Written by Jiangsu Liangyi Engineering Team · ISO 9001:2015 Certified Forging Manufacturer Since 1997
This guide is written by practicing metallurgical engineers who have produced 1.7735 (14CrMoV6-9) forgings for power generation, nuclear, and petrochemical clients in 50+ countries. All technical data is drawn directly from EN 10222-2 and in-house process documentation. For full size range, shapes, and ordering, see our 1.7735 (14CrMoV6-9) forging parts page.
01What Is 1.7735 Steel?
1.7735 is the European numeric material designation under EN 10027-2 for the chromium–molybdenum–vanadium alloy steel designated 14CrMoV6-9 by its chemical symbol name under EN 10027-1. These two names refer to exactly the same steel and are fully interchangeable on engineering drawings, purchase orders, and mill test reports.
It belongs to the family of heat-resistant, creep-resistant low-alloy steels standardized primarily under EN 10222-2 (steel forgings for pressure purposes), with additional coverage in EN 10083 for quenched-and-tempered structural use. The steel is designed to maintain mechanical strength, dimensional stability, and pressure integrity under sustained high temperature (up to 565°C), high pressure, and long-duration cyclic loading over the 20–40 year service lives typical of power plant equipment.
The three alloying additions — Chromium (oxidation resistance and hardenability), Molybdenum (creep resistance and temper embrittlement suppression), and Vanadium (grain boundary pinning via stable carbide precipitation) — together make 14CrMoV6-9 the optimum-cost solution for critical forgings in power generation, pressure vessel fabrication, and nuclear plant engineering operating in the 450–565°C temperature window.
1.7735 and 14CrMoV6-9 are the same steel. The numeric designation (1.7735) is used most often in purchase orders and mill certificates. The chemical symbol designation (14CrMoV6-9) is more common in engineering drawings and specification documents. Both formats are accepted under EN 10222-2.
02Decoding "14CrMoV6-9": What Each Part Means
The EN chemical symbol system (EN 10027-1) encodes alloy chemistry directly into the grade name. Understanding the convention allows any engineer to read the approximate composition from the label alone — no lookup table required.
Carbon × 100
≈ 0.14% C
Chromium
principal element
Molybdenum
creep resistance
Vanadium
grain refinement
Cr content × 4
≈ 1.5% Cr
Mo content × 10
≈ 0.90% Mo
The vanadium content (typically 0.25–0.35%) is not encoded in the trailing numbers — it is governed directly by the EN 10222-2 composition table rather than the grade label. The trailing figures apply only to the chromium and molybdenum contents, which are the two highest-concentration alloying elements.
03Chemical Composition of 1.7735 (14CrMoV6-9)
The composition limits below are the heat analysis (ladle analysis) requirements from EN 10222-2:2017+A1:2022. Product analysis (check analysis from the finished forging) is permitted to deviate by the tolerances specified in EN 10222-2 Annex A. All values are weight percent.
At Jiangsu Liangyi, 1.7735 steel is produced by Electric Arc Furnace (EAF) + Ladle Refining Furnace (LRF) + Vacuum Degassing (VD) to achieve composition uniformity, very low hydrogen (≤1.5 ppm), and clean steel practice essential for heavy-section forgings.
| Element | Symbol | Min (%) | Max (%) | Metallurgical Function |
|---|---|---|---|---|
| Carbon | C | 0.10 | 0.17 | Base strengthener; controlled low to preserve toughness and weldability |
| Silicon | Si | — | 0.35 | Deoxidation; moderate oxidation resistance contribution |
| Manganese | Mn | 0.40 | 0.70 | Hardenability support; sulphide morphology control |
| Phosphorus | P | — | 0.015 | Residual element; excess segregates to grain boundaries, promoting temper embrittlement |
| Sulphur | S | — | 0.010 | Residual element; excess forms MnS inclusions that reduce transverse impact toughness |
| Chromium | Cr | 1.20 | 1.70 | Hardenability; oxidation resistance; stable chromium carbide formation |
| Molybdenum | Mo | 0.70 | 1.10 | Creep resistance; solid-solution strengthener; counteracts phosphorus grain-boundary segregation |
| Vanadium | V | 0.25 | 0.35 | Stable VC and V₄C₃ precipitation; grain boundary pinning up to 550°C; elevated-temperature strength |
| Nickel | Ni | — | 0.40 | Residual; improves low-temperature toughness in moderate quantities |
| Aluminium | Al | — | 0.020 | Grain refinement aid; capped to avoid AlN-related embrittlement in thick sections |
The tight limit of P ≤ 0.015% combined with Mo ≥ 0.70% is a deliberate synergy, not coincidence. Phosphorus segregates to austenite grain boundaries during service and drastically lowers toughness — a phenomenon called temper embrittlement. Molybdenum slows phosphorus diffusion to boundaries, directly counteracting this mechanism. For a component that cannot be re-heat-treated during a 30-year service life, this synergy is the primary design feature that makes 14CrMoV6-9 safe in long-term elevated-temperature service.
04Mechanical Properties of 1.7735 Forgings
All properties below apply to the quenched-and-tempered (QT) condition per EN 10222-2. Minimum values are guaranteed by destructive coupon testing from the thermally least-favorable location of each forging — typically mid-thickness of the heaviest section — after all heat treatment is complete.
Elevated-Temperature Strength — Why Vanadium Makes the Difference
The key performance advantage of 14CrMoV6-9 over simpler grades like 13CrMo4-5 (1.7335) is its sustained strength at elevated temperature. Vanadium-rich carbide precipitates (VC and V₄C₃) remain stable and finely dispersed up to approximately 550°C, continuously impeding dislocation movement — a precipitation-hardening effect that 13CrMo4-5, which contains no vanadium, cannot replicate.
| Temperature | Yield Rp0.2 (MPa) | Tensile Rm (MPa) | Creep Rupture Stress at 10⁵ h (MPa) |
|---|---|---|---|
| 20°C (Room Temp) | ≥ 440 | ≥ 590 | — |
| 400°C | ~380 | ~520 | — |
| 450°C | ~360 | ~490 | ~230 |
| 500°C | ~330 | ~450 | ~145 |
| 540°C | ~290 | ~400 | ~85 |
| 565°C | ~240 | ~350 | ~45 |
Indicative values for QT forgings in the 150–300 mm ruling section range. Project-specific values are confirmed by test certificates issued with each order.
05Heat Treatment of 14CrMoV6-9 Forgings
Heat treatment for 1.7735 is not a finishing operation — it is a core manufacturing step that directly sets the final microstructure and all resulting mechanical properties. Every heat treatment furnace at our Jiangyin factory is computer-controlled with verified ±10°C temperature uniformity across the full load.
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1
Post-Forge Slow Cool / Immediate Stress Relief
Immediately after the final forging pass, parts are placed in insulated boxes or transferred directly to a furnace for controlled cooling to below 300°C. For sections exceeding 250 mm in minimum dimension, a subcritical stress-relief anneal at 650–700°C is performed before the part is allowed to cool below 300°C. This is mandatory — 14CrMoV6-9's high hardenability means even moderate air cooling can generate sufficient internal quench stress to initiate surface cracks in heavy sections.
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2
Soft Annealing (Prior to Rough Machining, When Required)
Heat to 780–840°C, hold for time proportional to section size, then furnace cool at a controlled rate of ≤20°C/hour to below 600°C, followed by air cooling. This produces a ferritic-pearlitic matrix with hardness ≤ 220 HB, allowing efficient heavy rough machining before final heat treatment. Not always required for parts that proceed directly to normalizing or hardening.
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3
Austenitizing / Hardening
Heat to 940–980°C, hold for a minimum of 1 hour per 25 mm of ruling section to achieve full austenitization and solution of alloying carbides. Quench in oil or water-polymer solution — quench medium selection depends on ruling section and hardenability calculation. Full martensitic transformation throughout the cross-section is the metallurgical target. Forgings produced at our facility with forging ratios ≥ 4:1 consistently achieve this in sections up to 600 mm.
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4
Primary Tempering
Temper at 680–750°C to transform the as-quenched martensitic structure to tempered martensite and re-precipitate the vanadium carbides in a fine, stable dispersion. Hold time is typically 2–3 hours per 25 mm of section, then air cool. Tempering temperature is the primary dial for setting the final strength class: higher temperatures produce lower strength but higher toughness. This step is recorded with full furnace chart documentation for the EN 10204 3.1 certificate.
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5
Post-Machining Stress Relief
After rough machining, a final stress relief at 620–650°C (always below the primary tempering temperature to prevent alteration of mechanical properties) removes machining-induced residual stresses and reduces the risk of distortion and cracking during subsequent precision machining and NDT. Standard practice for all complex-geometry and pressure-rated components.
For heavy sections or nuclear/power generation pressure components, we apply a double temper protocol: the part is fully tempered, cooled, ultrasonically inspected, and then re-tempered at 10–20°C below the first temper temperature. This ensures complete transformation of any retained austenite that re-formed during the first temper cycle, and measurably improves toughness consistency across thick cross-sections — a quality difference that matters over a 30-year service life.
06Applications of 1.7735 (14CrMoV6-9) Forgings
The application profile of 14CrMoV6-9 is defined by environments where high temperature (350–565°C) + high pressure + long service life (20–40 years) + zero tolerance for in-service failure all apply simultaneously. These combined requirements eliminate most common alloy steels.
Steam Turbine Rotor Discs & Shafts
IP and HP rotor discs in supercritical and ultra-supercritical power turbines at 540–565°C steam inlet. The material's resistance to stress relaxation — the gradual loss of interference fit stress under sustained temperature — is the defining selection criterion for disc-shaft assemblies designed to last 30+ years without re-machining.
Main Steam Valve Bodies
Stop valves, control valves, and bypass valves for high-pressure steam systems in power plants. The combination of creep strength and acceptable weldability makes 14CrMoV6-9 suitable for large valve bodies manufactured as open die forgings and then welded into main steam pipelines.
Nuclear Pressure Circuit Components
14CrMoV6-9 is specified for reactor pressure vessel internals, CRDM (control rod drive mechanism) housings, and high-pressure valve bodies in PWR and BWR reactor circuits in non-irradiated structural zones where elevated temperature and pressure cycling govern design. Nuclear projects require project-specific qualification — contact us to discuss your requirements.
Pressure Vessel & Heat Exchanger Components
Flanges, nozzles, tube sheets, and forged shell sections for high-pressure heat exchangers in refinery and petrochemical service above 350°C — the temperature range where carbon steel and 13CrMo4-5 reach their practical creep limit.
Supercritical Boiler Drum Components
Forged drum shells, header end caps, and nozzle blocks for supercritical boilers. EN 10222-2 directly lists 14CrMoV6-9 as a primary approved grade for pressure vessel forgings in boiler service — its most common and highest-volume application globally.
Defense & High-Performance Structural Housings
Armored vehicle transmission housings and structural casings where impact resistance combined with long-term structural stability at elevated operating temperatures are required — and where the high cost of P91 is not justified by the operating temperature.
071.7735 vs. Similar Grades: How to Choose
Engineers specifying a CrMoV forging grade typically face a short-list of three to five candidates. The table below positions 1.7735 against its closest alternatives across the properties that matter most at the point of selection:
| Criterion | 1.7335 13CrMo4-5 |
1.7735 14CrMoV6-9 |
1.7380 10CrMo9-10 |
1.4903 X10CrMoVNb9-1 (P91) |
|---|---|---|---|---|
| Max service temp | ~530°C | ~565°C | ~580°C | ~620°C |
| Creep strength at 500°C | Lower | Medium-High | Medium-High | Highest |
| Room-temp toughness | Excellent | Excellent | Good | Good |
| Weldability | Excellent | Good | Good | Strict PWHT |
| Forgeability (heavy section) | Easy | Easy | Moderate | Demanding |
| Vanadium carbide strengthening | No | Yes — key advantage | No | Yes + Nb (stronger) |
| Stress relaxation resistance | Lower | High | High | Very High |
| Temper embrittlement risk | Moderate | Low (Mo mitigates) | Moderate | Low |
| Primary governing standard | EN 10222-2 | EN 10222-2 | EN 10222-2 | EN 10302 |
| Relative material cost | Base | +15–25% | +20–30% | +60–90% |
Choose 1.7735 (14CrMoV6-9) when your operating temperature is in the 450–565°C range and you need significantly better creep performance than 13CrMo4-5 — but without the higher cost, stricter PWHT requirements, and more demanding forgeability of P91 (1.4903). It is the optimal balance grade for steam turbine discs, main steam valves, and pressure vessel nozzles in this temperature window. If your operating temperature exceeds 565°C continuously, evaluate 1.4903 (P91) forgings instead. To order or request a quote for custom 14CrMoV6-9 forgings, visit our product page.
08Manufacturing 1.7735 Open Die Forgings: Process Overview
Producing a 14CrMoV6-9 forging that meets EN 10222-2 for pressure-purpose service requires disciplined process control from melt to final inspection — not simply shaping hot steel. Here is the production sequence at our 80,000 m² Jiangyin facility.
Steel Melting & Secondary Metallurgy
Raw material starts with selected low-residual scrap, smelted in an Electric Arc Furnace (EAF), refined in a Ladle Refining Furnace (LRF) to achieve precise target composition, and then processed through Vacuum Degassing (VD) to reduce hydrogen below 1.5 ppm — non-negotiable for heavy forgings where retained hydrogen causes internal flaking. VD simultaneously reduces dissolved oxygen and nitrogen, improving steel cleanliness and impact toughness.
Ingot Casting & Homogenization
Steel is bottom-poured into ingot molds to minimize turbulence and inclusion entrapment. Ingots are then soaked at 1,200–1,250°C for 10–20 hours (scaled to ingot mass) to homogenize the as-cast dendritic segregation of Cr, Mo, and V — elements with relatively low solid-state diffusion coefficients that concentrate in interdendritic regions during primary solidification of large ingots.
Open Die Forging
Forging is carried out on our 6,300-ton hydraulic press through multiple upsetting-and-stretching passes to achieve a minimum forging ratio of 3:1 (typically 4:1 or higher for critical pressure parts). This ratio ensures complete breakdown of the cast dendritic structure, closure of residual micro-porosity, and development of the wrought grain flow that gives forgings decisively superior fatigue and fracture toughness compared to castings of the same composition.
Critical forging temperature management: upper temperature ≤1,200°C to prevent grain coarsening; finishing temperature ≥850°C to avoid forging into a partially transformed microstructure, which would produce non-uniform grain size and inconsistent mechanical properties.
Non-Destructive Testing (NDT)
All 1.7735 pressure forgings undergo ultrasonic testing (UT) per EN 10228-3. For nuclear and power generation components, magnetic particle inspection (MT) per EN 10228-1 is performed on accessible surfaces after rough machining and again after final heat treatment. Our in-house UT laboratory operates at 1–6 MHz frequency with both pulse-echo and TOFD (Time of Flight Diffraction) capabilities for reliable detection of planar and volumetric internal indications.
09International Grade Equivalents for 1.7735 / 14CrMoV6-9
There is no perfectly certified direct 1:1 equivalent in every national standard system. The table below gives the closest functional comparisons used by procurement teams working across multiple standards environments. Always verify composition limits and property requirements against both standards before substituting — grade-name similarity does not guarantee interchangeability.
| Standard System | Designation | Status | Notes |
|---|---|---|---|
| EN (European) | 1.7735 / 14CrMoV6-9 | Primary | Definitive designation; governs this guide |
| DIN (Germany, historical) | 14CrMoV6-9 / WNr 1.7735 | Identical | Legacy DIN; same composition, now harmonized under EN |
| BS (UK, historical) | No direct equivalent | None | Closest: 2½Cr-1Mo-V type forgings; verify independently |
| ASTM / ASME (USA) | No certified equivalent | None | Nearest: ASME Code Case 2098 (2.25Cr-1Mo-0.25V). Substitution requires code authority approval. |
| JIS (Japan) | SCMV6 (approx.) | Approximate | JIS composition limits differ; not a certified substitute without engineering review |
| GOST (Russia) | 15Х1М1Ф (approx.) | Approximate | Similar CrMoV concept; different composition and property limits |
| GB (China) | 12Cr1MoV (approx.) | Approximate | Widely used Chinese CrMoV grade; composition and heat treatment differ |
10Quality Certification for 1.7735 Forgings
Every 1.7735 forging from Jiangsu Liangyi is supplied with an EN 10204 Type 3.1 Mill Test Certificate (MTC) as standard. The 3.1 certificate is issued and signed by our qualified QA inspector and documents:
- Heat (melt) number and complete heat analysis
- Product analysis (check analysis from the forging body)
- Full mechanical test results at room temperature and elevated temperature (where required)
- Complete heat treatment record with furnace charts, temperatures, hold times, and quench method
- Ultrasonic testing results, scan coverage map, and acceptance class per EN 10228-3
- Dimensional inspection report with actual versus drawing comparison
- Statement of conformity to EN 10222-2 and any additional customer specification or project standard
For nuclear, offshore, or other safety-critical applications requiring independent verification, we can accommodate EN 10204 Type 3.2 certificates co-signed by a customer-nominated third-party inspection agency. Common agencies accepted by our customers include TÜV, DNV, Bureau Veritas, ABS, Lloyd's Register, SGS, and Intertek. Please specify your required inspection agency and hold points at the enquiry stage so we can confirm availability and scheduling.
11Our 1.7735 Forging Manufacturing Capabilities
Jiangsu Liangyi has produced 1.7735 (14CrMoV6-9) forgings for customers in power generation, nuclear energy, petrochemical, and defense industries across 50+ countries since 1997. Visit our 1.7735 forging parts product page formats, and quotation. Key manufacturing facts:
| Capability / Parameter | Our Specification |
|---|---|
| Factory established | 1997 — 29+ years specializing in CrMoV and alloy steel forgings |
| Factory area & location | 80,000 m² in Jiangyin City, Jiangsu Province, China (150 km from Shanghai Port) |
| Fixed assets | USD 40 million in forging, heat treatment & testing equipment |
| Annual production capacity | 120,000 tons across all grades |
| Max press capacity | 6,300-ton hydraulic press |
| Hammer capacity | 0.75-ton to 9-ton electro-hydraulic forging hammers |
| Ring rolling machine | 5-meter ring rolling machine — rings up to Φ5,000 mm OD |
| Single-piece weight range | 30 kg – 30,000 kg |
| Maximum bar length | Up to 12 meters |
| Heat treatment furnaces | 10+ computer-controlled furnaces, ±10°C uniformity, up to 1,250°C |
| Quality certification | ISO 9001:2015 certified |
| Standard MTC | EN 10204 3.1 with every order |
| 3rd-party inspection | Customer-nominated inspection agencies accepted — please specify at enquiry stage (common agencies: TÜV, DNV, BV, ABS, LR, SGS, Intertek) |
| Export experience | 50+ countries including Germany, Italy, South Korea, USA, India, Saudi Arabia, Australia |
| Standard lead time | 8–16 weeks (complex/large parts: 16–24 weeks) |
12Frequently Asked Questions About 1.7735 / 14CrMoV6-9
Yes — completely. 1.7735 is the EN 10027-2 numeric designation and 14CrMoV6-9 is the EN 10027-1 chemical symbol designation for exactly the same steel. Both appear in EN 10222-2 and are fully interchangeable on engineering drawings, purchase orders, and mill test certificates.
There is no certified direct ASTM equivalent. The closest comparison is ASME Code Case 2098 (2.25Cr-1Mo-0.25V) or ASTM A182 F22V with vanadium addition — neither is a certified substitute without engineering review and code authority approval. Contact our team for a project-specific cross-standard review.
The practical upper limit for continuous pressure service is approximately 565°C, per EN 10222-2 and published long-term creep data. Above this, vanadium carbide precipitates coarsen and the long-term creep rupture strength falls below design allowable values in EN 13480 and EN 12952. For service above 565°C, evaluate 1.4903 (P91).
The key difference is vanadium. 14CrMoV6-9 (1.7735) contains 0.25–0.35% V, forming stable carbides that deliver significantly better creep strength at 450–565°C. 13CrMo4-5 (1.7335) has no vanadium — better weldability and lower cost make it preferable below ~500°C continuous service. See our 1.7335 product page for details.
Yes, with a qualified WPS. Requirements: pre-heat 200–300°C for sections above 25 mm; low-hydrogen consumables with matching CrMoV composition; PWHT at 700–740°C for all pressure-retaining welds. We supply forgings with weld-procedure-qualification test coupon material on request.
We supply from 30 kg to 30,000 kg single piece weight: round bars up to 2,000 mm Ø and 12 m length; seamless rolled rings up to 5,000 mm OD; discs up to 2,400 mm OD; and custom open die shapes per drawings. Contact us for a capacity confirmation and quotation.
Standard: EN 10204 Type 3.1 Mill Test Certificate covering heat analysis, product analysis, full mechanical test results, heat treatment records with furnace charts, UT results, and EN 10222-2 conformity statement. EN 10204 Type 3.2 (co-signed by a customer-nominated third-party inspection agency) can be arranged for critical applications — please specify your required inspection body at enquiry stage.