Forged rings
Open-die forged and mandrel forged rings for bearing races, retaining rings and structural couplings.
Form Open-die · mandrel forged
Condition Annealed or aged
Also known as Maraging 350 · 18Ni(350) · 18Ni1900 · X2NiCoMo18-12-4
Jiangyin Jiangnan Metal Co., Ltd. forges 1.6356 maraging steel into rings, shafts, flanges, discs, sleeves and tube sheets to customer drawings. 1.6356 is an 18% nickel iron-based martensitic precipitation-hardening steel that reaches a minimum tensile strength of 2345 MPa (340 ksi) and up to 56 HRC after ageing, which puts it among the strongest steels sold commercially.
Supplied solution annealed for machining, or solution annealed and aged. Ultrasonic testing to EN 10228-3, SEP 1921 or ASTM A388. EN 10204 3.1 or 3.2 certificates. One-piece minimum, no tooling charge.
1.6356 maraging steel contains up to 18.5% nickel, 12.0% cobalt, 4.8% molybdenum and 1.4% titanium, with carbon held to a maximum of 0.03%. Iron makes up the balance. Unlike conventional hardenable steels, 1.6356 gains its strength from intermetallic precipitates of Ni₃Ti and Fe₂Mo formed during ageing, not from carbon. That is why the carbon level is held so low.
| Element | Min | Max |
|---|---|---|
| Nickel (Ni) | — | 18.5 |
| Cobalt (Co) | — | 12.0 |
| Molybdenum (Mo) | — | 4.8 |
| Titanium (Ti) | — | 1.4 |
| Manganese (Mn) | — | 0.10 |
| Silicon (Si) | — | 0.10 |
| Aluminium (Al) | — | 0.10 |
| Carbon (C) | — | 0.03 |
| Zirconium (Zr) | — | 0.01 |
| Phosphorus (P) | — | 0.01 |
| Sulphur (S) | — | 0.01 |
| Boron (B) | — | 0.003 |
| Iron (Fe) | Balance | |
| Property | Value | Imperial |
|---|---|---|
| Tensile strength | 2345 MPa min | 340 ksi min |
| Yield strength (0.2%) | 2275 MPa min | 330 ksi min |
| Hardness | 56 HRC max | — |
| Elongation | 3 % min | 3 % min |
| Hardness, annealed | 30–35 HRC | — |
| Solution anneal | 815–830 °C, air cool | |
| Age hardening | 480 °C, 3–6 h, air cool | |
| Max service temp. | approx. 400 °C | |
Values as supplied by Jiangyin Jiangnan Metal · Verified · Confirm against the mill certificate for your order.
The three commercial 18% nickel maraging grades differ mainly in cobalt and titanium, which sets the strength ceiling. Maraging 250 reaches roughly 1725 MPa, Maraging 300 roughly 2000 MPa, and Maraging 350, the grade designated 1.6356, a minimum of 2345 MPa. Toughness and ductility fall as strength rises, so 1.6356 has the lowest elongation of the three at about 3% minimum. Specify 1.6356 when strength-to-weight is the governing requirement and the part will not be shock loaded.
| Grade | Werkstoff | Co % | Ti % | Mo % | Tensile | Elongation | Typical choice |
|---|---|---|---|---|---|---|---|
| Maraging 250 | 1.6359 | ≈8.0 | ≈0.4 | ≈5.0 | ≈1725 MPa | ≈8 % | Tooling, best toughness |
| Maraging 300 | 1.6358 | ≈9.0 | ≈0.7 | ≈5.0 | ≈2000 MPa | ≈6 % | Aerospace structure, balanced |
| Maraging 350 | 1.6356 | ≈12.0 | ≈1.4 | ≈4.8 | 2345 MPa min | 3 % min | Maximum strength-to-weight |
Jiangyin Jiangnan Metal supplies 1.6356 as open-die forged rings, shafts and spindles, flanges, discs and gear blanks, sleeves and bushings, tube sheets, round bars, blocks and forged tubes. All forms are made to customer drawings, with a minimum order quantity of one piece and no tooling charge.
Open-die forged and mandrel forged rings for bearing races, retaining rings and structural couplings.
Form Open-die · mandrel forged
Condition Annealed or aged
Straight, stepped and eccentric shafts for power transmission, gearboxes and high-load drive lines.
Form Round · stepped · flanged
Condition Annealed for machining
Flange blanks and tube sheets for pressure vessels, air receivers and shell-and-tube heat exchangers.
Form Blank · pre-machined
NDT UT to EN 10228-3
Solid and bored discs for gear wheels, couplings and highly stressed rotating components.
Form Solid · bored
Condition Annealed or aged
Hollow forgings bored on the press for compressor components, wear sleeves and bearing housings.
Form Bored hollow
Condition Annealed for machining
Round bars, rectangular blocks and forged tubes as stock for tooling, dies and machined components.
Form Round · square · hollow
MOQ 1 piece
1.6356 maraging steel is specified where the highest strength-to-weight ratio is required and the part must not distort during heat treatment. Typical uses are aerospace and defence structural components, rocket motor cases, landing gear parts, high-load shafting and couplings, die casting and extrusion tooling, and precision components in oil and gas equipment. Because ageing produces almost no dimensional change, parts can be finish machined before hardening.
1.6356 is not a high-temperature material. It is aged at around 480 °C, and sustained service above roughly 400 °C causes over-ageing and progressive loss of strength. For gas turbine hot sections and similar high-temperature duty, specify a nickel-base superalloy such as Inconel 617, Inconel 625 or Haynes 188 instead.
Rocket motor cases, missile bodies, landing gear components, structural fittings and load-bearing airframe parts.
High-torque shafts, spindles, couplings, gear blanks and flexible drive members where section size must stay small.
Die casting dies, extrusion tooling, punches and mandrels that benefit from near-zero distortion on ageing.
High-pressure valve components, wellhead parts and subsea fittings where strength governs the wall thickness.
Flanges, tube sheets and nozzles for pressure vessels, air receivers and shell-and-tube heat exchangers.
Eccentric shafts, forged rolls, crankshafts and highly stressed components in mills, presses and compressors.
Jiangyin Jiangnan Metal normally supplies 1.6356 forgings solution annealed at 815 to 830 °C and air cooled, which leaves the material at roughly 30 to 35 HRC and easily machinable. The customer finish machines the part and then ages it at approximately 480 °C for three to six hours, raising tensile strength above 2345 MPa with almost no dimensional change. Forgings can also be supplied already aged when no further machining is needed.
| Condition | Treatment | Hardness |
|---|---|---|
| As forged | No treatment | — |
| Solution annealed | 815–830 °C, air cool | 30–35 HRC |
| Annealed + rough machined | 815–830 °C, then turning / boring | 30–35 HRC |
| Solution annealed + aged | 480 °C, 3–6 h, air cool | up to 56 HRC |
| Test | Standard |
|---|---|
| Ultrasonic testing | EN 10228-3 · SEP 1921 · ASTM A388 |
| Chemical analysis | ASTM A751 |
| Tensile & yield | ASTM A370 · ISO 6892 |
| Hardness | ASTM E18 (HRC) |
| Magnetic particle | ASTM E709 |
| Dye penetrant | ASTM E165 |
| Material certificate | EN 10204 3.1 · 3.2 third party |
| Third-party inspection | SGS · BV · TUV · LR · DNV |
1.6356 is the German Werkstoff number for an 18% nickel maraging steel of the 350 grade, also written Maraging 350 or 18Ni(350). It is an iron-nickel martensitic steel that gains its strength from intermetallic precipitates of Ni₃Ti and Fe₂Mo formed during ageing, not from carbon. Carbon is held below 0.03%. In the fully aged condition 1.6356 reaches a minimum tensile strength of 2345 MPa and a hardness of up to 56 HRC, which makes it one of the strongest commercially available steels.
1.6356 is a steel, not a nickel-base alloy. Although it contains about 18% nickel, the matrix is iron and the material is classified as an iron-nickel martensitic precipitation-hardening steel, commonly grouped with maraging steels or ultra-high-strength steels rather than with nickel superalloys such as Inconel or Monel.
The three grades differ mainly in cobalt and titanium content, which sets the achievable strength. Maraging 250 (1.6359) contains about 8% cobalt and 0.4% titanium and reaches roughly 1725 MPa tensile. Maraging 300 (1.6358) contains about 9% cobalt and 0.7% titanium and reaches roughly 2000 MPa. Maraging 350 (1.6356) contains about 12% cobalt and 1.4% titanium and reaches a minimum of 2345 MPa. Toughness and ductility fall as strength rises, so 350 has the lowest elongation of the three at about 3% minimum.
No. 1.6356 is not a high-temperature material. It is aged at around 480 °C, and sustained service above roughly 400 °C causes over-ageing and progressive loss of strength. For gas turbine hot sections and other high-temperature service, a nickel-base superalloy such as Inconel 617, Inconel 625 or Haynes 188 should be specified instead. 1.6356 is chosen for ambient and moderate-temperature applications where the highest strength-to-weight ratio and dimensional stability during heat treatment are required.
Jiangyin Jiangnan Metal supplies 1.6356 as open-die forged rings, shafts and spindles, flanges, discs and gear blanks, sleeves and bushings, tube sheets, round bars, blocks and forged tubes. All items are made to customer drawings, with a minimum order quantity of one piece and no tooling charge.
1.6356 is normally supplied solution annealed at 815 to 830 °C and air cooled, which leaves it at about 30 to 35 HRC and easily machinable. The customer then finish machines the part and ages it at approximately 480 °C for three to six hours, which raises the strength to over 2345 MPa with almost no dimensional change. Jiangyin Jiangnan Metal can also supply the forging already aged when finish machining is not required.
Ultrasonic testing to EN 10228-3, SEP 1921 or ASTM A388 is available on 1.6356 forgings, together with chemical analysis, tensile and yield testing, hardness and dimensional inspection. Material certificates are issued to EN 10204 3.1, or to EN 10204 3.2 countersigned by SGS, BV, TUV, Lloyd's Register or DNV when specified on the purchase order.
Send the drawing or the required dimensions, the delivery condition and the quantity to sales@steelforgepieces.com, or call +86-189-2135-9659. Jiangyin Jiangnan Metal returns a price, forged weight and lead time, normally within 24 hours on working days. The plant is at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China.
Send a drawing in PDF, DWG, DXF, STEP or IGES, or simply the dimensions, the delivery condition and the quantity. Jiangyin Jiangnan Metal replies with price, forged weight and lead time, normally within 24 hours on working days.