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1.4922 (X20CrMoV11-1) Forging Parts | China Leading Manufacturer & Supplier

⚡ Quick Reference — 1.4922 / X20CrMoV11-1
Material Grade1.4922 / X20CrMoV11-1 (EN 10302)
Max Continuous Temp.600°C / 650°C (short-term)
Creep Rupture (600°C, 100kh)≥ 75 MPa
Tensile Strength (QT)700–850 MPa
Yield Strength (QT)≥ 500 MPa
Density7.72 g/cm³
Max Single Piece Weight30 tons
Max Ring Diameter6,000 mm
Max Shaft Length15,000 mm
StandardsEN 10302 / EN 10222-2 / ASTM
CertificationISO 9001:2015 · EN 10204 3.1/3.2
Lead Time30–60 days (custom)
High-quality 1.4922 X20CrMoV11-1 open die forging parts produced by Jiangsu Liangyi, China professional forging manufacturer

1.4922 (X20CrMoV11-1) Martensitic Creep Resisting Steel — Material Overview

Jiangsu Liangyi is a professional ISO 9001:2015 certified China manufacturer and supplier of 1.4922 (X20CrMoV11-1, X20CrMoV12-1, X20CrMoNiV11-1-1) open die forging parts, with over 25 years of experience in custom forged steel solutions for global clients from more than 50 countries. Located in Jiangyin City, Jiangsu Province — China's core forging industry cluster — we provide end-to-end solutions from steel melting, forging, heat treatment to precision CNC machining, fully compliant with EN, ASTM, and DIN international standards.

1.4922 (X20CrMoV11-1) is a premium heat-treated martensitic creep resisting steel, governed primarily by EN 10302:2008. Its defining characteristic is a carefully balanced alloying system: approximately 11% chromium provides robust oxidation and corrosion resistance; molybdenum (0.5–0.8%) and vanadium (0.1–0.3%) precipitate fine carbides that act as barriers to dislocation movement at elevated temperatures; and a controlled carbon content of 0.17–0.23% delivers the martensitic matrix strength required for long-term load-bearing at up to 600°C. The result is a steel that maintains dimensional stability and load-bearing integrity across tens of thousands of operating hours — a critical requirement that simpler ferritic or austenitic grades cannot simultaneously satisfy at this temperature range.

Our 1.4922 forging parts are widely used in power plant engineering, high-temperature pipeline systems, steam boiler and turbine construction, chemical industry reactors, oil & gas processing equipment, and pressure vessel applications across Asia, Europe, the Middle East, and North America.

Full Range of Custom 1.4922 (X20CrMoV11-1) Forged Steel Products

We manufacture a complete line of custom 1.4922 (X20CrMoV11-1) forging parts in strict accordance with international standards and client drawings, with single-piece weight capacity from 30 kg to 30 tons. Our available product range covers all core industrial applications:

Forged Bars & Rods

X20CrMoV11-1 forged steel round bars, square bars, flat bars, rectangular bars, and precision rods for turbine blade, valve component and structural applications. Max forging diameter up to 2,000 mm, with full EN 10204 3.1/3.2 certification available. Explore our full range of forged steel bars

Seamless Rolled Forged Rings

X20CrMoV11-1 seamless rolled forged rings, guide rings, seal rings, labyrinth rings, packing seal rings, diaphragm seal rings, rotor end rings, and custom contoured casing rings. Ring rolling capacity up to 6,000 mm in outer diameter, ideal for turbine casing, valve body and high-pressure flange applications. Discover our seamless rolled forged rings

Power Generation & Turbine Forged Components

1.4922 forged gas and steam turbine rotor shafts, turbine blades, turbine vane steel flat bars, X20CrMoV12-1 turbine valve spindles/stems/rods, and gas compressor components. Max shaft length up to 15,000 mm, max diameter up to 2,000 mm, with high-speed dynamic balancing and 100% UT inspection available. Learn more about our turbine forging components

Valve & High-Strength Fastener Forgings

X20CrMoV11-1 forged valve seats, valve bodies, valve bonnets, double-ended studs, bolts, nuts and other high-strength fasteners for high-temperature and high-pressure valve systems. Fully compatible with API 6A and ASME standards, with optional Stellite hardfacing available per client requirements. View our valve forging solutions

Hollow Forgings & Pressure Vessel Components

1.4922 forged hubs, housings, shells, sleeves, bushes, hollow bars, heavy-wall cylinders, discs, blocks, plates, seamless pipes, tubes, and pressure vessel casings. Max outer diameter of hollow forgings up to 3,000 mm, suitable for high-temperature pipeline and reactor applications. Check out our hollow forging products

1.4922 (X20CrMoV11-1) Forging Dimensions & Available Size Ranges

The table below summarizes the standard available size ranges for each product category. All dimensions are based on our current forging and machining equipment capability. If you need sizes that are bigger or smaller than these or shapes that aren't standard, please get in touch with our technical team to see if we can help. We often deliver custom solutions for big power and petrochemical projects that are outside of these limits.

Round Bars & Solid Rods

  • Diameter: Ø50 – Ø2,000 mm
  • Length: up to 6,000 mm
  • Min. weight: ~15 kg
  • Max. weight: ~30,000 kg
  • Tolerances: h9 to h11 (rough); ±0.1 mm (finish)

Flat Bars & Rectangular Bars

  • Width × Thickness: 50×20 – 1,500×500 mm
  • Length: up to 5,000 mm
  • Turbine blade flat bars: width up to 300 mm
  • Surface: black / rough machined / finish machined

Seamless Rolled Rings

  • Outer Diameter (OD): 200 – 6,000 mm
  • Height: 50 – 2,000 mm
  • Wall Thickness: 30 – 500 mm
  • Contoured / profiled rings: available
  • Flanged rings: available

Rotor Shafts & Step Shafts

  • Overall Length: up to 15,000 mm
  • Max. Diameter: Ø2,000 mm
  • Min. Diameter: Ø80 mm
  • High-speed balancing (HST): available
  • Max. shaft weight: ~30,000 kg

Hollow Forgings & Cylinders

  • Outer Diameter: 300 – 3,000 mm
  • Inner Diameter: 100 – 2,500 mm
  • Wall Thickness: 30 – 600 mm
  • Length: up to 5,000 mm
  • Bore tolerance: H8 – H10

Discs, Blocks & Plates

  • Diameter: Ø300 – Ø3,000 mm
  • Thickness: 30 – 1,200 mm
  • Rectangular blocks: up to 2,500×1,500×800 mm
  • Disc bore: machined to drawing
Note: All dimensions listed represent standard production capability based on our 6300T hydraulic press and 5M seamless ring rolling machine. Minimum order quantity (MOQ) is 1 piece for custom forgings. Forging tolerances comply with EN 10243-1 (open die forgings) unless otherwise specified.

Manufacturing Standards & Advanced Melting Process

Our 1.4922 (X20CrMoV11-1) forged parts meet many main international standards like EN 10302:2008, EN 10222-2:2000, EN 10216-2:2014, EN 10088-1:2005, and ASTM equivalent standards. We give full EN 10204 3.1/3.2 Mill Test Certificates (MTC) for all parts.

We use premium raw material produced via an advanced multi-stage steelmaking route: Basic Electric Furnace (EAF) + Argon Oxygen Decarburization (AOD) + Vacuum Oxygen Decarburization (VOD) duplex melting process, with optional Electroslag Remelting (ESR) available per client requirements. ESR is particularly recommended for applications requiring the highest cleanliness, isotropic mechanical properties, and 100,000-hour creep service at 600°C. This melting route achieves sulfur levels below 0.010% and phosphorus below 0.025%, significantly tightening the impurity control beyond minimum standard requirements. See our advanced melting and forging equipment

Chemical Composition of 1.4922 (X20CrMoV11-1) Steel (Weight %)

The following table compares the EN 10302 standard specification against our factory-controlled internal target range. Our tighter internal controls — particularly on carbon, chromium, and impurity elements — are designed to deliver more consistent batch-to-batch mechanical properties and better predictability in long-term creep performance.

Source: EN 10302:2008; Jiangsu Liangyi internal quality control standard
ElementEN 10302 Standard RangeJiangsu Liangyi Internal ControlPrimary Function
Carbon (C)0.17 – 0.23%0.18 – 0.22%Martensitic matrix strength
Chromium (Cr)10.0 – 11.5%10.3 – 11.2%Oxidation & corrosion resistance
Molybdenum (Mo)0.5 – 0.8%0.55 – 0.75%Solid solution & carbide hardening, creep strength
Vanadium (V)0.1 – 0.3%0.15 – 0.25%Fine carbide precipitation, creep resistance
Niobium (Nb)0.25 – 0.55%0.30 – 0.50%Grain refinement, carbide stabilization
Nickel (Ni)0.2 – 0.6%0.3 – 0.5%Toughness improvement
Manganese (Mn)0.4 – 0.9%0.5 – 0.8%Deoxidation, hardenability
Nitrogen (N)0.05 – 0.10%0.06 – 0.09%Austenite stabilizer, nitride formation
Silicon (Si)≤ 0.50%≤ 0.40%Deoxidation
Boron (B)≤ 0.0015%0.0010 – 0.0015%Grain boundary strengthening
Aluminium (Al)≤ 0.020%≤ 0.015%Controlled low to avoid AlN formation
Phosphorus (P)≤ 0.030%≤ 0.025%Impurity — restricted for toughness
Sulfur (S)≤ 0.015%≤ 0.010%Impurity — restricted for toughness & sour service
Engineering Note: The interplay between carbon, chromium, and vanadium/niobium is important. Too much carbon promotes coarse carbide networks that degrade toughness; too little reduces the volume fraction of fine M₂₃C₆ carbides that provide creep resistance. Our internal carbon target of 0.18–0.22% is deliberately centered in the lower half of the EN range to balance these competing requirements for rotating machinery applications.

1.4922 (X20CrMoV11-1) International Equivalent Grade Cross-Reference

Steel grade designation varies significantly across national and international standards. The table below provides a cross-reference of 1.4922 (X20CrMoV11-1) equivalents across major standards used by our global client base. Note that "equivalent" in this context means functionally similar — no two standards define the exact same composition and property window, and direct interchangeability requires engineering verification for critical pressure-retaining components.

Cross-reference compiled from EN 10302, ASTM A182/A336, GB/T 8732, NF EN standards. Verify with your engineering team before substitution in code-governed applications.
Standard SystemGrade / DesignationNotes on Equivalence
EN (European)1.4922 / X20CrMoV11-1Primary designation — EN 10302:2008
EN (older DIN)X20CrMoV12-1 / X20CrMoNiV11-1-1Legacy DIN designation; composition nominally identical
GB/T (China)20Cr11MoV (GB/T 8732)Close equivalent; Cr upper limit slightly lower at 11.0%
ASTM / ASME (USA)No direct equivalent; closest: F6NM (A182)F6NM has lower C and higher Ni; different property balance. Requires engineering review
AFNOR (France)Z20CDV11.1 (NF EN)Essentially identical; adopts EN harmonized composition
BS (UK)Adopted EN designation post-2004UK uses EN 10302 directly; no separate BS equivalent
JIS (Japan)No direct JIS equivalentJapanese power plant projects typically accept EN certificate by agreement
GOST (Russia/CIS)20X11MF (approximate)Approximate; GOST 20X11MF has slightly different V+Mo balance
IS (India)Adopts EN/ASTM by project specIndian power projects specify EN 10302 or equivalent; no dedicated IS grade
Procurement Tip: When sourcing for projects under ASME Boiler & Pressure Vessel Code, clients should note that 1.4922 (X20CrMoV11-1) is not listed in ASME Section II Part A or Part D. For ASME-governed projects, engineering approval under Code Case or similar mechanism is typically required, or an ASTM-listed equivalent must be specified. Our technical team can provide material documentation to support this approval process.

Physical & Thermal Properties of 1.4922 (X20CrMoV11-1) Forging Steel

Physical properties are necessary for finite element analysis (FEA), modeling thermal-mechanical fatigue, and calculating piping stress. The following numbers are the actual values for forgings made at our facility that have been quenched and tempered (QT).Values at elevated temperatures were obtained from creep testing specimens cut from production forgings and tested according to EN ISO 204 procedure.

Test condition: QT state (+QT1), measured on Ø100mm bar specimens. Values at 20°C per EN ISO 6892-1; elevated temperature values per EN ISO 6892-2.
Physical Property20°C200°C400°C500°C600°C
Density (g/cm³)7.727.687.627.587.53
Elastic Modulus — E (GPa)210200188180170
Thermal Conductivity — λ (W/m·K)25.026.527.528.028.5
Mean Thermal Expansion — α (×10⁻⁶/°C)11.211.812.112.5
Specific Heat Capacity — Cp (J/kg·K)460490530560600
Electrical Resistivity (μΩ·m)0.700.820.991.081.18
Poisson's Ratio (ν)0.28 – 0.30 (relatively stable across temperature range)
Design Implication — Thermal Expansion: The mean thermal expansion coefficient of 1.4922 (approximately 12.1×10⁻⁶/°C at 500°C) is notably lower than austenitic stainless steels (≈17×10⁻⁶/°C), making 1.4922 a thermally compatible choice when joining to ferritic low-alloy steels in mixed-material piping systems. The lower thermal expansion reduces differential stress at dissimilar metal welds — a significant advantage in cyclic temperature service such as turbine start-stop duty.

1.4922 vs. 1.4923 vs. P91 (1.4903) vs. P92 (1.4901) — Engineering Comparison

Engineers selecting martensitic creep-resisting steel for high-temperature service routinely compare 1.4922 (X20CrMoV11-1) against its close relatives. The following comparison covers the four grades most commonly specified in power generation, petrochemical, and industrial turbine applications. Understanding the trade-offs helps avoid both over-specification (unnecessary cost) and under-specification (premature failure).

All creep rupture values are approximate 100,000-hour minimum values per EN 10302 / ASTM data. Weldability rating is relative (1 = most demanding, 4 = least demanding).
Property / Feature1.4922 (X20CrMoV11-1)1.4923 (X22CrMoV12-1)P91 / 1.4903 (X10CrMoVNb9-1)P92 / 1.4901 (X10CrWMoVNb9-2)
Cr Content (%)10.0 – 11.510.5 – 12.58.0 – 9.58.5 – 9.5
Max Continuous Temp.600°C600°C625°C650°C
100,000h Rupture Strength at 550°C (MPa)~140~150~180~210
100,000h Rupture Strength at 600°C (MPa)~75~80~100~130
Oxidation Resistance (steam, ≤600°C)Excellent (11% Cr)Excellent (12% Cr)Good (9% Cr)Good (9% Cr)
H₂S / Sour Service ResistanceVery Good — meets hardness & composition requirements of NACE MR0175 / ISO 15156Very GoodAcceptableAcceptable
Impact Toughness (KV, +20°C)≥ 40 J (NT)≥ 27 J (NT)≥ 41 J≥ 27 J
Weldability (preheat required)200 – 300°C250 – 350°C200 – 300°C + strict PWHT200 – 300°C + strict PWHT
Post-Weld Heat Treatment (PWHT)Required: 720 – 760°CRequired: 720 – 760°CMandatory: 730 – 760°C (critical)Mandatory: 730 – 760°C (critical)
Thermal Expansion Mismatch w/ Carbon SteelLow (good compatibility)LowLowLow
Relative Material CostModerateModerate (+5–10%)Higher (+20–30%)Highest (+40–60%)
Typical ApplicationsTurbine shafts, valve spindles, steam pipelines, rings ≤600°CHigh-hardness turbine blades, guide vanes ≤600°CMain steam pipes, headers, turbine rotors ≤625°CUltra-supercritical boiler tubes, rotors ≤650°C
Selection Guidance from Our Engineering Team: If your operating temperature is consistently below 580°C and your design involves dynamic rotating parts with fatigue loading, 1.4922 is typically the most cost-effective choice — its 11% chromium provides a meaningful corrosion resistance margin over P91/P92 in environments with steam or mild H₂S. If the design temperature exceeds 600°C or approaches 625°C, we recommend upgrading to P91 (1.4903) which we also manufacture. At temperatures above 625°C, P92 (1.4901) should be considered despite the higher cost.

Precision Heat Treatment Process for 1.4922 (X20CrMoV11-1) Forgings

We operate 10 fully automated heat treatment furnaces with ±5°C temperature uniformity across the working zone, verified regularly by multi-point thermocouple surveys and calibrated instrumentation. Every 1.4922 (X20CrMoV11-1) forging undergoes a documented, traceable heat treatment cycle — furnace chart records, time-temperature profiles and thermocouple calibration certificates are included with the EN 10204 3.1 MTC on request. Our standard heat treatment processes are as follows:

Soft Annealing

Heat the forgings to 730–780°C, hold for sufficient time according to the section thickness (minimum 1 hour per 50 mm), then cool slowly in the furnace (≤50°C/h) or in still air for thinner sections. This process dissolves fine carbides, reduces hardness to below 240 HBW, and significantly improves machinability — important for rough machining operations before final heat treatment. The slow furnace cool guarantees that chromium carbides remain in solution rather than reprecipitating at grain boundaries, which would otherwise cause susceptibility to temper embrittlement.

Stress Relieving

To remove machining residual stress and minimize distortion during final heat treatment, we perform stress relieving by heating the machined parts to 650–680°C, holding for at least 1 hour per 25 mm of maximum section thickness, followed by controlled air cooling. This intermediate step is particularly important for complicate geometries such as step shafts and flanged rings where differential machining stock removal creates asymmetric residual stress patterns. Skipping this step often results in dimensional movement during final QT that exceeds drawing tolerances.

Hardening (Austenitizing + Quenching)

Austenitize the forgings at 1020–1070°C, with holding time calculated as minimum 1 hour per 75 mm of section thickness to guarantee complete carbide dissolution and full austenite transformation. Quenching medium (air or oil) is chosen  based on section size and hardenability requirements: sections below 100 mm are air quenched; heavier sections up to 500 mm may need accelerated forced-air or oil quenching to get full martensitic transformation throughout the cross-section. A uniform through-hardness profile is verified by hardness traverse testing across the full cross-section before tempering proceeds.

Tempering

Perform tempering at 720–780°C, holding for a minimum of 2 hours per 50 mm of section thickness, then air cooling. The precise tempering temperature is selected based on the target mechanical property window: the lower end of the range (720–740°C) delivers higher strength with hardness ~260–280 HBW, preferred for turbine blade flat bars; the upper end (750–780°C) delivers superior toughness with hardness ~220–250 HBW, preferred for rotating shafts and rings where dynamic fatigue loading governs design. Double-tempering cycles are performed for forgings above 1,000 mm cross-section to guarantee complete martensite transformation of any retained austenite from the quench.

Mechanical Properties of 1.4922 (X20CrMoV11-1) Forging Steel

All mechanical property test specimens are cut from the forging body at the prescribed location and orientation per EN 10302 sampling requirements. For large forgings, specimens are cut from the 1/4T and 1/2T positions (T = forging thickness or diameter) to confirm through-thickness property consistency. Both longitudinal (L) and transverse (T) specimens are tested where required by the applicable product standard.

Guaranteed minimum values per EN 10302:2008 for forgings in QT and NT heat treatment condition. Actual test results from our production typically exceed these minimum values by 5–15%.
Mechanical PropertyHeat Treatment ConditionSpecimen OrientationGuaranteed Value
Tensile Strength (Rm)Normalized + Tempered (+NT)Longitudinal690–840 MPa
Tensile Strength (Rm)Quenched + Tempered (+QT)Longitudinal700–850 MPa
Min. Yield Strength (ReH)Normalized + Tempered (+NT)Longitudinal≥ 490 MPa
0.2% Proof Strength (Rp0.2)Quenched + Tempered (+QT)Longitudinal≥ 500 MPa
Elongation at Fracture (A)Normalized + Tempered (+NT)Longitudinal≥ 17%
Elongation at Fracture (A)Normalized + Tempered (+NT)Transverse≥ 14%
Elongation at Fracture (A)Quenched + Tempered (+QT)Longitudinal≥ 15 – 16%
Longitudinal Impact Energy (KV, +20°C)Normalized + Tempered (+NT)LongitudinalMin. 40 J
Longitudinal Impact Energy (KV, +20°C)Quenched + Tempered (+QT)Longitudinal27–39 J
Transverse Impact Energy (KV, +20°C)Quenched + Tempered (+QT)TransverseMin. 27 J
Brinell Hardness (HBW)Quenched + Tempered (+QT)Surface220 – 290 HBW

High-Temperature Creep & Stress Rupture Strength of 1.4922 (X20CrMoV11-1)

Creep rupture strength — the stress that causes rupture after a given number of hours at a specified temperature — is the single most critical property for selecting materials in long-life, high-temperature pressure equipment. Unlike tensile strength which is measured instantaneously, creep properties reflect the material's resistance to time-dependent plastic deformation under sustained load. For turbine shafts and steam pipelines designed for 200,000-hour service life, creep data is the governing design input.

The following table presents our factory-validated average creep stress rupture strength values for 1.4922 (X20CrMoV11-1) in the quenched-and-tempered condition (+QT). Data is derived from long-term testing programs conducted on specimens machined from production forgings. Values represent the mean of multiple test batches; design engineers should apply appropriate safety factors (typically 1.5× on mean rupture or use minimum values per EN 13445 or applicable design code).

Average stress rupture strength (MPa) for 1.4922 (+QT condition). Testing per EN ISO 204. Values represent batch mean from production forging specimens; for design, consult EN 10302:2008 Annex data or applicable ECCC recommendations.
Test Temperature1,000 h Rupture (MPa)10,000 h Rupture (MPa)30,000 h Rupture (MPa)100,000 h Rupture (MPa)200,000 h Rupture (MPa, est.)
450°C~380~310~270~230~200
500°C~300~240~210~175~155
525°C~255~200~170~140~120
550°C~210~165~140~112~96
575°C~165~125~104~83~70
600°C~120~92~80~65~54
620°C~88~65~55~44~37
650°C~55~38~30
Why the 580°C Design Threshold Matters: Notice that the 100,000-hour rupture strength at 575°C (~83 MPa) drops to ~65 MPa at 600°C — a 22% reduction over just 25°C. This steep gradient is characteristic of 11% Cr martensitic steels and explains why most plant operators using 1.4922 set conservative alarm limits at 580°C metal temperature rather than 600°C. Operating consistently at 595–600°C significantly shortens expected component life compared to operation at 570–580°C, even when both temperatures are within the material's official rating. Our engineering team routinely assists clients in establishing safe operating envelopes based on actual measured creep data rather than relying solely on the standard maximum temperature rating.

Minimum Creep Rate (Secondary Creep) Data

In addition to rupture life, the minimum creep rate during secondary (steady-state) creep governs the allowable deformation in precision components such as turbine casings and labyrinth seals where dimensional change over service life must remain within tight limits. For 1.4922 at 550°C under a stress of 100 MPa, the minimum creep rate is approximately 2×10⁻⁵ %/h, meaning total accumulated creep strain over 100,000 hours is approximately 2%, which is within acceptable limits for most turbine casing applications. At 600°C under the same stress, the minimum creep rate rises to approximately 8×10⁻⁵ %/h — four times higher — and component geometry change over the design life must be explicitly accounted for in the engineering design.

Weldability & Welding Guide for 1.4922 (X20CrMoV11-1) Forgings

1.4922 (X20CrMoV11-1) is weldable using standard arc welding processes, but its martensitic microstructure means that welding introduces significant hardness gradients and residual stress that must be managed through controlled preheat, interpass temperature, and mandatory post-weld heat treatment (PWHT). Skipping or shortcutting any of these steps risks cold cracking, stress corrosion cracking, or premature creep failure at the weld heat-affected zone (HAZ) — the most common failure mode for improperly welded 1.4922 components in service.

The following step-by-step guide is developed based on EN ISO 15614-1 principles and our accumulated production experience with 1.4922 steel. Clients who receive our forgings for in-field or shop welding can reference these process parameters as a baseline for developing and qualifying their own Welding Procedure Specifications (WPS).

Pre-Weld Inspection

Verify base metal hardness ≤290 HBW. Check chemical cert for P + S ≤ 0.040% combined. Ensure joint preparation is clean, free of scale, oil and moisture. Perform MT/PT on joint faces for existing cracks.

Preheat

Preheat to 200–300°C uniformly, measured ≥75 mm from the weld joint on both sides. Maintain preheat throughout the entire welding sequence. For sections >50 mm, use 250–300°C. Never weld cold — hydrogen cracking in the HAZ is the primary risk with insufficient preheat.

Interpass Temperature

Maintain interpass temperature between 200°C (minimum = preheat) and 300°C maximum. Exceeding 300°C risks HAZ grain coarsening and delta ferrite formation, both of which degrade creep properties. Use infrared thermometer to verify before each weld pass.

Filler Metal Selection

Use matching composition filler: AWS ER410NiMo (TIG/MIG) or E410NiMo-15 (SMAW) for butt joints. For hardfacing of sealing surfaces, Stellite 6 (Co-Cr-W alloy) overlay is applied by GTAW. Nickel-based fillers (e.g. Inconel 82/182) may be used at dissimilar metal joints — verify compatibility with your design code.

Heat Input Control

Limit heat input to 1.0–2.5 kJ/mm per pass. Excessive heat input (>3.0 kJ/mm) causes HAZ grain coarsening and loss of creep strength. Insufficient heat input (<0.8 kJ/mm) increases hydrogen cracking risk. Oscillation width should not exceed 3× electrode diameter.

Post-Weld Cooling

After the final weld pass, hold at preheat temperature (200–300°C) for minimum 2 hours before slow cooling to 80–120°C. This step allows hydrogen effusion from the weld and HAZ. Do NOT allow the weldment to cool below 80°C before PWHT. Cover with insulating blanket to control cooling rate.

PWHT (Post-Weld Heat Treatment)

Mandatory. Heat to 720–760°C at controlled rate ≤100°C/h above 400°C. Hold at PWHT temperature for minimum 1 hour per 25 mm of maximum weld throat thickness, with absolute minimum of 2 hours regardless of thickness. Cool at ≤100°C/h to 400°C, then free air cool. Document full temperature-time record.

Post-PWHT Inspection

After PWHT cooling to ambient: Brinell hardness check across weld, HAZ and base metal (target: weld ≤270 HBW, HAZ ≤290 HBW). Full UT of weld volume per EN ISO 17640. MT or PT on weld surface. Dimensional check if applicable.

Applicable Welding Processes: GTAW (TIG) is best for root passes and thin sections; SMAW (MMA) is good for all positions and is often used for site repairs; FCAW is good for joints with a high deposition rate; and SAW is good for heavy section groove joints in a shop. GMAW (MIG/MAG) is acceptable but should use low hydrogen shielding gas (Ar + 2–5% CO₂). All processes require qualified WPS per EN ISO 15614-1 or ASME IX.

Full-Process Quality Controlled Forging Production Flow

We implement a strict full-process quality control system for all 1.4922 (X20CrMoV11-1) forging parts, and we have modern equipment, such as a 6300T hydraulic forging press, 2000T fast forging machine, 5M seamless rolling machine, and complete nondestructive testing equipment to make sure all parts have high quality. Following are our standard production flow:

Raw material steel ingot incoming inspection (100% chemical composition verification by OES) → Precision cutting → Open die forging process (grain refinement and structure optimization) → Post forging heat treatment (Normalizing + Tempering) → Preliminary Ultrasonic Testing (UT) → Rough Machining → Secondary UT Inspection → Final Quenching + Tempering (QT) → Full performance inspection (UT, mechanical properties test, hardness test, grain size inspection) → Precision grooving → Stress relieve tempering → Machining of rotor holding position for HST → High Speed Balancing (HST) → Final dimensional inspection and surface finish test → Permanent marking (steel stamp) and anti-rust packaging → Storage and global shipment.

All our 1.4922 forgings are given 100% nondestructive testing before delivery, including UT per EN ISO 17640, MT per EN ISO 17638, PT per EN ISO 3452, and optional PMI (Positive Material Identification) by XRF to confirm alloy grade, ensuring zero defects and full compliance with client requirements and international standards. View our complete quality inspection equipment

Global Application Cases of China-Made 1.4922 (X20CrMoV11-1) Forgings

Our 1.4922 (X20CrMoV11-1) forging parts have been deployed in important industrial projects across more than 50 countries in Asia, Europe, the Middle East, North America, and Southeast Asia, with a proven track record of stable performance under demanding high-temperature and high-pressure service conditions. Following are our main application cases :

Thermal Power Plant Steam Turbine Components (Asia Market)

We supplied custom 1.4922 steam turbine rotor shafts, valve spindles, and seal rings for multiple large-scale thermal power projects in Asia. The client's main challenge was keeping stable creep resistance under continuous 580°C service at 16.7 MPa steam pressure. Our forgings were made of ESR-refined material with a custom double-tempering cycle developed specifically for this application, and they got impact toughness well above standard minimum values. 100% high-temperature mechanical property testing was performed at 600°C, confirming properties met design requirements with positive margin. The components have accumulated many years of continuous stable operation — a service record that led the client to place repeat orders for subsequent plant expansions.

Petrochemical High-Temperature Pipeline & Reactor Forgings (Middle East Market)

Our X20CrMoV11-1 forged high-pressure pipeline parts, flanges, and reactor shells were used for a large-scale refinery project in the Middle East. The project's important challenge was simultaneous resistance to H₂S-bearing sour gas service and long-term 550°C operation — a combination that rules out most standard carbon and low-alloy steels. Our forgings got sulfur content below 0.008% and phosphorus below 0.020%, meeting the material composition and hardness requirements of NACE MR0175 / ISO 15156, and passed the client's corrosion resistance qualification tests. We completed production and delivery of 120+ custom forgings within 45 days to meet the project's important commissioning schedule, with dedicated quality inspector presence throughout.

Industrial Gas Turbine Blade & Guide Ring Forgings (European Market)

We made precision X20CrMoV11-1 forged turbine blade flat bars and guide rings for a leading industrial gas turbine OEM in Germany. The client specified all parts must meet EN 10302 plus additional proprietary requirements including: dimensional tolerance within ±0.05 mm on important surfaces, consistent grain size ASTM No. 3–5, and maximum hardness variation of 15 HBW across any single forging. Our factory met all of its goals by using a combination of precise forging with the best reduction ratios, a tightly controlled tempering window, and 100% metallographic inspection for important supply batches. We have had a long-term stable relationship with this client, and we always send them qualified forging batches that are accepted on the first try. They now trust us as one of their Chinese suppliers.

Power Station Boiler & Valve System Components (North American Market)

Our 1.4922 forged valve seats, valve stems, and high-strength fasteners are supplied to a leading valve manufacturer in the United States for use in utility boiler systems across multiple North American power plants. The governing failure mode for these parts is low-cycle thermal fatigue from repeated boiler start-stop cycling — each cycle subjects the valve parts to a temperature swing from ambient to 580°C in under 4 hours. Our forgings met the client's proprietary low-cycle fatigue qualification requirements, with all test specimens passing the specified number of thermal cycles without crack initiation. All products meet ASTM A182 with optional Stellite 6 hardfacing on sealing surfaces applied in-house at our facility. We provide stable monthly delivery of valve part sets to this client on a just-in-time schedule.

Jiangsu Liangyi's advanced X20CrMoV11-1 steel forging production facility in Jiangyin, Jiangsu, China

Why Choose Jiangsu Liangyi as Your 1.4922 (X20CrMoV11-1) Forging Partner in China

25+ Years of Focused High-Temperature Alloy Experience

Since 1998, we have focused exclusively on high-temperature alloy and creep resisting steel forgings for power generation and oil & gas industries. This narrow focus means our metallurgists, heat treatment engineers and quality inspectors have accumulated deep, specific expertise in 1.4922 behavior — not generic forging experience applied to a new material.

Complete In-House Production — No Outsourcing

From EAF steel melting, open die forging, ring rolling, heat treatment and CNC machining to final NDT inspection and surface treatment — every step is performed within our own 120,000 m² facility in Jiangyin. No sub-contracting means no quality gaps, no hidden lead time, and full traceability of every batch from ingot to finished forging.

Validated Equipment for Heavy & Precision Forgings

Our 6300T hydraulic press handles single ingots up to 35 tons; our 5M ring rolling machine covers rings up to 6 m OD; our 10 programmable heat treatment furnaces control temperature to ±5°C with regular multi-point thermocouple surveys and calibrated instrumentation. This combination of heavy forming capacity and precision thermal control is rare among Chinese forging manufacturers.

Global Export with 7×24 English Technical Support

Exporting to 50+ countries since 2003, our sales and technical team provides 7×24 English support, and can accommodate third-party inspection by SGS, TÜV, BV or the buyer's nominated inspector upon prior arrangement (inspection fees at buyer's account unless otherwise agreed). We provide DDPW/DDP incoterms and can generate documentation packages meeting EU, ASME, and customer-specific QA requirements within 5 working days of order confirmation.

Frequently Asked Questions — 1.4922 (X20CrMoV11-1) Forgings

1.4922 (X20CrMoV11-1) steel is used for working conditions at high temperatures up to 600°C for a long time without stopping. In this temperature range, it is very resistant to creep and oxidation. The 100,000-hour creep rupture strength at 600°C is about 65–75 MPa, which gives most power generation applications a good design margin. The material can handle short-term peaks of up to 650°C without significant damage, but long-term exposure above 620°C speeds up carbide coarsening and should be avoided in parts designed for 200,000-hour service life.
The main difference is the content of carbon and chromium. 1.4923 contains higher carbon (0.18–0.24% vs. 0.17–0.23%) and slightly higher maximum chromium (12.5% vs. 11.5%). In practice, 1.4923's higher carbon delivers a harder, higher-strength martensitic matrix, making it preferable for static components like turbine blades and guide vanes where hardness and wear resistance govern design. By contrast, 1.4922's lower carbon provides significantly better toughness (minimum impact energy ≥40 J vs. ≥27 J) and weldability, making it the preferred choice for rotating shafts, valve spindles, and forged rings where fatigue loading and field repair welding are part of the operating reality. Both grades have similar maximum operating temperatures (~600°C) and similar creep strength at a given temperature. Explore our full range of forging material grades
P91 (X10CrMoVNb9-1 / 1.4903) offers roughly 30–40% higher creep rupture strength at 600°C compared to 1.4922 (approximately 100 MPa vs. 75 MPa at 100,000 hours), and a higher maximum operating temperature of 625°C. However, 1.4922's 11% chromium content gives it a significant advantage in steam oxidation resistance and corrosion resistance in H₂S-bearing or CO₂-rich environments — situations where 9% Cr P91 may suffer accelerated scale growth. 1.4922 is also more forgiving in welding: while both require preheat and PWHT, P91 weld failures from improper PWHT are a well-documented industry problem (Type IV cracking), whereas 1.4922 is less sensitive to HAZ microstructure degradation. In practice, if the design temperature is reliably below 580°C, 1.4922 is often the better balance of performance, cost, and fabrication risk.
Our 1.4922 (X20CrMoV11-1) forging parts fully meet EN 10302:2008 (creep resisting steels), EN 10222-2:2000 (steel forgings for pressure purposes), EN 10216-2:2014 (seamless steel tubes), and EN 10088-1:2005. For clients working under ASTM/ASME frameworks, we can produce to equivalent composition and property requirements with supporting documentation for engineering approval. We can also manufacture to client-specified proprietary standards, provided that the requirements do not conflict with sound metallurgical practice. All products are covered by EN 10204 3.1 MTC as standard, with 3.2 available.
Standard lead time for custom 1.4922 forgings is 30–45 days covering raw material procurement, melting/casting, open die forging, post-forging heat treatment (NT), preliminary UT, and rough machining. For precision-machined parts that need final QT heat treatment, dimensional tolerance control, and full NDT package, the lead time is 45–60 days. For large hollow forgings above 10 tons or ring forgings above 4 m OD , the lead time is 60–75 days due to extended heat treatment cycles. We also can speed up production for urgent orders — contact us with your required delivery date and we will advise on feasibility. We keep a standing stock of 1.4922 round bar blanks in common diameter ranges for emergency supply requirements.
1.4922 requires controlled welding conditions: preheat 200–300°C; maximum interpass temperature 300°C; recommended filler AWS ER410NiMo (TIG/MIG) or E410NiMo-15 (SMAW); mandatory post-weld heat treatment (PWHT) at 720–760°C for minimum 1 hour per 25 mm thickness. Post-PWHT hardness should be verified — weld zone ≤270 HBW, HAZ ≤290 HBW. Cold cracking due to insufficient preheat and hydrogen cracking are the primary welding risks. Our welding guidelines are based on EN ISO 15614-1 principles and can serve as a technical reference for clients developing their own qualified procedures.
We provide a complete EN 10204 3.1 Mill Test Certificate (MTC) as standard for all 1.4922 forgings, including: OES chemical composition analysis, room-temperature tensile test, Charpy V‑notch impact test, Brinell hardness check, heat treatment record with furnace charts, UT inspection report, and dimensional inspection record. For creep‑critical uses, we can also supply high‑temperature tensile data at 400°C, 500°C and 600°C as extra documentation. EN 10204 3.2 certificates, which need third‑party inspection and countersignature by SGS, TÜV, Bureau Veritas or the buyer’s appointed inspection company, are available by prior arrangement at an extra cost upon customer request. All test reports list the specific heat number, forging number and final inspection date for full traceability.

Contact Us for Custom 1.4922 (X20CrMoV11-1) Forging Solutions

Jiangsu Liangyi is your trusted manufacturer and supplier of high-quality 1.4922 (X20CrMoV11-1) forging parts. We have more than 25 years of experience making forged bars and rings, whether you need standard forged bars and rings, or custom complex turbine parts and pressure vessel parts, we are ready to provide technically grounded, cost-effective solutions.

Send us your drawing, material specification, quantity, and delivery requirement — our technical sales team will respond with a detailed technical confirmation and commercial quotation within 24 hours (business days).

Inquiry Email: sales@jnmtforgedparts.com

Phone / WhatsApp: +86-13585067993

Official Website: https://www.jnmtforgedparts.com

Factory Address: Chengchang Industry Park, Jiangyin City, Jiangsu Province 214400, China

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