel blanks, retaining rings, bearing races and spacer rings in AISI 4150.

Shafts and rotating parts

Forged shafts, gear shafts, pinion shafts, spindles, eccentric shafts, axles, torsion bars and stems, rough or finish machined to drawing.

Discs, blocks and plates

Forged discs, disks, blocks, blanks, hubs, housings, plates and die blocks up to the plant envelope in the capability section.

Bars and hollow forms

Forged round bars, rods, square, rectangular, flat and hex bar; trepanned hollow bars, sleeves, bushings, cylinders, barrels, casings and shells.

Table 1. AISI 4150 forged product forms, typical size ranges and where each is used. Sizes are the plant envelope across all grades; confirm your specific part before designing to the limit.
Forged productTypical size rangeWhere it is used
AISI 4150 forged rings and seamless rolled rings200–6,000 mm OD, 40 mm minimum wallRing gears, gear wheel blanks, bearing races, retaining rings, flange blanks
AISI 4150 forged shafts, gear shafts and pinion shaftsTo 12,000 mm lengthDrive shafts, gear and pinion shafts, spindles, eccentric shafts, axles
AISI 4150 forged discs, disks and platesTo 3,000 mm diameterGear blanks, hubs, housings, die blocks, blind heads
AISI 4150 forged blocks and blanksTo 15,000 kg single pieceForging dies, die holders, near-net preforms for machined parts
AISI 4150 forged round bars, rods and square, flat, hex barØ50–1,200 mm; squares and flats to drawingMachined components, tool holders, shafting stock, upset preforms
AISI 4150 hollow bars, sleeves, bushings and bushesTo 2,000 mm OD, trepanned or boredWear sleeves, guide bushings, cylinder liners, drill collar blanks
AISI 4150 forged cylinders, barrels, casings, cases and shellsTo 2,000 mm OD, to 6,000 mm longHydraulic cylinders, extruder barrels, gearbox casings, housings
AISI 4150 forged pipes, tubes and tubingTrepanned hollows machined from forged barDownhole tool bodies, heavy-wall pressure tubes, thermowell blanks
AISI 4150 forged flanges and hubsTo 3,000 mm ODWeld-neck and blind flange blanks, coupling hubs, drive flanges
AISI 4150 forged rolls and mill rollsBarrel to 1,600 mm Ø, 15,000 kgWork rolls, back-up rolls, straightening and levelling rolls

Source: Jiangyin Jiangnan Metal Co., Ltd. open-die forging plant capability, Jiangyin, Jiangsu, China. Every form above can be supplied annealed, normalised, or quenched and tempered to a stated hardness, rough or finish machined to drawing, and certified to EN 10204 3.1 or 3.2. Send the finished drawing rather than a billet size: on a hardenable steel the forging route and the ruling section decide the achievable core properties.

What is AISI 4150, and why choose it over 4140?

The 41xx series is the workhorse family of chromium–molybdenum engineering steels. Every grade in it carries the same nominal 0.95% chromium and 0.20% molybdenum; the last two digits give the carbon content in hundredths of a percent. So 4130 is 0.30% carbon, 4140 is 0.40%, and 4150 is 0.50%.

Chromium and molybdenum do two jobs. They push the nose of the transformation curve to the right, so the steel can be quenched more slowly and still form martensite. That is hardenability, and it is why a 200 mm 4150 shaft can be hardened through where a plain carbon steel of the same carbon content could not. Molybdenum also suppresses temper embrittlement and holds strength at elevated temperature. Carbon works on a separate axis. It sets how hard the martensite can be, whatever depth it forms to.

The argument for 4150 over 4140 rests on that distinction.

  • Maximum hardness. At 0.40% carbon, fully martensitic steel tops out near 55–57 HRC. At 0.50% carbon it reaches 58–60 HRC. If a drawing calls for 55 HRC on a wear surface, 4140 is at its ceiling and 4150 is comfortable.
  • Tempered strength. At the same tempering temperature 4150 runs roughly 100–200 MPa stronger than 4140. To reach a given strength, 4150 can be tempered hotter, which leaves a more stable structure and lower residual stress.
  • Wear resistance. More carbon means more carbide and a harder tempered martensite. This is why 4150 dominates in mill rolls, drill collars and die blocks.
  • What you give up. Impact toughness at equal hardness is lower, the carbon equivalent rises to roughly 0.85–0.90 so welding needs real preheat, and the quench-cracking risk on section changes and sharp corners is materially higher.

The practical selection rule

Specify AISI 4150 when hardness, strength or wear governs the design and the part will not be welded. Specify AISI 4140 or 42CrMo4 when impact toughness, weldability or a low quench-cracking risk governs. If the requirement is a deep hard case over a tough core, consider 4140 with induction hardening or nitriding before reaching for 4150 through-hardened.

What are the equivalents of AISI 4150?

Buyers meet this steel under half a dozen names. The designations below describe the same nominal 0.50C–1Cr–0.2Mo chemistry and we accept purchase orders under any of them. They are not, however, identical: the manganese ranges differ between the American and European grades, and manganese is a hardenability element. On a thin section the difference is invisible; on a 300 mm ruling section it is the difference between a hardened core and a soft one.

Table 2. AISI 4150 equivalent and near-equivalent designations by standards body
Body / regionDesignationScope and notes
USA · SAE / AISI4150The original designation, per SAE J404. 4150H is the hardenability-guaranteed version with a Jominy band.
USA · UNSG41500The unambiguous number. Use this on drawings and purchase orders alongside the product-form standard.
USA · ASTMA29/A29M, A322, A331, A519, A646Product-form standards: hot-wrought bar, alloy bar standard grades, cold-finished bar, seamless mechanical tubing, premium-quality forging steel.
Germany / EU · EN50CrMo4, W.Nr. 1.7228The nearest European grade, EN 10083-3. Carbon, chromium and molybdenum overlap closely; manganese is 0.50–0.80% against 0.75–1.00% for 4150, so hardenability is slightly lower.
EU · forgingsEN 10250-3Open-die steel forgings for general engineering, alloy special steels. The correct product standard to cite for a European forging order.
Japan · JISSCM445JIS G4053. Carbon 0.43–0.48%, slightly lower than 4150. The nearest JIS grade, not an exact twin.
France · AFNOR50CD4NF A35-552. Direct counterpart to 50CrMo4.
China · GB50CrMo4 / 50CrMoSupplied to GB/T 3077 or GB/T 17107 for forgings. We cross-certify Chinese and American callouts on one certificate where a project needs both.
UK · BS 970No exact equivalentBS 970 has no 0.50% carbon Cr–Mo grade. 708M40 / En 19 is the nearest and carries 0.36–0.44% carbon, so it will not reach 4150 hardness. Do not substitute without re-checking the hardness requirement.
Related US grades4145, 4145H, 4147, 4161, 4140Adjacent carbon levels in the same family. 4145H modified is the usual API drill collar grade; 4150 is common for kellys and subs.

Cross-reference compiled by Jiangyin Jiangnan Metal Co., Ltd. from published national standards. Standards are cited by number only; always work to the revision in force at your contract date. A designation match is not by itself proof of equivalence. The product-form specification decides the test regime, not the chemistry.

Check the manganese row before you substitute

The most common substitution error on this grade is treating AISI 4150 and 50CrMo4 as interchangeable in a heavy section. They are close, but 50CrMo4 permits manganese as low as 0.50% where 4150 requires at least 0.75%. In a 300 mm ruling section that gap can move the core hardness by several HRC points. If the core property is on the drawing, require the actual ladle analysis before accepting the substitution, and state which specification governs.

Tool 1 of 6

AISI 4150 designation lookup

Type any name on your drawing (4150, G41500, 50CrMo4, 1.7228, SCM445, 50CD4, 4140 or 42CrMo4) and see every designation it maps to, with the carbon range so you can tell a true equivalent from a near one.

The lookup covers the chromium–molybdenum engineering steels we forge most often. Matching a name here does not by itself certify equivalence: acceptance requirements differ between product-form specifications, and manganese ranges differ between the American and European grades.

What is the chemical composition of AISI 4150?

The composition below is the SAE J404 / ASTM A29 requirement for grade 4150, and it is what we buy raw material against unless a drawing calls for a tighter band. Carbon sets the attainable hardness. Chromium and molybdenum carry the hardenability and, in molybdenum's case, the resistance to temper embrittlement. Manganese contributes hardenability and ties up sulphur.

Table 3. Chemical composition, AISI 4150 / SAE 4150 / UNS G41500 (weight %)
ElementMinMaxWhy it is there
Carbon (C)0.480.53Sets the maximum attainable martensite hardness. The only element that distinguishes 4150 from 4140.
Manganese (Mn)0.751.00Hardenability and deoxidation; combines with sulphur to prevent hot shortness during forging.
Silicon (Si)0.150.35Deoxidiser; raises strength slightly and improves temper resistance.
Chromium (Cr)0.801.10The main hardenability element here. Forms carbides that raise wear resistance and temper resistance.
Molybdenum (Mo)0.150.25Hardenability, hot strength, and suppression of temper embrittlement on slow cooling from tempering.
Phosphorus (P)0.035Residual. Segregates to prior-austenite grain boundaries and embrittles; keep it low on impact-critical parts.
Sulphur (S)0.040Residual. Forms manganese sulphide stringers that reduce transverse ductility. Specify 0.015% max if transverse impact matters.
Iron (Fe)96.7597.67Balance.

Source: SAE J404 and ASTM A29/A29M grade 4150, as forged by Jiangyin Jiangnan Metal Co., Ltd. Every heat is supplied with a ladle analysis on the mill certificate; product analysis can be added on request. Some published datasheets print silicon as 0.15–0.30% rather than 0.15–0.35%; both appear in circulation, so state which specification governs your order.

Table 4. AISI 4150 against 4150H, the hardenability-guaranteed grade (weight %)
ElementAISI 4150AISI 4150HWhat changes
Carbon0.48–0.530.47–0.54Wider band
Manganese0.75–1.000.70–1.05Wider band
Chromium0.80–1.100.75–1.20Wider band
Molybdenum0.15–0.250.15–0.25Unchanged
HardenabilityNot guaranteedJominy band guaranteedThe reason to buy the H grade

The H grade trades tighter chemistry for a guaranteed end-quench hardenability band to SAE J1268. For a heavy section where core hardness after quenching is on the drawing, specify 4150H and state the required Jominy band. For a small section where surface hardness governs, plain 4150 is normally sufficient and cheaper. Compiled by Jiangyin Jiangnan Metal Co., Ltd.

What are the physical properties of AISI 4150?

Table 5. Physical properties of AISI 4150 alloy steel
PropertyMetricImperialCondition / note
Density7.85 g/cm³0.284 lb/in³Room temperature. Used by the weight calculator on this page.
Melting point≈ 1,427 °C≈ 2,600 °FApproximate; the steel melts over a range, not at a point.
Modulus of elasticity190–210 GPa27,557–30,458 ksiTension at 20 °C. Essentially independent of heat treatment.
Shear modulus80 GPa11,600 ksiTypical for steel.
Bulk modulus140 GPa20,300 ksiTypical for steel.
Poisson's ratio0.27–0.300.27–0.30Dimensionless.
Thermal conductivity≈ 42.6 W/m·K≈ 296 Btu·in/ft²·h·°FAt 100 °C. Falls as temperature rises.
Specific heat capacity≈ 477 J/kg·K≈ 0.114 Btu/lb·°F50–100 °C mean.
Coefficient of thermal expansion≈ 12.3 µm/m·°C≈ 6.8 µin/in·°F20–100 °C mean. Rises with temperature.
Ac1 (transformation start)≈ 725 °C≈ 1,337 °FTempering must stay below this. It is why 650 °C is the practical ceiling.
Ac3 (transformation complete)≈ 770 °C≈ 1,418 °FAustenitising is set 60–90 °C above this.
Ms (martensite start)≈ 285–300 °C≈ 545–570 °FCalculated from composition. Governs quench-cracking risk and marquenching practice.
Magnetic responseFerromagneticSuitable for magnetic particle examination in any condition.

Compiled by Jiangyin Jiangnan Metal Co., Ltd. from published data for AISI 4150 and closely related 41xx grades. Transformation temperatures vary by a few degrees with the actual heat analysis and heating rate; where a heat-treatment procedure is being qualified, determine them by dilatometry on the actual heat rather than from a table.

What are the mechanical properties of AISI 4150?

There is no single set of mechanical properties for AISI 4150. The delivery condition sets the numbers, and there are three to order from: annealed, normalised, and quenched and tempered to a stated hardness or strength. Everything below is for a 25 mm test section; larger sections cool more slowly in the quench and will read lower, which is why the ruling section belongs on the enquiry.

Table 6. Mechanical properties of AISI 4150 in the annealed and normalised conditions
PropertyAnnealed (815 °C, furnace cooled)Normalised (900 °C, air cooled)
Tensile strength731 MPa · 106,000 psi1,158 MPa · 168,000 psi
Yield strength, 0.2%380 MPa · 55,100 psi731 MPa · 106,000 psi
Elongation in 50 mm20.2%11.7%
Reduction of area40.2%30.8%
Hardness, Brinell197 HB321 HB
Hardness, Rockwell92 HRB · ≈ 13 HRC≈ 35 HRC
Hardness, Vickers207 HV≈ 338 HV
Izod impact24 J · 17.7 ft·lb12 J · 8.9 ft·lb
Machinability (AISI 1212 = 100)55%Lower; machine in the annealed condition

Source: Jiangyin Jiangnan Metal Co., Ltd., AISI 4150 forging specification, compiled from published typical values for 25 mm sections. Rockwell C values below about 20 HRC are conversions outside the normal range and are given for comparison only. Annealed material is the condition to rough machine in; normalised material is the condition to buy if the part will be used as-forged without hardening.

How does AISI 4150 respond to tempering?

This is the table that actually gets used. Quench the part in oil from 830–860 °C and you have brittle martensite at 58–60 HRC that is unusable and, left overnight, liable to crack on its own. Tempering trades that hardness back for toughness, and the tempering temperature is the single control you have over the finished properties.

The colour bands below are the actual oxide tempering colours that form on a clean steel surface at each temperature. Before pyrometers they were how the heat treater read the temperature, and on a bright-machined part they still tell you at a glance roughly where a temper ran.

205 °C400 °F
1,931 MPa · 280 ksi · 578 HB · ≈55 HRCMaximum strength. Elongation 10%, RA 39%. Wear surfaces only; almost no impact capacity.
315 °C600 °F
1,765 MPa · 256 ksi · 534 HB · ≈52 HRCInside the tempered-martensite embrittlement range. Avoid as a final temper on impact-loaded parts.
370 °C700 °F
≈1,640 MPa · 238 ksi · ≈500 HB · ≈50 HRCUpper end of the embrittlement trough. Interpolated between the 315 and 425 °C points.
425 °C800 °F
1,517 MPa · 220 ksi · 461 HB · ≈48 HRCElongation 12%, RA 45%. Common for gears, drill collars and heavily loaded shafts.
540 °C1,000 °F
1,207 MPa · 175 ksi · 375 HB · ≈40 HRCElongation 15%, RA 52%. The general-purpose condition for shafts, spindles and axles.
650 °C1,200 °F
965 MPa · 140 ksi · 302 HB · ≈32 HRCElongation 19%, RA 60%. Maximum toughness. Cool rapidly from this temper.

Table 7. Typical properties of AISI 4150 oil quenched from 830 °C and tempered, 25 mm section, one hour at temperature. Source: Jiangyin Jiangnan Metal Co., Ltd., compiled from published typical values for SAE 4150. These are typical results for screening, not design allowables, and not acceptance minima. Acceptance values are set by the specification on your order and are what appear on the certificate.

Two tempering ranges to avoid

Tempered martensite embrittlement, 250–375 °C. Impact toughness falls into a trough here even though hardness is behaving normally. It is caused by carbide films forming on prior-austenite grain boundaries and it cannot be undone by re-tempering elsewhere. Do not use this range as a final temper on any part that sees impact.

Classic temper embrittlement, 375–575 °C with slow cooling. Chromium-bearing steels held in or cooled slowly through this range lose toughness through phosphorus segregation to grain boundaries. The molybdenum in 4150 suppresses it but does not eliminate it. Cool rapidly in water or forced air from any temper above about 575 °C rather than letting the part cool in the furnace.

Tool 2 of 6

AISI 4150 tempering calculator

Work in either direction. Set a tempering temperature to see the properties it produces, or enter the hardness your drawing calls for and read back the tempering temperature to specify.

Interpolated from published typical values for SAE 4150 oil quenched from 830 °C, 25 mm section, one hour at temperature. The section-size correction is a first-pass mass-effect estimate, not a hardenability calculation. For a heavy section specify 4150H with a Jominy band and qualify on a test coupon from the same heat.

AISI 4150 compared with 4140, 4145, 4340 and 1045

Most enquiries come down to this comparison. AISI 4150 is chosen over 4140 when hardness or wear governs, and over 4340 when cost governs and the section is not very heavy. It loses on toughness, on weldability and on quench-cracking risk.

Table 8. AISI 4150 against the grades it competes with in forgings
PropertyAISI 4150
G41500
AISI 4140
G41400
AISI 4145
G41450
AISI 4340
G43400
AISI 1045
G10450
Carbon %0.48–0.530.38–0.430.43–0.480.38–0.430.43–0.50
Chromium %0.80–1.100.80–1.100.80–1.100.70–0.90none
Molybdenum %0.15–0.250.15–0.250.15–0.250.20–0.30none
Nickel %nonenonenone1.65–2.00none
Max as-quenched hardness58–60 HRC55–57 HRC56–58 HRC55–57 HRC55–58 HRC surface only
HardenabilityGoodGoodGoodExcellentPoor
Toughness at equal hardnessModerateGoodModerateExcellentLow
WeldabilityDifficult, CE ≈ 0.87Difficult, CE ≈ 0.76DifficultDifficultFair, CE ≈ 0.61
Quench-cracking riskHighModerateModerate-highModerateHigh in water
Relative costLowLowLowHighLowest
Choose it whenHardness above 50 HRC or wear governsToughness and weldability matterAPI drill collar workVery heavy section must through-harden toughCost governs, low duty

Comparison compiled by Jiangyin Jiangnan Metal Co., Ltd. Carbon equivalent calculated to the IIW formula at mid-range composition. All five grades are forged in this plant; see alloy steel grades for the full list.

Three questions that settle the choice

  1. Is the hardness requirement above about 50 HRC? If yes, 4140 is at or past its practical ceiling and 4150 is the right answer.
  2. Does the part take impact, or will it be welded? If yes, the extra carbon is working against you. Use 4140 or 42CrMo4 and get the hardness from induction hardening or nitriding instead.
  3. Is the ruling section above roughly 150 mm and must the core be hard? Then hardenability, not carbon, is the limiting factor. Specify 4150H with a Jominy band, or move to 4340.

Tool 3 of 6

Grade substitution check

Tell it what is specified now and what you are trying to gain. It says whether moving to or from AISI 4150 is defensible, and what to watch.

Screening guidance from published behaviour of these grades. A substitution is only final when the design authority has signed it off. Parts made to API, ASME or an OEM specification cannot be substituted without that body's approval.

How is AISI 4150 forged and heat treated?

At 0.50% carbon with 1% chromium, this steel is hardenable enough to harden itself. A heavy forging left to cool in still air forms bainite and martensite in the skin while the core is still hot and contracting, and the resulting stresses crack parts. Most of the process rules below exist to manage that.

  1. Verify the billet

    Confirm the heat analysis against SAE J404 / ASTM A29 grade 4150 and record the heat number. EAF + ladle furnace + vacuum degassing is our standard melt route; electroslag remelting is available where the drawing calls for it or where the part is ultrasonically critical.

  2. Charge cold, heat slowly

    Charge below 400 °C and raise the temperature gradually. A cold 4150 billet pushed straight into a hot furnace develops a thermal gradient the material cannot accommodate.

  3. Soak at 1,100–1,200 °C

    Roughly 30 minutes per 25 mm of ruling section, so the core reaches temperature and not just the surface. Do not exceed about 1,220 °C: at this carbon level the grain coarsens quickly and the coarse grain will still be there after quenching.

  4. Forge, finishing above 900 °C

    Aim for a minimum 3:1 reduction ratio to break down the cast structure and develop grain flow. Reheat rather than continue deforming a cooling billet. Below about 900 °C forging loads climb steeply and surface cracking risk rises.

  5. Cool slowly from the forging heat

    Cool in still air to about 400 °C, then cover, bury or furnace cool. This is the step most often skipped and it is the most common cause of cracked 4150 forgings arriving at the heat treatment shop.

  6. Normalise at 860–900 °C

    Air cool. Refines the coarse as-forged grain and produces a uniform structure so the subsequent hardening responds predictably. Expect about 321 HB after normalising.

  7. Anneal if rough machining follows

    Full anneal at 800–830 °C, furnace cool at 10–20 °C per hour to 600 °C, then air cool. Gives roughly 197 HB, the softest practical condition and the one to machine in.

  8. Austenitise at 830–860 °C and oil quench

    Soak through, then quench in agitated oil. Water and polymer quenching are not recommended at this carbon level. The cracking risk on section changes outweighs the extra hardness. Radius every corner and avoid abrupt section changes at the design stage.

  9. Temper immediately

    Temper as soon as the part reaches roughly 60 °C. Two hours per 25 mm of section, minimum two hours, at the temperature your hardness requires. Leaving quenched 4150 untempered overnight is how parts crack in the rack.

  10. Test, examine and certify

    Tensile, impact and hardness testing, ultrasonic examination to ASTM A388 or EN 10228-3 and magnetic particle examination to ASTM E709 where the order calls for it. EN 10204 3.1 certification as standard, 3.2 with third-party witness.

Table 9. AISI 4150 heat-treatment windows
OperationTemperatureCoolingResult
Forging1,100–1,200 °C, finish > 900 °CStill air to 400 °C, then covered or furnaceGrain flow developed; no quench cracks
Normalising860–900 °CAir≈ 321 HB, refined uniform grain
Full annealing800–830 °CFurnace, 10–20 °C/h to 600 °C≈ 197 HB, best machinability
Stress relief (as-forged)600–680 °CFurnace to 400 °C, then airResidual stress removed before machining
Hardening830–860 °CAgitated oil58–60 HRC as quenched, fully martensitic
Tempering200–650 °CAir; rapid cool above 575 °C55 HRC down to 32 HRC per Table 7
Nitriding500–530 °CFurnaceCase 600–650 HV, 0.2–0.6 mm deep
Induction hardening870–900 °C surfaceWater or polymer spraySurface 55–60 HRC over a tough core

Source: Jiangyin Jiangnan Metal Co., Ltd. heat-treatment practice for AISI 4150 open-die forgings, Jiangyin, Jiangsu, China. Furnaces are temperature-uniformity surveyed with chart recording; charts are supplied with the certificate. These are starting windows, not a qualified procedure. Qualify on coupons from the same heat, with thermocouples on the part, before releasing production parts.

Tool 4 of 6

Forge and heat-treatment cycle generator

Enter the ruling section and the hardness you need. The tool writes a printable cycle for your forge shop or heat-treatment subcontractor, using the standard 30 minutes per 25 mm soak rule and two hours per 25 mm for tempering.

Starting cycles, not a qualified procedure. Soak times assume a single piece in a surveyed furnace; a loaded basket needs more. Qualify on coupons from the same heat, with thermocouples on the part and a chart record, before releasing production parts.

Can AISI 4150 be nitrided or induction hardened?

Yes to both, and on many parts one of them is a better answer than through-hardening to high hardness.

Gas or plasma nitriding

The 1% chromium and 0.2% molybdenum form stable nitrides, so 4150 nitrides well. Treat at 500–530 °C for 10–60 hours to give a case of roughly 600–650 HV, 0.2–0.6 mm deep. The part must first be quenched and tempered above the nitriding temperature, normally at 580–620 °C, or the core will soften during the treatment. Distortion is minimal because there is no quench.

Induction or flame hardening

Heat the surface to 870–900 °C and spray quench to give 55–60 HRC over a tough quenched-and-tempered core. The usual route for journals, gear teeth, wear tracks and roll barrels. Temper at 150–200 °C afterwards to relieve the case. Case depth is set by the frequency and the heating time.

Carburising

Not appropriate. At 0.50% carbon the core already responds fully to hardening, so there is nothing to gain and the long carburising cycle coarsens the grain. If a case-hardened part is wanted, start from a low-carbon grade.

Chrome plating and coatings

Hard chrome plating is common on 4150 hydraulic rods and roll surfaces. Bake at 190–210 °C for four hours or more after plating to drive off absorbed hydrogen. At this strength level 4150 is susceptible to hydrogen embrittlement and the bake is not optional.

Welding and machining AISI 4150

Welding

AISI 4150 is weldable but unforgiving. The carbon equivalent to the IIW formula is roughly 0.87 at mid-range composition, far above the 0.45 threshold at which preheat becomes mandatory. Weld metal and heat-affected zone both transform to untempered martensite on cooling, and with hydrogen present that martensite cracks.

  • Weld in the annealed or normalised condition wherever the design allows.
  • Preheat to 300–400 °C and maintain the interpass temperature. Do not let the part fall below preheat between passes.
  • Use low-hydrogen consumables, dried and held in a quiver. Hydrogen is the variable most often ignored and most often responsible.
  • Post-weld: either stress relieve at 600–680 °C, or re-temper below the original tempering temperature if the part is already quenched and tempered. Go straight from welding to the furnace without letting the part cool to room temperature.
  • On a fully hardened part above 45 HRC, treat welding as a repair operation requiring a qualified procedure, not a shop-floor task.

Machining

Machinability is about 55% of the AISI 1212 free-machining reference in the annealed and cold-drawn condition. The practical window is 180–230 HB; below that the steel smears, above about 300 HB tool life falls away quickly.

  • Rough machine annealed or normalised, leaving stock for heat-treatment distortion, then quench, temper and finish machine.
  • Above 40 HRC, plan on carbide or CBN tooling, rigid setups, and finishing by grinding rather than turning.
  • Deep holes and keyways are stress raisers in a quenched part. Where possible machine them before hardening, and radius every internal corner.
  • Resulphurised variants give better chip control but reduce transverse ductility. Do not specify one for an impact-loaded forging.

How do AISI 4150 parts fail, and how do you prevent it?

Quench cracking

Cause: sharp internal corners, abrupt section changes, a quench that is too severe, or a delay between quenching and tempering. Prevention: oil rather than water, radius every corner, temper as soon as the part reaches 60 °C, and magnetic particle examine after tempering rather than before.

Temper embrittlement

Cause: slow cooling through 375–575 °C after tempering, with phosphorus segregating to grain boundaries. Prevention: cool rapidly from tempers above 575 °C and specify phosphorus at 0.020% maximum on impact-critical parts.

Soft core in a heavy section

Cause: the ruling section exceeded the hardenability of the heat. Prevention: specify 4150H with a Jominy band, state the hardness at a defined depth rather than at the surface, and test at that depth on a prolongation.

Hydrogen embrittlement

Cause: plating, pickling or welding a part above roughly 40 HRC without baking. Failure is delayed, often days after assembly. Prevention: bake at 190–210 °C for four hours or more within 4 hours of plating.

Coarse grain from over-soaking

Cause: forging or austenitising above about 1,220 °C, or excessive soak time. The coarse grain survives into the finished part and shows up as low impact energy. Prevention: control soak time as well as temperature, normalise after forging, and state a maximum grain size to ASTM E112.

Fatigue from a machined stress raiser

Cause: a sharp fillet, tool mark or hard-turned surface in a high-strength condition. At 1,500 MPa the steel has very little notch tolerance. Prevention: generous fillet radii, controlled surface finish on fatigue-critical areas, and shot peening where the duty warrants.

What can Jiangyin Jiangnan Metal forge in AISI 4150?

AISI 4150 is one of our routine alloy steel grades. We hold billet in the common sizes and buy to specification for anything heavier, which is why lead times on this grade are short compared with the nickel and cobalt alloys.

Diameter range
100–6,000 mm
Length
to 12,000 mm
Single piece
10–15,000 kg
Rolled ring OD
200–6,000 mm
Ring wall, min
40 mm
Bar diameter
50–1,200 mm
Condition
Q&Tannealed or normalised also
Lead time
4–8 weekstypical for this grade

Forging

1, 3, 5 and 9 tonne open-die hammers; 4,500 and 5,000 tonne hydraulic presses; 3 m and 6 m seamless ring rolling lines.

Heat treatment

Bogie-hearth and car-bottom furnaces with temperature uniformity survey and chart recording; agitated oil, polymer and water quench tanks with controlled transfer times; tempering furnaces to 700 °C.

Inspection

Optical emission spectrometer, universal tensile machine, Charpy and Izod impact machines, Brinell and Rockwell hardness testers, magnetic particle and penetrant lines, ultrasonic flaw detection, metallographic microscope.

Machining

Vertical and horizontal lathes, boring mills, gear hobbing and machining centres for rough or finish machining to drawing, with in-process dimensional records.

Jiangyin Jiangnan Metal Co., Ltd. employs approximately 460 people including 9 senior engineers and 32 intermediate engineers, at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China. The envelope above is the plant capability across all grades. Send the drawing and we will confirm the size, weight and lead time for your specific part before quoting.

Which standards and certificates apply to AISI 4150 forgings?

Material and product

  • SAE J404, chemical composition of SAE alloy steels
  • SAE J1268, hardenability bands for 4150H
  • ASTM A29/A29M, hot-wrought bar general requirements
  • ASTM A322, alloy steel bars, standard grades
  • ASTM A331, cold-finished alloy steel bars
  • ASTM A519, seamless mechanical tubing
  • ASTM A646, premium-quality alloy steel blooms and billets for aircraft and aerospace forgings
  • EN 10083-3, steels for quenching and tempering (50CrMo4)
  • EN 10250-3, open-die steel forgings, alloy special steels
  • GB/T 3077 and GB/T 17107 for Chinese callouts

Testing and examination

  • Tensile: ASTM E8/E8M or ISO 6892-1
  • Impact: ASTM E23 or ISO 148-1, at a stated temperature
  • Hardness: ASTM E10 Brinell, ASTM E18 Rockwell
  • Ultrasonic: ASTM A388, EN 10228-3, SEP 1921
  • Magnetic particle: ASTM E709 or ISO 9934
  • Penetrant: ASTM E165 or ISO 3452
  • Grain size: ASTM E112; macroetch ASTM E381
  • Jominy end-quench hardenability: ASTM A255
  • Chemistry: optical emission spectrometry, wet-chemical umpire analysis on request

Quality management is certified to ISO 9001:2015. Third-party witness certificates are issued through the inspection body you nominate: Lloyd's Register, DNV, Bureau Veritas, ABS, TÜV or SGS. Customers keep an unrestricted right to witness any production stage, including chemistry, forging, heat treatment and mechanical testing.

How do you specify an AISI 4150 forging order?

  1. Name the grade and the product standard. Write AISI 4150 / UNS G41500 together with the product-form standard, for example ASTM A29 for bar or EN 10250-3 for an open-die forging. Chemistry alone does not define an acceptance regime.
  2. State the delivery condition. Annealed, normalised, or quenched and tempered. If quenched and tempered, give the hardness or strength required, not just the words.
  3. Give the hardness at a depth. "40–44 HRC at mid-radius" is a specification. "40 HRC" on its own means the surface, and on a heavy section the surface will pass while the core does not.
  4. State the ruling section. It sets the soak times, the quench severity and whether 4150 or 4150H is needed. It is the single most useful number on the enquiry.
  5. Specify 4150H if hardenability is critical. Name the required Jominy band to SAE J1268 and the distance at which it applies.
  6. Define the test regime. Tensile and impact temperature and direction, test location, and whether tests come from a prolongation or a separately forged coupon. Above 50 mm section, say whether tests are longitudinal or transverse.
  7. Define NDE and the acceptance class. "UT per EN 10228-3, quality class 3" or "UT per ASTM A388 with acceptance per the purchase order". An unqualified "ultrasonic test" is not a specification.
  8. Cap the residuals if impact matters. Phosphorus 0.020% max and sulphur 0.015% max are worth specifying on impact-critical forgings, and cost very little.
  9. Give quantity, date, Incoterm and destination. Quantity drives the melt and the machining setup, and both affect price and schedule.

Drawing callout you can copy

MATERIAL:      AISI 4150 / SAE 4150 / UNS G41500
               (nearest EN grade 50CrMo4 / 1.7228 - state which governs)
SPECIFICATION: ASTM A29/A29M grade 4150 (bar) or EN 10250-3 (open-die forging)
               SAE J1268 hardenability band if 4150H is required
MELT ROUTE:    EAF + LF + VD (state ESR if required)
FORGING:       Minimum 3:1 reduction ratio, finish above 900 deg C,
               cooled in still air to 400 deg C then covered
CONDITION:     Quenched and tempered. Austenitise 830-860 deg C, oil quench,
               temper ______ deg C, 2 h per 25 mm, minimum 2 h
HARDNESS:      ______ HRC at ______ mm depth / at mid-radius, per ASTM E18
CHEMISTRY:     Report all elements. P 0.020% max, S 0.015% max
TENSILE:       Per ASTM E8/E8M, ______ direction, from prolongation
IMPACT:        Charpy V per ASTM E23, ______ J average at ______ deg C
GRAIN SIZE:    ASTM E112, ______ or finer, reported per piece
NDE:           UT per EN 10228-3 quality class 3 (or ASTM A388)
               MT per ASTM E709 after final tempering
CERTIFICATE:   EN 10204 3.1 (3.2 with third-party witness if stated on the PO)
MARKING:       Heat number, specification, condition and drawing number,
               low-stress stamped or vibro-etched

Seven mistakes buyers make with AISI 4150

  1. Ordering "4150, 50 HRC" with no depth and no section. Surface hardness on a 400 mm forging tells you nothing about the core. State the hardness, the depth and the ruling section together.
  2. Assuming 50CrMo4 is an exact substitute. It permits manganese down to 0.50% where 4150 requires 0.75% minimum. On a heavy section that changes the core hardness.
  3. Specifying 4150 for a welded fabrication. Carbon equivalent 0.87 means 300–400 °C preheat and mandatory post-weld heat treatment. If it must be welded, 4140 or 42CrMo4 will cost less overall.
  4. Tempering in the 250–375 °C range for an impact-loaded part. Hardness looks right, toughness is in a trough, and no later treatment recovers it.
  5. Water quenching to chase hardness. At 0.50% carbon this cracks parts. Oil quench and accept the hardenability limit, or move to 4150H or 4340.
  6. Skipping the normalise after forging. As-forged grain is coarse and non-uniform, and the subsequent hardening will be equally non-uniform. Normalising costs one furnace cycle and prevents a scrapped part.
  7. Buying to a billet size instead of a drawing. On a hardenable steel the forging route and the ruling section decide the achievable properties. Send the finished drawing and let the route be chosen for it.

Tool 5 of 6

AISI 4150 forging weight calculator

Pick a shape, enter the finished dimensions and get the net weight at 7.85 g/cm³ plus a rough forging weight with machining stock. Forgings are priced per kilogram, so this is usually the first number you need.

Net finished weight at 7.85 g/cm³. Our single-piece limit is 15,000 kg and maximum diameter 6,000 mm. On a ring geometry, compare the ring-rolled weight against machining from a solid disc. Ring rolling often halves the purchased weight.

Tool 6 of 6

AISI 4150 RFQ writer

Fill in what you know and it writes a complete, unambiguous enquiry you can paste into email or WhatsApp. Nothing is submitted from this tool; the text stays in your browser.

We answer enquiries within 24 hours with price, lead time and the standards we will certify to.

Ask for an AISI 4150 quotation

Send the drawing, the specification and the quantity. We answer within 24 hours with price, lead time and the certificate we will issue.

Email us instead WhatsApp

If the form does not reach you, write directly to sales@steelforgepieces.com or call 0086-189-2135-9659.

Where is AISI 4150 used?

Oil and gas drilling

Drill collars, kellys, subs, crossovers, stabiliser bodies, downhole tool housings and drilling jar components. The grade is chosen for through-hardened strength in thick wall sections and for resistance to the wear that comes with rotating steel in an abrasive hole.

Rolling mills

Forged work rolls, back-up rolls, straightening and levelling rolls and roll necks. The carbon gives the barrel surface hardness and the chromium gives the depth, so the roll can be reground many times before the hardness falls away.

Gears and power transmission

Heavy gears, pinions, ring gears, gear wheel blanks, gear shafts, pinion shafts, sprockets and couplings, usually quenched and tempered to a tough core with the teeth induction hardened or nitrided.

Shafts and rotating machinery

Drive shafts, spindles, eccentric shafts, axles, torsion bars and crankshafts where the strength requirement sits above what 4140 will carry.

Dies and tooling

Forging die blocks, die holders, bolsters, punch and shear components, tool holders and press tooling that needs hardness without the cost of a true hot-work tool steel.

Heavy industry and hydraulics

Hydraulic cylinder rods and bodies, extruder barrels, crusher and mill components, wear sleeves, guide bushings and general heavy-section machine parts.

Two worked examples

Example 1: choosing between 4140 and 4150 for a ring gear

Given. A 1,200 mm outside diameter ring gear, 180 mm wall, teeth to be induction hardened to 55 HRC over a core at 280–320 HB, moderate shock loading from a mill drive.

Assessment. The 55 HRC tooth requirement is right at the ceiling of what 4140 will give after induction hardening, and the ceiling is where scatter turns into rejections. AISI 4150 reaches 58–60 HRC as quenched, so 55 HRC on the tooth flank is comfortable rather than marginal. The core requirement, 280–320 HB, is roughly 30–34 HRC and corresponds to a temper near 620 °C in 4150. That is above the temper-embrittlement range, so the ring must be cooled rapidly from the temper rather than furnace cooled.

Decision. Specify AISI 4150, seamless rolled ring, quenched and tempered to 280–320 HB at mid-wall, rapid cool from temper, teeth induction hardened to 55 HRC minimum with the case depth stated, magnetic particle examined after the final temper. Roll it as a ring rather than machine it from a disc. That saves cost, and in a ring gear the circumferential grain flow is a real service benefit rather than only a saving.

Example 2: why a rolled ring beats a machined disc

Given. A finished ring, 620 mm OD × 420 mm ID × 200 mm high, in AISI 4150.

Method. Net volume = π/4 × (0.620² − 0.420²) × 0.200 = 0.0327 m³. At 7,850 kg/m³ that is 257 kg finished. Rolled as a ring with 25% machining stock, the forging is about 321 kg. Machined instead from a solid forged disc of the same outside diameter and height, the input is 474 kg bare, or roughly 545 kg once stock is added to the diameter and the faces. Of that, 218 kg ends up as swarf.

Result. Ring rolling saves roughly a third of the purchased weight on this geometry, and rather more of the machining time. The saving grows as the wall gets thinner. At 480 mm bore instead of 420 mm it approaches half. Run both numbers through the weight calculator above with your own dimensions. Its defaults are set to this example, so the figures reproduce. This is also why we ask for the finished drawing rather than a billet size on every enquiry.

Glossary

Table 10. Terms used on this page
TermMeaning
AISI 4150 / SAE 4150Medium-carbon chromium–molybdenum engineering steel, 0.50% nominal carbon. The last two digits of a 41xx designation give the carbon in hundredths of a percent.
UNS G41500Unified Numbering System designation. The unambiguous way to specify this steel on a drawing or purchase order.
4150HThe hardenability-guaranteed version: wider chemistry bands, but a guaranteed Jominy end-quench band to SAE J1268.
HardenabilityHow deeply martensite forms for a given quench, set by the alloy content. Distinct from hardness, which is how hard that martensite is, and is set by carbon.
Jominy end-quenchA standard test to ASTM A255 in which one end of a bar is water sprayed and hardness is measured along its length. The resulting curve is the hardenability band.
Ruling sectionThe greatest thickness through which heat must travel during heat treatment. It sets soak times and the achievable core properties, not the part's overall size.
Quenching and tempering (Q&T)Austenitise, quench to martensite, then reheat below Ac1 to trade hardness for toughness. The standard delivery condition for this grade.
Ms temperatureThe temperature at which martensite starts forming during the quench, about 285–300 °C for this composition. Governs quench-cracking risk.
Tempered martensite embrittlementA toughness trough at roughly 250–375 °C caused by carbide films on prior-austenite grain boundaries. Not recoverable by re-tempering elsewhere.
Temper embrittlementToughness loss from slow cooling through 375–575 °C, caused by phosphorus segregating to grain boundaries. Suppressed but not eliminated by molybdenum.
Carbon equivalent (CE)A single number combining carbon and alloy content to predict weldability. Above 0.45 preheat is required; AISI 4150 is roughly 0.87.
Reduction ratioThe ratio of starting to finished cross-section in forging. A minimum of 3:1 is normally required to break down the cast structure and develop grain flow.
ProlongationAn extension forged onto the part, heat treated with it and cut off for mechanical testing, so the test result represents the part rather than a separate coupon.
EN 10204 3.1 / 3.2Certificate types. 3.1 is issued by the manufacturer's own independent inspection function; 3.2 is countersigned by a third party or the buyer's representative.

AISI 4150 frequently asked questions

What is AISI 4150 steel?

AISI 4150 is a medium-carbon chromium–molybdenum low-alloy steel designated UNS G41500, containing 0.48–0.53% carbon, 0.75–1.00% manganese, 0.80–1.10% chromium and 0.15–0.25% molybdenum. It is the higher-carbon member of the 41xx family, sitting above AISI 4140. It is bought for quenched-and-tempered forgings that need high strength, deep hardening and wear resistance, such as drill collars and kellys, mill rolls, gears, shafts, axles and forging dies.

What is the chemical composition of AISI 4150?

In weight percent: carbon 0.48–0.53, manganese 0.75–1.00, silicon 0.15–0.35, chromium 0.80–1.10, molybdenum 0.15–0.25, phosphorus 0.035 maximum, sulphur 0.040 maximum, iron balance at roughly 96.7–97.7%. The H-grade 4150H widens those bands to carbon 0.47–0.54, manganese 0.70–1.05 and chromium 0.75–1.20, and adds a guaranteed hardenability band.

What is the difference between AISI 4140 and AISI 4150?

Carbon is the only significant difference: 0.38–0.43% in 4140 against 0.48–0.53% in 4150. Chromium and molybdenum are identical. The extra carbon raises the maximum as-quenched hardness from about 55–57 HRC to about 58–60 HRC, raises tempered strength by roughly 100–200 MPa at the same tempering temperature, and improves wear resistance. It costs toughness and weldability, and raises the risk of quench cracking. Choose 4150 when hardness or wear governs and 4140 when impact toughness or welding governs.

What is the European equivalent of AISI 4150?

The nearest European grade is 50CrMo4, W.Nr. 1.7228, in EN 10083-3. The carbon, chromium and molybdenum ranges overlap closely, but 50CrMo4 specifies manganese at 0.50–0.80% against 0.75–1.00% for AISI 4150, so hardenability is slightly lower. The grades are normally accepted as interchangeable for general engineering, but for a hardenability-critical heavy section state which specification governs and require the actual ladle analysis before substituting.

What hardness can AISI 4150 reach?

Fully martensitic AISI 4150 reaches approximately 58–60 HRC as quenched. After tempering, typical hardness is about 55 HRC at 205 °C, 52 HRC at 315 °C, 48 HRC at 425 °C, 40 HRC at 540 °C and 32 HRC at 650 °C. In the annealed condition it is about 197 HB and normalised about 321 HB. Hardness in a real part depends on section size, quench severity and position, so specify the hardness at a stated depth rather than at the surface alone.

Is AISI 4150 weldable?

It is weldable but difficult. The carbon equivalent is roughly 0.85–0.90, well above the 0.45 threshold at which preheat becomes mandatory. Weld in the annealed or normalised condition where possible, preheat to 300–400 °C, maintain interpass temperature, use low-hydrogen consumables, and stress relieve or re-temper immediately after welding below the original tempering temperature. Welding fully hardened 4150 without preheat will produce hydrogen cracking in the heat-affected zone.

What is the forging temperature of AISI 4150?

Forge from 1,100–1,200 °C (2,010–2,190 °F) and finish above 900 °C (1,650 °F). Heat slowly from below 400 °C and soak approximately 30 minutes per 25 mm of ruling section. After forging, cool in still air to about 400 °C then cover or furnace cool: at this carbon and alloy content heavy sections will air harden and can crack if cooled quickly. Normalise at 860–900 °C before hardening.

What are the mechanical properties of AISI 4150 in the annealed condition?

Annealed AISI 4150 has a tensile strength of approximately 731 MPa (106,000 psi), yield strength 380 MPa (55,100 psi), elongation in 50 mm of 20.2%, reduction of area 40%, Brinell hardness 197 and Izod impact energy 24 J (17.7 ft·lb). Normalised at 900 °C it rises to about 1,158 MPa tensile, 731 MPa yield and 321 HB with elongation around 11.7%.

How is AISI 4150 heat treated?

Normalise at 860–900 °C and air cool. Full anneal at 800–830 °C with furnace cooling to 600 °C gives about 197 HB. Harden by austenitising at 830–860 °C and quenching in agitated oil. Temper immediately at 200–650 °C for two hours per 25 mm of section, choosing the temperature from the required hardness. Avoid tempering in the 250–375 °C tempered-martensite embrittlement range, and cool rapidly from tempers above 575 °C to avoid temper embrittlement in this chromium-bearing steel.

What sizes of AISI 4150 forgings can Jiangyin Jiangnan Metal produce?

Jiangyin Jiangnan Metal Co., Ltd. forges diameters from 100 mm to 6,000 mm, lengths to 12,000 mm and single-piece weights from 10 kg to 15,000 kg. The plant runs 1, 3, 5 and 9 tonne open-die hammers, 4,500 and 5,000 tonne hydraulic presses and 3 m and 6 m seamless ring rolling lines. Send the finished drawing rather than a billet size so the forging route can be chosen before quoting.

Is AISI 4150 the same as 4150H?

No. 4150H is the hardenability-guaranteed version. It has wider chemistry bands but adds a guaranteed Jominy end-quench hardenability band, which 4150 does not carry. For a heavy section where the core hardness after quenching matters, specify 4150H and state the required Jominy band; for a small section where surface hardness governs, plain 4150 is usually sufficient and cheaper.

What is AISI 4150 used for?

Oil and gas drilling hardware such as drill collars, kellys, subs and downhole tool bodies; forged steel mill rolls and back-up rolls; heavy gears, pinions and ring gears; shafts, spindles, axles and torsion bars; sprockets, couplings and hydraulic cylinder rods; and forging and die blocks. It is chosen where the part must be through-hardened to high strength and resist wear.

What certificates are supplied with AISI 4150 forgings?

EN 10204 3.1 inspection certificates are supplied as standard and EN 10204 3.2 with third-party witness on request, through Lloyd's Register, DNV, Bureau Veritas, ABS, TÜV or SGS. The certificate carries the ladle analysis, heat number, heat-treatment condition and chart records, tensile and impact results, hardness, and any ultrasonic or magnetic particle examination called for on the order. Quality management is certified to ISO 9001:2015.

Can AISI 4150 be nitrided or induction hardened?

Yes to both. The 1% chromium and 0.2% molybdenum form stable nitrides, so gas or plasma nitriding at 500–530 °C gives a case of roughly 600–650 HV with minimal distortion, provided the part is first quenched and tempered above the nitriding temperature. Induction hardening of the quenched-and-tempered part gives a surface of 55–60 HRC over a tough core, and is the usual route for journals, gear teeth and wear tracks.

What is the machinability of AISI 4150?

Approximately 55% of the AISI 1212 free-machining reference in the annealed and cold drawn condition. Best machinability is between about 180 and 230 HB. Rough machine in the annealed or normalised condition, then quench, temper and finish machine, leaving stock for heat-treatment distortion. Above about 40 HRC, expect carbide or ceramic tooling, rigid setups and finishing by grinding.

References

  1. SAE International, SAE J404: Chemical Compositions of SAE Alloy Steels. The source of the 4150 composition band.
  2. SAE International, SAE J1268: Hardenability Bands for Alloy H Steels. Covers 4150H.
  3. ASTM International, ASTM A29/A29M: General Requirements for Steel Bars, Carbon and Alloy, Hot-Wrought; and ASTM A322: Steel Bars, Alloy, Standard Grades.
  4. ASTM International, ASTM A255: Determining Hardenability of Steel (Jominy end-quench test).
  5. CEN, EN 10083-3: Steels for quenching and tempering — Alloy steels, covering 50CrMo4 / 1.7228; and EN 10250-3: Open-die steel forgings for general engineering purposes — Alloy special steels.
  6. ASM International, ASM Handbook, Volume 1: Properties and Selection: Irons, Steels and High-Performance Alloys. Composition and property data for the 41xx series.
  7. ASM International, ASM Handbook, Volume 4: Heat Treating. Tempering response, temper embrittlement and quench-cracking mechanisms in low-alloy steels.
  8. ASM International, ASM Handbook, Volume 14A: Metalworking: Bulk Forming. Forging practice for medium-carbon low-alloy steels.
  9. ASTM A388/A388M and EN 10228-3, ultrasonic examination of forgings; ASTM E709 magnetic particle examination; ASTM E112 grain size; ASTM E8/E8M and E23 tensile and impact testing; ASTM E10 and E18 hardness testing.
  10. CEN, EN 10204: Metallic products — Types of inspection documents.

Standards are cited by number; always work to the revision in force at your contract date. Property values on this page are published typical figures for screening and are not design allowables. Test results on our certificates are independent and traceable to calibrated equipment.

About the manufacturer, and how to cite this page

Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China, with approximately 460 employees including 9 senior and 32 intermediate engineers. The plant runs 1 to 9 tonne open-die hammers, 4,500 and 5,000 tonne hydraulic presses and 3 m and 6 m seamless ring rolling lines, with in-house heat treatment, machining, mechanical testing and non-destructive examination. Alongside AISI 4150 we forge carbon, alloy and tool steels, the precipitation-hardening and duplex stainless families, and the nickel and cobalt high-temperature alloys. Quality management is certified to ISO 9001:2015; material is supplied with EN 10204 3.1 certification as standard and 3.2 with third-party witness on request.

Cite this page

Jiangyin Jiangnan Metal Co., Ltd. (2026). AISI 4150 / SAE 4150 / UNS G41500 forgings: composition, quenched-and-tempered properties and ordering guide. Updated 13 September 2026. Retrieved from https://www.steelforgepieces.com/Alloy-Steel/AISI-4150.html

Contact for technical questions or a quotation: Jiangyin Jiangnan Metal Co., Ltd., No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China · 0086-189-2135-9659 · sales@steelforgepieces.com · WhatsApp