The Steel Built for Large, High-Load Carburized Components
(defining feature)
1.6657 excels
(2008 edition)
after carburizing
KV₂ at room temp
offshore/cold duty
If you have spent time specifying case-hardening steels for heavy transmission components — particularly those exceeding 60 mm in section diameter — you have almost certainly encountered a performance ceiling with common grades like 16MnCr5 or 20MnCr5. These steels work well for smaller sections, but their hardenability falls short when the core of a large-diameter shaft or ring gear needs the toughness required for cyclic heavy loads.
1.6657 (14NiCrMo13-4) was engineered specifically to solve this problem. Its high nickel content and carefully balanced Cr-Mo additions provide hardenability for large sections, outstanding core toughness, and low ductile-to-brittle transition temperatures that lower-alloy grades cannot match at equivalent section sizes.
This guide is written by the metallurgical engineering team at 1.6657 forging parts, an ISO 9001:2015 certified open-die forging manufacturer established in 1997, with over 26 years of production experience in EN 10084 case-hardening steels and an annual capacity of 120,000 metric tons. Our goal is a single authoritative resource that explains not just what 1.6657 is, but why it behaves the way it does and when it is — and is not — the right choice.
1.6657 is the EN material number for the steel grade designated 14NiCrMo13-4, standardized under EN 10084:2008 (Case hardening steels — Technical delivery conditions). Also written as 14NiCrMo13.4, 14NiCrMo134, or 14NiCrMo13. It is a low-alloy, high-nickel carburizing steel designed for components requiring a hard, wear-resistant carburized surface layer over a tough, fracture-resistant core — simultaneously, in the same finished part, at section sizes above 60 mm where lower-hardenability grades are inadequate.
Reading the Name: What "14NiCrMo13-4" Encodes
EN steel designation names follow EN 10027-1 systematic rules. Every element in 14NiCrMo13-4 carries specific quantitative meaning:
// EN 10027-1 designation decoding — 14NiCrMo13-4 14 → Nominal carbon content × 100 → C ≈ 0.14 % Ni → Principal alloying element (1st) → Nickel Cr → Principal alloying element (2nd) → Chromium Mo → Principal alloying element (3rd) → Molybdenum 13 → Ni content × 4 = 13 → Ni ≈ 3.25 % (factor 4 for Ni) 4 → Mo content × 10 = 4 → Mo ≈ 0.30 % (factor 10 for Mo) // Cr is listed but unsuffixed — its range (0.8–1.1%) // is implicit in the alloy family position. // EN material number 1.6657 takes precedence in contracts.
This naming logic matters for cross-standard sourcing. All of the following names refer to the same material: 1.6657 · 14NiCrMo13-4 · 14NiCrMo13.4 · 14NiCrMo134 · 14NiCrMo13. The EN material number 1.6657 is the definitive identifier and takes precedence in contract and certification documentation.
Chemical Composition per EN 10084:2008
The standard sets maximum and minimum limits per heat. At Jiangsu Liangyi, our internal control limits are tighter than required — particularly for P, S, and the Ni/Cr ratio — because batch-to-batch consistency in large-volume forging programs demands tighter in-process control than the published standard provides.
| Element | Min % | Max % | Metallurgical Function |
|---|---|---|---|
| C · Carbon | 0.11 | 0.17 | Core strength; low C allows carbon gradient during carburizing |
| Si · Silicon | 0.10 | 0.40 | Deoxidation; minor solid-solution strengthening |
| Mn · Manganese | 0.40 | 0.70 | Hardenability improvement; deoxidation |
| Cr · Chromium | 0.80 | 1.10 | Case hardenability; wear resistance; moderate carbide formation |
| Ni · Nickel | 3.00 | 3.50 | Core toughness; large-section hardenability; DBTT reduction |
| Mo · Molybdenum | 0.20 | 0.30 | Hardenability; temper brittleness resistance; creep resistance |
| P · Phosphorus | — | 0.025 max | Impurity — embrittles grain boundaries; minimize |
| S · Sulfur | — | 0.015 max | Impurity — reduces impact toughness; minimize |
When reviewing mill test certificates (MTCs) for 1.6657, verify that both P and S are reported as actual measured values — not listed as "≤ limit" or "conforms." A supplier who cannot provide measured values for P and S per heat is not delivering the traceability required for safety-critical gear forgings. Always request EN 10204 3.1 or 3.2 mill test certificates (MTC) — never accept 2.2 declaration of compliance alone.
Why 3.0–3.5% Nickel Is the Defining Feature of 1.6657
Many engineers look first at carbon or chromium when comparing case-hardening steels. For 1.6657, neither is the critical differentiator. The 3.0–3.5% nickel content is. Here is the metallurgical logic:
1. Hardenability for Large Sections
Hardenability — the ability to through-harden across a large cross-section during quenching — is primarily determined by alloy content. Nickel, chromium, and molybdenum all contribute, but nickel is the dominant factor in 1.6657. Jominy end-quench data shows maintained hardness at J25 (25 mm from quenched end) that lower-Ni grades like 17CrNiMo6 (1.6587) cannot match at equivalent diameters. For forgings with section thickness above 60 mm — and especially those exceeding 150–300 mm — this hardenability directly determines achieved core hardness and mechanical properties after heat treatment.
2. Core Toughness
Nickel strengthens the ferritic matrix while simultaneously improving toughness — a rare combination in alloy design. In a carburized-and-hardened component, the core must absorb bending and impact loads without brittle fracture initiation. 1.6657's high-Ni core achieves Charpy impact values (KV₂ at room temperature) significantly higher than equivalent-strength low-Ni grades, making it especially suited to applications with high cyclic bending loads at the tooth root of large gears.
3. Ductile-to-Brittle Transition Temperature (DBTT)
Nickel is one of the very few alloying additions that simultaneously raises strength and lowers the DBTT. This means the steel retains ductile fracture behavior at lower temperatures. For wind turbine gearboxes operating at nacelle temperatures that can drop below −20 °C in northern European and offshore environments, this is a core design requirement — not a marginal benefit. 1.6657's DBTT is typically 20–30 °C lower than that of 18CrNiMo7-6 at comparable hardness levels.
4. Moderate Chromium — Lower Carbide Network Risk
The moderate Cr content of 1.6657 (0.8–1.1%) reduces the risk of continuous grain-boundary carbide formation during carburizing compared to higher-Cr grades like 18CrNiMo7-6 (1.50–1.80% Cr). This translates into more robust process tolerance during gas carburizing — particularly important when carbon potential control is less than perfect.
1.6657 vs. Competing Case-Hardening Steel Grades
Specifying 1.6657 over other grades should be a deliberate engineering decision, not a default. Below is a direct comparison with the four grades most commonly specified for similar applications:
- Highest Ni: 3.0–3.5%
- Best large-section hardenability
- Best low-temp core toughness
- Lowest carbide network risk
- Sections >60 mm — essential
- Premium material cost
- Ni: 1.40–1.70%
- Medium section (30–80 mm)
- Lower cost; EU stock available
- Lower core toughness
- Common automotive/industrial
- Ni: 1.40–1.70%
- Higher Cr: 1.50–1.80%
- Higher carbide network risk
- Good wind gearbox grade
- Less tough core vs 1.6657
- Ni: 0.40–0.70% (very low)
- Light-duty applications only
- Not suitable >40 mm
- Automotive transmission parts
- Lowest cost of group
| Property | 1.6657 | 18CrNiMo7-6 | 17CrNiMo6 |
|---|---|---|---|
| Ni content | 3.0–3.5% | 1.40–1.70% | 1.40–1.70% |
| Cr content | 0.80–1.10% | 1.50–1.80% | 1.50–1.80% |
| Large-section hardenability | Excellent | Good | Moderate |
| Core KV₂ (room temp) | ≥ 78 J | ~55–65 J | ~50–60 J |
| DBTT | Lowest (−30 to −50 °C) | ~−10 to −30 °C | ~0 to −20 °C |
| Carbide network risk | Low | Moderate–High | Moderate |
| Recommended max section | > 300 mm | ~200 mm | ~100 mm |
| Relative material cost | Highest | Medium | Medium–Low |
If your forged component has section diameter above 100 mm, requires core KV₂ > 60 J, and must maintain ductile behaviour at or below −20 °C, the technical case for 1.6657 over 17CrNiMo6 or 18CrNiMo7-6 is compelling. Below 60 mm section, 17CrNiMo6 will typically achieve equivalent case/core hardness at meaningfully lower material cost. The switch point is not fixed — involve a metallurgist when section size falls between 60–100 mm.
Carburizing 14NiCrMo13-4: Step-by-Step Process Guide
Carburizing is the diffusion-based thermochemical process by which carbon is introduced into the steel surface, raising the surface carbon content from the base 0.11–0.17% to a target of 0.75–0.90% (or higher, application-dependent). This enriched surface layer develops very high hardness upon quenching while the underlying low-carbon core remains comparatively soft and tough.
Austenizing — Pre-Carburize Heating (880–980 °C)
Parts are heated uniformly to 880–980 °C in a controlled atmosphere furnace. The high nickel content of 1.6657 raises the A₃ temperature slightly compared to lower-Ni grades, so furnace setpoints must account for this. Uniform heating across large sections is critical to prevent thermal gradient stresses, particularly for forgings exceeding 200 mm in cross-section.
Gas Carburizing with Carbon Potential Control (Cp 0.80–0.95%)
The furnace atmosphere — endothermic gas enriched with propane or methane — is maintained at a carbon potential (Cp) of 0.80–0.95% using oxygen probe or dew-point control. For 1.6657, the moderate chromium content (0.8–1.1%) means grain-boundary carbide network formation risk is lower than in higher-Cr grades, providing greater process tolerance and making 1.6657 a more forgiving steel to carburize at the production level.
Diffusion Stage (Cp reduced to 0.75–0.80%)
After the enrichment stage, carbon potential is reduced to 0.75–0.80% and the part is held to allow the carbon gradient to diffuse inward, creating a smooth hardness transition from surface to core. This stage defines the effective case depth profile and prevents a sharp, brittle interface. Skipping or shortening the diffusion stage is one of the most common causes of fatigue failures in carburized gears.
Direct Quench or Re-Heat Quench (790–850 °C → oil/polymer quench)
Parts may be quenched directly from carburizing temperature (direct quench) or cooled, re-heated to 790–850 °C, then quenched in oil or polymer media. 1.6657's high hardenability means oil quench is normally sufficient for sections up to 200 mm+, avoiding the dimensional distortion risks associated with water or brine quenching.
Low-Temperature Tempering (150–200 °C)
A final temper at 150–200 °C relieves quench stresses and reduces retained austenite without significantly reducing surface hardness. This stage is critical for dimensional stability and must never be omitted — especially for precision gear forgings with close-tolerance bores or OD profiles where residual stress can cause post-machining distortion.
Recommended CHD vs. Module and Section Size
Case-hardening depth (CHD) is defined per ISO 2639 as the distance from the surface to the point where hardness equals 550 HV. The table below gives starting-point guidelines based on Jiangsu Liangyi production experience and ISO 6336-5 methodology. CHD must always be confirmed on the engineering drawing.
| Gear Module or Section | Recommended CHD | Typical Application |
|---|---|---|
| Module 4–6 | 0.5–0.8 mm | Light industrial gearboxes, accessory drives |
| Module 6–10 | 0.8–1.4 mm | Medium industrial gearboxes, mill drives |
| Module 10–16 | 1.4–2.2 mm | Heavy industrial, offshore gearbox pinion shafts |
| Module 16–25 | 2.2–3.5 mm | Wind turbine main gearbox stages |
| Section > 300 mm | 3.0–5.0+ mm | Large forge rolls, mining drive shafts |
Hardness Gradient: Surface to Core
A properly processed 1.6657 forging exhibits a characteristic hardness gradient measurable by HV10 microhardness traverse on a metallographic cross-section. The gradient profile from surface to core looks like this:
The transition slope (hardness gradient) is controlled via diffusion stage duration during carburizing. A steeper gradient increases surface compressive residual stress, improving tooth root bending fatigue life. For safety-critical applications (wind turbine main stages, offshore drives), residual stress measurement by X-ray diffraction is recommended.
Mechanical Properties After Carburizing and Hardening
| Property | Test Location | Required Value | Standard / Reference |
|---|---|---|---|
| Yield Strength Rp0.2 | Core, ¼ radius | ≥ 835 MPa | EN 10084:2008, Table 7 |
| Tensile Strength Rm | Core | 1030–1280 MPa | EN 10084:2008 |
| Elongation A₅ | Core | ≥ 11 % | EN 10084:2008 |
| Reduction of Area Z | Core | ≥ 50 % | EN 10084:2008 |
| Impact Energy KV₂ | Core, room temp | ≥ 78 J (longitudinal) | EN 10084:2008 |
| Surface Hardness | Carburized surface | 58–62 HRC | ISO 2639 |
| Core Hardness | Centre after Q+T | 30–40 HRC | Engineering drawing |
| Bending Fatigue σbW | Case (tooth root) | ~600–700 MPa | ISO 6336-5 MQ grade |
All mechanical property values above are for a 16 mm reference test piece machined from the forging core per EN 10084:2008. For actual large forgings (section > 100 mm), properties must be verified on integral prolongations cut from the actual forging — not from a separately forged test bar, which does not represent the through-section thermal history of the production piece. Insist on this in your purchase specification. Complement with EN 10228-3 UT results (Class 3 minimum for gear applications).
Forging 1.6657: Temperature, Ratio, and Microstructure Control
Working Temperature Range: 1050–1200 °C
The recommended open-die forging temperature window for 14NiCrMo13-4 is 1050–1200 °C. Forging must not continue below 900 °C to avoid working in the two-phase (α+γ) region, which causes microstructural banding and unacceptable property anisotropy in large forgings. Start temperature is capped at 1220 °C to prevent incipient melting at nickel-rich grain boundary segregations — a specific risk in high-Ni steels if the billet is oversoaked at maximum temperature.
Minimum 3:1 Forging Reduction Ratio
A minimum 3:1 forging reduction ratio (cross-sectional area of ingot to finished forging) is mandatory for 1.6657 to close ingot porosity, refine the as-cast grain structure, and develop the full mechanical property potential — especially transverse Charpy impact values. Forgings produced with less than 3:1 reduction will not achieve EN 10084 core toughness requirements regardless of heat treatment.
Post-Forge Cooling and Hydrogen Degassing
After forging, 1.6657 billets are slow-cooled in covered sandboxes or isothermal annealing furnaces to prevent hydrogen flaking — a specific risk in high-nickel steels. All production lots undergo vacuum degassing (VD) in the EAF + LF + VD triple-melt process, and post-forge cooling rates are documented and controlled with thermocouple verification.
Where 1.6657 (14NiCrMo13-4) Is Used
The following industries represent the primary demand drivers for 1.6657 forgings globally. The common thread: large section size + high cyclic load + requirement for both surface hardness and core toughness simultaneously.
Wind Turbine Gearboxes
Main stage ring gears, planet carriers, pinion shafts. Offshore duty demands low-temperature core toughness below −20 °C.
Large Industrial Gear Drives
Mill pinions, crusher drives, kiln drive rings — sections frequently exceed 200 mm, where 1.6657 is decisive over 17CrNiMo6.
Marine Propulsion Systems
Gearbox shafts and ring gears for ship propulsion. High Ni content provides strength and corrosion tolerance in marine environments.
Offshore Drive Systems
Drill rig top-drive gearbox internals and subsea power-transmission components at seawater ambient temperatures.
Construction Equipment
Slewing ring gears and travel drive gears in heavy excavators and cranes requiring high tooth root bending fatigue resistance.
Steel Mill Roll Journals
Backup roll journals and intermediate roll bodies in rolling mills, where surface wear resistance and core toughness must coexist.
How to Procure 1.6657 Forgings: Engineering Buyer Checklist
Sourcing 1.6657 forgings requires rigorous documentation to ensure the material actually meets the standard. The following checklist represents minimum requirements for competent procurement of custom 1.6657 (14NiCrMo13-4) forged components:
| Requirement | Why It Matters | What to Specify in PO |
|---|---|---|
| Melt traceability | Confirms controlled melt (EAF + LF + VD, not scrap-only) | Melt record; heat number traceable to MTC |
| Chemistry certification | Verifies actual composition meets EN 10084 per heat | EN 10204 3.1 mill test certificate with actual measured values |
| Mechanical test results | Ensures heat treatment achieved EN 10084 Table 7 values | Tensile + Charpy per EN 10084, from integral prolongation |
| Ultrasonic testing | Detects internal flaws, inclusions, hydrogen flakes | EN 10228-3 Class 3 or 4 |
| Forging ratio record | Confirms ≥ 3:1 reduction — mandatory for EN 10084 properties | Forging process record: ingot and finished cross-sections |
| CHD verification | Validates carburizing achieved drawing-specified case depth | Hardness traverse report per ISO 2639 |
| Dimensional report | Confirms machining tolerance compliance | CMM report per ISO 8062 tolerance class |
Custom 1.6657 forgings including forging, carburizing heat treatment, rough machining, and inspection typically require 10–18 weeks from order confirmation to shipment. Orders including finish machining or complex profiles should allow 20–26 weeks. Lead-time claims below 8 weeks for fully certified custom forgings should be questioned carefully.
Frequently Asked Questions About 1.6657 Steel
1.6657 is the EN material number for 14NiCrMo13-4, a low-alloy case-hardening steel per EN 10084:2008. It is used for large-section forgings above 60–100 mm that require a hard carburized surface (58–62 HRC) over a tough core (30–40 HRC). Primary applications: wind turbine gearboxes, large industrial gear drives, marine propulsion gearboxes, offshore drive systems, and heavy construction equipment slewing rings.
Not exactly. SAE 9315 is the closest American equivalent but differs in chromium range (1.00–1.40% vs 0.80–1.10%) and critically in molybdenum content (0.08–0.15% vs 0.20–0.30%). The higher Mo in 1.6657 confers better temper-brittleness resistance. SAE 9315 may be acceptable as a documented substitution after engineering approval — but it is not a direct drop-in equivalent under EN 10084.
CHD (case-hardening depth per ISO 2639) is the distance from the surface to the 550 HV point — the engineering specification parameter placed on the drawing. Total case depth (TCD) extends to where the microstructure transitions to fully ferritic-pearlitic core structure, typically 1.2–1.8× CHD. TCD is used in process development; CHD is what your drawing specifies and what the inspector measures.
Welding is technically feasible but not recommended for carburized 1.6657 components. The high carbon equivalent (CE ≈ 0.8+) makes weld heat-affected zones prone to cold cracking. For un-carburized blanks in normalized-and-tempered condition, welding is possible with 200–300 °C pre-heat and post-weld heat treatment under a qualified procedure. However, 1.6657 is fundamentally a forging steel, not a structural weldment material.
For sections above approximately 80 mm diameter, the mechanical property difference is significant. Open-die forging closes ingot porosity, creates a fine and uniform grain structure across the full cross-section, and aligns inclusion morphology favorably. Rolled bar at large diameters cannot achieve the same internal homogeneity or transverse impact properties. For large-section 1.6657 gear forgings, forged product is technically necessary — not merely preferred.
The recommended carburizing temperature for 14NiCrMo13-4 (1.6657) is 880–980 °C. The higher end (940–980 °C) accelerates carbon diffusion and reduces cycle time but requires more precise atmosphere control. For production forgings with complex cross-sections, 920–940 °C with a controlled diffusion stage provides the best balance of throughput, case depth consistency, and low distortion risk.
Need 1.6657 (14NiCrMo13-4) Forging Parts?
Jiangsu Liangyi Co., Limited — ISO 9001:2015 certified open-die forging manufacturer since 1997. Custom forgings and seamless rolled rings from 30 kg to 30,000 kg, EN 10204 3.1/3.2 mill test certificates available on request, shipped to 50+ countries.
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