Quick reference — 1.8550 / 34CrAlNi7-10 key facts
Among the nitriding steels defined in DIN EN 10085, grade 1.8550 — short name 34CrAlNi7-10 — is the workhorse for applications demanding an exceptionally hard, wear-resistant surface combined with a tough, fatigue-resistant core. It is the standard choice for nitrided gearbox shafts, extrusion screws, injection moulding barrels, crusher eccentric shafts, and high-cycle components across heavy industry worldwide.
This guide covers the alloy in full: what the designation means, what numbers you will see on a mill test certificate, how the gas nitriding process transforms the surface, and how to write a purchase specification that protects you from quality risk. Engineers who have completed the specification checklist in Section 10 can request custom 34CrAlNi7-10 forgings directly from Jiangsu Liangyi Co., Limited.
Material designation and naming convention
The full designation 1.8550 is the EN material number under the European standard DIN EN 10085 — Nitriding Steels: Technical Delivery Conditions. The short name 34CrAlNi7-10 is a direct read-out of the alloy architecture:
| Code element | Meaning | Engineering significance |
|---|---|---|
34 | ~0.34 % Carbon (×100) | Core hardenability and tensile strength after quench & temper |
Cr | Chromium present | Secondary nitride-former; contributes to case hardness |
Al | Aluminium present | Primary nitride-former — AlN precipitates drive hardness to 900–1100 HV |
Ni | Nickel present | Core toughness in large cross-sections; key differentiator vs. 38CrMoAl |
7 | Cr ×4 → ~1.75 % | EN multiplier for Cr content |
10 | Al ×10 → ~1.0 % | EN multiplier for Al content |
Naming variants
Also written as 34CrAlNi710, 34CrAlNi7.10, or simply 1.8550. All refer to the same grade. The EN number 1.8550 is unambiguous on international orders — always request both the short name and EN number in your mill test report (MTR).
Chemical composition per DIN EN 10085
The ranges below are the cast analysis limits in EN 10085 for grade 34CrAlNi7-10. Product analysis on finished forgings may carry slightly wider permitted deviations per the standard.
| Element | Symbol | Min % | Max % | Role in the alloy |
|---|---|---|---|---|
| Carbon | C | 0.30 | 0.37 | Core strength and hardenability |
| Silicon | Si | — | 0.40 | Deoxidation; minor solid-solution strengthening |
| Manganese | Mn | 0.40 | 0.70 | Hardenability; scavenger for sulfur |
| Phosphorus | P | — | 0.025 | Impurity — controlled to limit temper embrittlement |
| Sulfur | S | — | 0.035 | Impurity — low S essential for fatigue performance |
| Chromium | Cr | 1.50 | 1.80 | Secondary nitride-former; case hardness contribution |
| Aluminium | Al | 0.80 | 1.20 | Primary nitride-former — AlN precipitates drive extreme surface hardness |
| Nickel | Ni | 0.85 | 1.15 | Core toughness; critical for large cross-sections and shock-load applications |
The aluminium content (0.80–1.20 %) is the defining characteristic. Aluminium has the highest affinity for nitrogen of any common alloying element. During gas nitriding it precipitates as coherent AlN platelets, producing surface hardness values — typically 900–1050 HV — that no other standard engineering steel grade reliably achieves.
Mechanical properties — quenched & tempered core
Mechanical properties are measured in the quenched and tempered (Q+T) condition before nitriding. These core values are fully retained after gas nitriding, as nitriding temperatures (480–530 °C) lie well below the tempering temperature and do not alter the core microstructure.
| Property | Symbol | Value | Test condition |
|---|---|---|---|
| 0.2% Proof Strength | Rp0.2 | ≥ 750 MPa | Room temp., longitudinal |
| Tensile Strength | Rm | 900 – 1100 MPa | Room temp., longitudinal |
| Elongation (A5) | A | ≥ 10 % | Room temp., longitudinal |
| Reduction of Area | Z | ≥ 40 % | Room temp., longitudinal |
| Charpy Impact (KV) | KV | ≥ 35 J | Room temp., ISO-V notch |
| Core Hardness (Q+T) | HB | 270 – 320 HB | Pre-nitriding |
| Nitrided Surface Hardness | HV1 | 900 – 1050 HV1 | Post gas nitriding, 0.02 mm depth |
| Effective Case Depth | Nht | 0.3 – 0.6 mm typical | To HV550 limit (EN ISO 18203) |
"The aluminium in 34CrAlNi7-10 is not there for corrosion resistance — it is there because AlN precipitates are the hardest nitride phase achievable in a practical engineering steel, giving surface values that rival case-hardened tool steels while preserving a ductile, tough core."
— Jiangsu Liangyi Co., Limited | Metallurgy Engineering TeamThe gas nitriding process for 1.8550 steel
Gas nitriding is a thermochemical surface hardening process conducted in dissociated ammonia (NH₃) atmosphere at 480–530 °C. Because this lies well below the lower critical temperature (Ac₁), no phase transformation occurs in the core — dimensional stability and core toughness are fully preserved.
Why 1.8550 responds better than conventional steels
Conventional alloy steel (e.g., 42CrMo4)
- Nitrided surface hardness: 550–700 HV
- Limited by Cr-only nitride formation
- Compound layer forms readily; masking often needed
- Adequate case depth in moderate cycle times
- Lower white-layer risk with careful NH₃ control
1.8550 / 34CrAlNi7-10
- Surface hardness: 900–1050 HV
- Coherent AlN + CrN dual-phase precipitation
- Thinner, more controlled compound layer
- Max case depth ~0.7 mm (longer cycles needed)
- White layer must be ≤10 µm for fatigue-critical parts
Gas nitriding cycle parameters
| Parameter | Standard gas nitriding | Two-stage Floe process |
|---|---|---|
| Temperature | 500–520 °C | Stage 1: 510 °C / Stage 2: 525 °C |
| Duration | 40–80 hours | 20–30 h + 20–30 h |
| NH₃ dissociation — Stage 1 | 18–25 % | 18–22 % |
| NH₃ dissociation — Stage 2 | — | 60–80 % |
| Target case depth (Nht) | 0.3–0.5 mm | 0.4–0.6 mm |
| Compound layer (white layer) | 10–20 µm | ≤ 8–10 µm |
| Surface hardness | 900–1000 HV | 950–1050 HV |
White layer warning — fatigue-critical parts
The compound layer (white layer) at the extreme surface is hard but brittle. For rotating shafts, gear roots, and journal surfaces, a white layer exceeding 10 µm is a crack initiation risk. Always specify maximum white layer thickness on your engineering drawing. Require masking of keyways, bore entries, and stress concentrations to preserve local ductility.
Heat treatment sequence before nitriding
All 1.8550 forgings must be in quenched and tempered (Q+T) condition before nitriding. The tempering temperature must be set at least 50 °C above the intended nitriding temperature to ensure dimensional stability during the nitriding cycle.
01
Austenitize
Heat to 840–880 °C. Soak ≥1 min/mm of ruling section for full carbide dissolution and uniform austenite.
02
Quench
Oil or water-polymer quench by section size. Target: full martensitic transformation to the core.
03
Temper
580–660 °C, always ≥50 °C above nitriding temp. Target: 270–320 HB. This temperature locks in the core microstructure.
04
Stress Relief
For precision parts, a sub-critical stress relief at ~550 °C after rough machining minimises distortion during nitriding.
05
Semi-Finish Machine
Leave 0.05–0.10 mm nitriding allowance on toleranced surfaces. Nitriding growth is small but must be planned for.
06
Gas Nitriding
480–530 °C, controlled NH₃ atmosphere, 40–80 hours per required case depth. Mask areas requiring local ductility.
International equivalents and cross-references
Engineers specifying in non-European standards frequently need the closest equivalent for procurement, import classification, or design validation.
| Standard / Country | Designation | Reference | Key notes |
|---|---|---|---|
| Europe (EN) | 1.8550 / 34CrAlNi7-10 | DIN EN 10085 | Primary reference — use on all international drawings |
| UK (BS) | 905M39 | BS 970-3 | Closest UK equivalent; slightly different Al range |
| Germany (legacy) | 34CrAlNi7 | DIN 17211 (withdrawn) | Predecessor; still appears on older drawings |
| USA (AISI/SAE) | No direct equivalent | — | Specify by composition citing EN 10085 |
| Japan (JIS) | SACM645 (38CrMoAl) | JIS G4053 | Mo replaces Ni — lower toughness in large sections |
| China (GB) | 38CrMoAl | GB/T 3077 | No Ni; verify toughness for large or shock-loaded forgings |
| France (NF) | 35CrAlNi7 | NF A35-552 | Near-identical composition |
| Sweden (SS) | SS 2940 | SS-EN 10085 | EN harmonised; same as 1.8550 |
38CrMoAl substitution risk
38CrMoAl (JIS SACM645 / GB 38CrMoAl) substitutes Molybdenum for Nickel. Similar nitrided surface hardness is achieved, but Charpy impact values in sections above 100 mm are significantly lower. For fatigue-critical applications and large forgings, specify 34CrAlNi7-10 (1.8550) and require verified toughness test data before accepting any 38CrMoAl substitute.
Forging considerations for 1.8550
The aluminium content in 34CrAlNi7-10 introduces specific forging process considerations that an experienced manufacturer manages proactively.
Steel melting route — the most critical specification decision
| Route | Process | Inclusion cleanliness | Best application |
|---|---|---|---|
| Standard | EAF + LF + VD | Good | General industrial components, prototype validation |
| Premium | EAF + PESR | Very Good | Fatigue-critical rotating shafts, gear shafts, crusher shafts |
| Ultra-Premium | VIM + PESR | Excellent | Aerospace, nuclear, highest fatigue-cycle applications |
Minimum forging ratio
The forging reduction ratio determines how thoroughly the as-cast dendritic structure is refined. Standard: minimum ≥ 4:1; fatigue-critical: ≥ 5:1; high-severity applications (gyratory crusher shafts, large gear journals): ≥ 6:1. The Jiangsu Liangyi Australian iron ore crusher case study achieved 4+ years of service without fatigue failure at ≥ 6:1 reduction versus 12–16 months for the previous 42CrMo4 design.
Hot working temperature range
Start temperature: 1100 °C. Finish above: 850 °C. The aluminium content means the steel must not be worked below ~850 °C — sub-critical deformation introduces residual stress that persists through heat treatment.
Industrial applications
| Industry | Component | Why 1.8550? |
|---|---|---|
| Mining & Minerals | Gyratory crusher eccentric shafts, pinion shafts | Extreme surface hardness resists journal wear; tough core survives ore fragment impact |
| Plastics / Rubber | Extrusion screws, injection moulding barrels, plungers | Nitrided case resists abrasion from glass and mineral fillers; core maintains pressure integrity |
| Gearboxes | Nitrided gear shafts, pinion shafts, worm shafts | No distortion risk of carburizing; excellent pitting resistance on tooth and journal contact surfaces |
| Hydraulics | Cylinder piston rods, plunger pumps | Nitrided surface resists seal wear; superior dimensional stability vs. induction-hardened chrome bar |
| Power Generation | Turbine spindles, compressor shafts | High fatigue endurance limit; low distortion preserves bearing fit tolerances |
| Cement & Aggregates | Vertical mill spindles, rotary kiln trunnions | Continuous abrasive loading; nitrided case significantly extends replacement intervals |
| Oil & Gas | Mud pump piston rods, drilling wear sleeves | Abrasive slurry resistance; review NACE MR0175 compliance for sour service applications |
1.8550 vs. 31CrMoV9 (1.8519): which nitriding steel to choose?
The two most widely specified grades in EN 10085 are 34CrAlNi7-10 (1.8550) and 31CrMoV9 (1.8519). They are not interchangeable — they trade off peak surface hardness against machinability and post-nitriding distortion.
| Property | 1.8550 / 34CrAlNi7-10 | 1.8519 / 31CrMoV9 |
|---|---|---|
| Primary nitride-formers | Al + Cr (dual) | Cr + V (dual) |
| Peak surface hardness | 900–1050 HV | 650–750 HV |
| Nitriding distortion | Low | Very low |
| Machinability pre-nitriding | Moderate (Al impairs chip break) | Good |
| Core toughness — large section | Higher (Ni content) | Good (no Ni) |
| Typical effective case depth | 0.3–0.6 mm | 0.3–0.7 mm |
| Best fit | Maximum hardness, wear, shock resistance | Precision parts, tight post-nitriding tolerances |
Selection rule
Choose 1.8550 when maximum contact fatigue resistance and wear hardness are the priority. Choose 31CrMoV9 when minimising post-nitriding distortion on precision gear teeth or complex spline profiles is the overriding requirement.
Purchase specification framework for 1.8550 forgings
A poorly written purchase specification is one of the most common causes of quality disputes and field failures with nitriding steel forgings. The eight items below form a complete checklist — missing any single item leaves a quality gap.
- 1Material standard: State DIN EN 10085, grade 34CrAlNi7-10, EN material number 1.8550. Include both short name and EN number — together they are unambiguous on any international order.
- 2Steel melting route: State EAF+LF+VD, EAF+PESR, or VIM+PESR explicitly. The most commonly omitted item — and the most consequential for fatigue life. Omitting it allows substitution with the cheapest available route.
- 3Forging standard and minimum reduction ratio: Reference EN 10243-1 or ASTM A668. State minimum forging ratio: ≥ 4:1 general use, ≥ 5:1 fatigue-critical, ≥ 6:1 high-severity applications.
- 4Heat treatment condition: State "quenched and tempered (Q+T)" with target hardness range in HB (e.g., 280–320 HB) and minimum tempering temperature (must be ≥50 °C above intended nitriding temperature).
- 5Nitriding specification: Process type (gas / plasma), temperature range, target effective case depth Nht in mm to HV550 limit, minimum surface hardness in HV, and maximum white layer (compound layer) thickness in µm.
- 6Masking requirements: Identify on the drawing all surfaces, bores, keyways, and threaded features to be masked during nitriding to preserve local ductility at stress concentrations.
- 7NDT requirements: UT class per EN 10228-3 (Class 3 or 4 for fatigue-critical), MT and/or PT for surface. Reference the acceptance standard and reject criteria explicitly.
- 8Material test report (MTR): EN 10204 3.1 (manufacturer-issued test report) or 3.2 (third-party witness). For critical applications, name the acceptable inspection body: Bureau Veritas, SGS, Lloyd's Register, TÜV, RINA, or equivalent.
Ready to source 1.8550 forgings?
Once you have completed your purchase specification using the eight-point framework above, the next step is to request a quotation. The product page has full details on sizes, shapes, heat treatment options, and how to submit your drawing.
Frequently asked questions
What is 1.8550 steel (34CrAlNi7-10) and what standard governs it?
1.8550 is the EN material number for grade 34CrAlNi7-10 under DIN EN 10085 (Nitriding Steels — Technical Delivery Conditions). It is a chromium-aluminium-nickel nitriding alloy steel with 0.80–1.20% Al. After gas nitriding at 480–530 °C for 40–80 hours, the surface achieves 900–1050 HV1 while the quenched-and-tempered core retains 270–320 HB and ≥35 J Charpy impact energy.
What is the difference between 1.8550 and 38CrMoAl (SACM645)?
Both are aluminium-bearing nitriding steels achieving high surface hardness. The critical difference is Nickel: 34CrAlNi7-10 contains 0.85–1.15% Ni for superior core toughness in large cross-sections. 38CrMoAl (Chinese GB / JIS SACM645) substitutes Molybdenum for Nickel, yielding significantly lower Charpy impact values in sections above ~80 mm. For fatigue-critical large forgings subject to shock loads, 1.8550 is the safer, more reliable choice.
What surface hardness does gas nitriding achieve on 34CrAlNi7-10?
Gas nitriding of 34CrAlNi7-10 at 480–530 °C achieves 900–1050 HV1 — significantly higher than 42CrMo4 (550–700 HV) under identical conditions, due to coherent AlN + CrN dual-phase precipitation. Using the two-stage Floe process, 950–1050 HV with a white layer of ≤10 µm is achievable. Effective case depth (Nht) to the HV550 limit is typically 0.3–0.6 mm.
Does gas nitriding cause significant distortion of 1.8550 components?
Distortion is very low at 480–530 °C — one of the key advantages of nitriding over carburizing. Typical dimensional changes are 0.01–0.05 mm on diameters from volumetric expansion of the nitrided case. Leave a 0.05–0.10 mm nitriding allowance on toleranced surfaces, with final grinding after nitriding if required. A pre-nitriding stress relief at ~550 °C after rough machining further minimises distortion.
Can 1.8550 be plasma nitrided instead of gas nitrided?
Yes. Plasma (ion) nitriding is fully compatible with 34CrAlNi7-10 and offers advantages: lower process temperature (~420 °C), finer compound layer control, and more uniform treatment of complex geometries such as deep bores or blind keyways. Resulting surface hardness is comparable to gas nitriding. For large industrial shafts, gas nitriding is more economical; for precision gears with complex root profiles, plasma nitriding is often preferred.
What is the minimum order quantity and lead time for 1.8550 forgings?
MOQ and lead time vary depending on the steel melting route chosen (EAF+LF+VD, EAF+PESR, or VIM+PESR), the forging complexity, heat treatment condition, and whether gas nitriding is included. Single-piece prototype orders are supported. For current MOQ, lead time, and pricing information, contact Jiangsu Liangyi directly for current MOQ, lead time, and pricing — details are available on request.
Is 1.8550 suitable for H₂S sour gas service?
Standard Q+T 34CrAlNi7-10 forgings are generally not sour-service compliant. Core hardness of 270–320 HB typically exceeds the NACE MR0175 / ISO 15156 maximum of 22 HRC (~248 HB) for carbon and low-alloy steels in H₂S environments. For sour service, either select a compliant grade tempered to ≤248 HB, a stainless steel, or a nickel alloy, or obtain project-specific qualification data for the actual H₂S partial pressure and stress level in the intended application.
Conclusion
Grade 1.8550 / 34CrAlNi7-10 occupies a well-defined and irreplaceable position in the engineering steel landscape. When an application demands the highest achievable surface hardness from a nitriding process — combined with a truly tough, fatigue-resistant core capable of surviving shock loads and large cross-sections — this is the steel DIN EN 10085 specifies.
Its aluminium content is what sets it apart. The AlN precipitation mechanism during gas nitriding is simply more powerful than the Cr-only or Cr+V mechanisms of competing grades. The trade-offs — slightly more demanding machinability, careful white-layer management, and the need to specify a competent melting route — are readily managed by an experienced, ISO 9001:2015 certified forging manufacturer.
For procurement and engineering teams sourcing 34CrAlNi7-10 forgings internationally: treat the purchase specification as your primary quality control document. Specify the melting route. Specify the minimum forging ratio. Specify the nitriding parameters and the white layer limit. Require EN 10204 3.1 or 3.2 material test reports. These requirements are the technical barriers between a reliable component and a costly field failure.
Engineers who have applied the specification framework in Section 10 to a specific application are ready to move to procurement. Jiangsu Liangyi Co., Limited manufactures 34CrAlNi7-10 forging parts to customer drawings, with full traceability from steel melt to finished component.