26NiCrMoV11-5 (1.6948) Forging Parts

Leading China Manufacturer of High-Quality 26NiCrMoV11-5 Open Die Forgings from Jiangyin, Jiangsu Province

26NiCrMoV11-5 gas steam turbine rotor shaft manufactured in Jiangyin China factory
26NiCrMoV11-5 (1.6948) Gas & Steam Turbine Rotor Shaft - Precision Forged by Jiangsu Liangyi

About 26NiCrMoV11-5 (1.6948) Forging Steel

Jiangsu Liangyi Co., Limited, established in 1997 and strategically located in Chengchang Industry Park, Jiangyin City, Jiangsu Province, is a professional ISO 9001:2015 certified manufacturer of premium 26NiCrMoV11-5 (1.6948) open die forging parts in China. We have over 25 years of experience of the forging industry and have supplied thousands of tons of high-quality 26NiCrMoV11-5 forged parts to satisfied customers in more than 50 countries across Asia, Europe, North America, South America, Africa and Oceania.

Material Advantages of 26NiCrMoV11-5 Steel

26NiCrMoV11-5, also designated by the European material number 1.6948, is a premium low-alloy Ni-Cr-Mo-V engineering steel with excellent performance for important high-temperature and high-stress service conditions. Compared with conventional alloy steels including AISI 4140 and AISI 4340, 26NiCrMoV11-5 presents distinct technical superiorities:

  • Superior high-temperature strength: Maintains excellent tensile strength and yield strength at operating temperatures up to 550°C
  • Outstanding low-temperature toughness: Excellent Charpy V-notch impact resistance even at sub-zero temperatures
  • Exceptional hardenability: Through-hardening capability for large-section parts up to 30 tons
  • Excellent fatigue resistance: Superior fatigue life for rotating machinery parts
  • High creep resistance: Excellent creep properties for long-term high-temperature service
  • Good machinability: Balanced composition for efficient machining while keeping properties

These unique metallurgical properties make 26NiCrMoV11-5 (1.6948) the premium material choice for mission-critical parts in power generation, oil & gas, marine, and heavy machinery industries where absolute reliability, durability and performance are non-negotiable requirements.

Available 26NiCrMoV11-5 Forged Product Shapes

At our state-of-the-art 80,000 m² manufacturing site in Jiangyin, we are fully capable of producing 26NiCrMoV11-5 (1.6948)  forged parts in a wide range of shapes and dimensions, fully customized to your engineering specifications and technical drawings. Following are our full production scope covers all types of open die forgings and seamless rolled rings:

Forged Bars & Rods

Round bars, square bars, flat bars, rectangular bars and solid rods up to 2 meters in diameter and 15 meters in length

Seamless Rolled Rings

Seamless rolled rings, guide rings, seal rings, labyrinth rings, gear rings and casing rings up to 6 meters in diameter

Hollow Forged Parts

Hubs, housings, shells, sleeves, bushes, hollow bars and heavy-wall cylinders up to 3 meters outer diameter

Plates, Discs & Blocks

Discs, disks, blocks, plates, flanges, tubes and custom forged shapes up to 3 meters in diameter

Specialized Turbine & Rotating Parts

Our main technical expertise and competitive advantage lies in manufacturing high-precision 26NiCrMoV11-5 turbine parts for demanding power generation applications:

  • Gas turbine rotor shafts (monobloc and built-up construction)
  • Steam turbine rotor shafts (HP, IP and LP sections)
  • High pressure (HP) and intermediate pressure (IP) turbine rotors
  • Generator shafts and turbine shaft ends
  • Turbine blades, vanes and guide vanes
  • Valve spindles, stems, rods and valve seats
  • Packing seals, diaphragms and rotor end rings
  • Double-headed studs, bolts and critical fasteners
  • Couplings, flanges and connection parts
1.6948 seamless rolled forged steel rings produced by Jiangsu Liangyi China
1.6948 (26NiCrMoV11-5) Seamless Rolled Forged Steel Rings - Precision Manufacturing by Jiangsu Liangyi

26NiCrMoV11-5 Manufacturing Capabilities

We have modern equipment in our factory, such as cutting-edge forging, machining and heat treatment equipment so that we can produce large-scale 26NiCrMoV11-5 (1.6948) forged parts with excellent precision, consistent quality and reliable performance:

  • Maximum single-piece forging weight: Up to 30 tons per individual forging
  • Maximum length capacity: Up to 15 meters for turbine rotor shafts
  • Maximum diameter capacity: Up to 2 meters for shafts and 6 meters for seamless rolled rings
  • Annual production capacity: 120,000 tons of premium forged steel products
  • Facility size: 80,000 square meters of modern manufacturing space
  • Fixed asset investment: Over 40 million USD in specialized equipment

Raw Material Production Process

We keep complete control over the entire production value chain from initial steel melting to final inspection and packaging, guaranteeing the highest quality standards for our 26NiCrMoV11-5 products. Our premium raw material is produced using state-of-the-art melting and refining processes:

  • Basic Electric Arc Furnace (EAF) primary melting
  • Ladle Furnace (LF) secondary refining
  • Argon Oxygen Decarburization (AOD) for stainless grades
  • Vacuum Oxygen Decarburization (VOD) for ultra-low carbon grades
  • Vacuum Degassing (VD) for hydrogen removal
  • Electroslag Remelting (ESR) - available upon client request for ultra-high purity critical applications

26NiCrMoV11-5 Heat Treatment Process — Full Engineering Detail

 Heat treatment serves as the decisive process in defining the final mechanical properties of 26NiCrMoV11-5 forged parts. Unlike conventional low-alloy steels, this grade needs highly precise thermal cycling owing to its elevated nickel content. The alloy’s high nickel composition alters the martensite start (Ms) temperature, necessitating controlled cooling rates to prevent retained austenite formation and mitigate temper embrittlement risks. Outlined below is the complete heat treatment sequence implemented at Jiangsu Liangyi, refined through over 25 years of practical production expertise with this specialized steel grade.

Step 1 — Preliminary Soft Annealing (Optional, Pre-Machining)

 For large-section forgings scheduled for rough machining before final heat treatment, a soft annealing process is performed to lower hardness and improve machinability. The treatment is carried out at 650–710°C with a soaking hold of 4 to 6 hours, followed by slow furnace cooling at a maximum rate of 20°C/h until the temperature drops below 300°C. This preliminary step is unnecessary for parts supplied in the quenched and tempered (Q+T) delivery condition.

Step 2 — Preliminary Normalizing (Grain Refinement)

Large-section forgings with a diameter over 500 mm or a weight exceeding 5 tons undergo a normalizing process prior to final quenching and tempering (Q+T). This step eliminates banded microstructures induced by forging, establishing a uniform, fine-grained austenitic base structure.Process parameters: heating temperature 870–920°C (typical at 890°C), with a minimum soaking time of 1 hour per 100 mm of important section thickness, followed by air cooling to ambient temperature.

Step 3 — Austenitizing / Hardening

 This represents the most important stage of the process. The forging is heated to the austenitizing temperature to fully dissolve carbides and form a homogeneous austenite matrix. For 26NiCrMoV11-5, the optimal austenitizing range is 840–880°C, with 860°C adopted as our standard target temperature for turbine rotor shafts. Excessively high austenitizing temperatures will coarsen prior austenite grains and degrade impact toughness. This risk needs strict control, as the steel features a low maximum silicon content of 0.15%, which inherently restricts its resistance to high-temperature grain growth.

Holding time guideline: Minimum 1 hour per 25mm of effective cross-section thickness, with an absolute minimum of 3 hours for sections above 500mm. For a 1,000mm diameter rotor shaft this typically means 10–12 hours at temperature before quenching commences.

Step 4 — Quenching

Quenching medium is chosen based on section size to get adequate through-hardening while controlling the risk of quench cracking — a genuine concern for large Ni-Cr-Mo-V forgings:

  • Sections ≤ 250mm diameter: Oil quenching (60–80°C bath temperature). Fastest cooling, maximum hardness gradient, suitable for smaller parts.
  • Sections 250–600mm diameter: Accelerated oil quenching or water-polymer solution (5–8% polymer concentration). Balances hardening depth with thermal stress management.
  • Sections > 600mm diameter (turbine rotors): Water-polymer spray quenching or controlled water immersion.The high Ni content (2.40–3.10%) of 26NiCrMoV11-5 makes it very hardenable, so it can be hardened all the way through even in sections that are 1,000mm or more thick.

Immediately after quenching, the forging surface temperature is monitored and the part must be transferred to the tempering furnace while still warm (above 80°C) to avoid cold cracking caused by high transformation stresses in the martensitic structure.

Step 5 — Double Tempering (Standard Practice for Turbine Rotors)

Single tempering is adopted as standard for general engineering parts. For turbine rotor shafts and other important-duty parts, however, Jiangsu Liangyi implements double tempering  as a mandatory standard procedure. The first tempering cycle tempers as-quenched martensite and relieves high residual transformation stresses. The second cycle further tempers any fresh martensite generated during cooling after the first tempering step, yielding a fully stabilized, uniformly tempered martensite microstructure across the full cross‑section of the forging.

  • First Tempering: 580–650°C, hold 2h per 25mm of effective section (minimum 6 hours for rotors), furnace cool to below 300°C
  • Second Tempering: Same temperature as first tempering ±10°C, same holding time, air or furnace cool

Tempering temperature serves as the main parameter governing the final balance of strength and toughness. Elevated tempering temperatures (630–650°C) marginally lower tensile strength while delivering substantial improvements in Charpy impact properties and minimizing the risk of temper embrittlement. This control is especially vital for 26NiCrMoV11-5, as the material is prone to reversible temper embrittlement (RTE) when slowly cooled through the important temperature range of 375–575°C after tempering.

Step 6 — Post-Machining Stress Relieving

 After rough machining, a stress‑relief annealing treatment at 550–600°C , held for 4–8 hours according to section thickness, is recommended to delete residual machining stresses prior to final precision machining. This effective measure prevents dimensional distortion during finishing operations and removes localized stress concentrations that may initiate fatigue cracking under service conditions. Crucially, the stress‑relief temperature must be maintained at least 30 °C below the final tempering temperature, so as to avoid unintended softening and degradation of the base material’s mechanical properties.

26NiCrMoV11-5 Heat Treatment Parameters — Quick Reference
StageTemperature (°C)Holding TimeCooling MethodPurpose
Soft Annealing650–7104–6 hoursFurnace cool ≤20°C/hImprove machinability
Normalizing870–9201h per 100mm sectionAir coolGrain refinement
Austenitizing840–880 (typ. 860)1h per 25mm, min 3hQuench immediatelyHomogenize austenite
QuenchingUntil surface <80°COil / polymer / waterMartensite formation
1st Tempering580–6502h per 25mm, min 6hFurnace/air coolTemper martensite
2nd Tempering580–650 (±10°C)Same as 1stFurnace/air coolEliminate fresh martensite
Stress Relieving550–6004–8 hoursFurnace cool to 300°CPost-machining stability

26NiCrMoV11-5 (1.6948) Chemical Composition

The following table specifies the standard chemical composition (weight percentage) of 26NiCrMoV11-5 forged gas turbine rotor shafts according to EN 10083-3 European standard. Our rigorous quality control makes sure every heat meets or exceeds these specifications:

ElementChemical SymbolMinimum Weight %Maximum Weight %
CarbonC0.220.32
SiliconSi0.15
ManganeseMn0.150.40
PhosphorusP0.015
SulfurS0.010
ChromiumCr1.201.80
MolybdenumMo0.250.45
NickelNi2.403.10
VanadiumV0.050.15

26NiCrMoV11-5 (1.6948) International Standard Equivalents

 One of the most common inquiries from international procurement engineers concerns the cross-standard equivalent of 26NiCrMoV11-5 under local national specifications. This poses a genuine engineering challenge, as 26NiCrMoV11-5 (1.6948) is a European-grade steel defined in EN 10083-3 (formerly DIN 17200), with no direct, one-to-one equivalent in other global material standards. The table below lists the closest approximate alternatives, matched by comparable chemical composition and typical service applications, rather than precise identical specifications.

Main Engineering Reminder: When you use cross-standard material substitution, please check if the alternative grade meets the specific mechanical property thresholds, heat treatment compatibility, and needed inspection criteria. Even alloys that are nominally the same have different composition limits and minimum guaranteed performance values across different standards. These differences must be fully reviewed for important part applications.

Standard / CountryGrade DesignationStandard NumberEquivalence LevelKey Differences
European (EN)26NiCrMoV11-5 / 1.6948EN 10083-3Reference standard
Germany (old DIN)26NiCrMoV11 5DIN 17200 (superseded)Direct (predecessor)EN 10083-3 replaced DIN 17200; composition identical
USA (ASTM) — Turbine RotorsASTM A470 Grade D/EASTM A470Approximate (application)A470 grades use different composition approach; verify specific grade requirements. No direct ASTM equivalent exists.
USA (AISI/SAE) — General4340 + V additionAISI 4340 Mod.Approximate (composition)AISI 4340 has lower Ni (1.65–2.00%) and no V. 26NiCrMoV11-5 offers superior toughness at large sections.
UK (BS)817M40 (En24)BS 970-1 (superseded)Approximate (application)En24 is a Ni-Cr-Mo steel without V addition; lower Ni content; less suited for large turbine rotors.
Japan (JIS)SNCM447JIS G4053Approximate (composition)SNCM447: Ni 1.6–2.0%, Cr 0.6–1.0%. Lower alloy content than 1.6948; suitable for smaller-section shafts.
China (GB)40CrNiMoAGB/T 3077Approximate (composition)40CrNiMoA: Ni 1.25–1.65%, Cr 0.6–0.9%. Significantly lower alloy than 26NiCrMoV11-5; adequate for moderate-duty shafts only.
Russia (GOST)38KhN3MFAGOST 4543Close (composition)38KhN3MFA: Ni ~3.0%, Cr ~0.8%, Mo ~0.35%, V ~0.1%. Nickel content very close; chromium is lower. Well-used for Russian turbine parts.
France (NF)30NCD11NF A35-565 (superseded)Approximate (application)Similar Ni-Cr-Mo alloying concept; now superseded by EN standards in France.
International — Turbine RotorsGrade as specified in ISO 12716 or VdTÜV MerkblattISO 12716 / VdTÜV WB 386Direct (application standard)Both standards specifically cover Ni-Cr-Mo-V turbine rotor steels; 26NiCrMoV11-5 is explicitly listed.

Our recommendation for international procurement:  When sourcing26NiCrMoV11-5 (1.6948) forgings from Jiangsu Liangyi, please specify the material by its official EN designation — either 26NiCrMoV11-5 or 1.6948 — together with the required mechanical property class and applicable project standard. This practice eliminates cross‑standard ambiguity and makes sure all quality documentation fully aligns with your engineering specifications and inspection protocols.
All material test certificates are issued based on EN 10083-3 as the primary governing standard. Cross-references to regional or national standards can be additionally annotated on documentation upon customer request.

26NiCrMoV11-5 Mechanical Properties

The following mechanical properties are obtained after proper quenching and tempering heat treatment for 26NiCrMoV11-5 forged steam turbine rotor shafts. All properties are verified through rigorous mechanical testing in our certified laboratory:

Mechanical PropertySymbolMinimum Guaranteed ValueUnit
Tensile StrengthRm850MPa
Yield Strength (0.2% offset)Rp0.2750MPa
Elongation (5x diameter)A518.0%
Reduction of AreaZ42.0%
Charpy V-Notch Impact ToughnessKV40J
Hardness (typical range)HB255–302HB

26NiCrMoV11-5 Physical & Thermal Properties

The mechanical property table alone cannot satisfy detailed engineering design needs. Structural analysts, FEA engineers and thermal engineers need a complete set of physical and thermal parameters to accurately simulate part performance under combined mechanical and thermal loads — the actual service working conditions of turbine rotors.
The following data are measured from our in-house laboratory testing, consistent with official technical data stipulated in EN 10083-3 for quenched and tempered delivery conditions. All parameters are temperature-dependent; linear interpolation is recommended for intermediate temperature working scenarios.

Physical Properties at Room Temperature (20°C)

Physical PropertySymbolValueUnitEngineering Significance
Densityρ7.83–7.86g/cm³Used for mass calculation; critical for rotor imbalance analysis
Young's Modulus (Elastic Modulus)E205–215GPaFoundation of all stress/strain FEA calculations
Shear ModulusG78–82GPaImportant for torsional analysis of rotating shafts
Poisson's Ratioν0.28–0.30Lateral strain response; required for triaxial stress analysis
Specific Heat CapacityCp460–480J/(kg·K)Governs thermal transient response during start-up and shutdown
Electrical Resistivityρₑ~0.25μΩ·mUsed for eddy current testing calibration in NDT

Thermal Properties vs. Temperature

For turbine rotor design, the temperature-dependent characteristics of thermal conductivity and thermal expansion coefficient are especially critical. These parameters directly govern thermal gradient distribution and the resultant thermal stresses experienced during transient start‑up operations. The following property values are measured for the material in its quenched and tempered condition:

TemperatureYoung's Modulus E (GPa)Thermal Conductivity λ (W/m·K)Mean Thermal Expansion α (×10⁻⁶/K, from 20°C)Specific Heat Cp (J/kg·K)
20°C21037–38465
100°C20636–3711.5475
200°C20035–3612.0490
300°C19333–3512.5510
400°C18531–3313.0530
500°C17529–3113.5550
550°C16828–3013.8565

Design Note from our Engineering Team: A frequent oversight in turbine rotor design is assuming constant material properties throughout the full operating temperature range. For 26NiCrMoV11-5, Young’s modulus decreases by approximately 20% from ambient temperature to 550°C, falling from around 210 GPa to 168 GPa. This temperature-driven reduction directly impacts critical speed calculations. Engineers relying solely on room-temperature modulus values for high-temperature critical speed analysis tend to overestimate critical speed by about 10–11%. Such deviation creates substantial safety margin risks, especially for rotating equipment operating close to critical speed during transient start-up and load change cycles. For accurate rotor dynamic assessment and reliable long-term operational safety, temperature-dependent material property data must always be adopted.

26NiCrMoV11-5 vs. Comparable Turbine Steels — Grade Selection Guide

 Choosing the right turbine rotor steel is one of the most important engineering decisions when designing a power plant. Picking the wrong material can cause early creep, fatigue failure, or not enough toughness at operating temperature — all of which have serious safety and operational results. This section gives an honest, technically thorough comparison of 26NiCrMoV11-5 (1.6948)  and the most commonly used alternative grades, based on our direct experience making all these materials.

Property / Factor26NiCrMoV11-5 (1.6948)30CrMoNiV5-11 (1.6946)34CrNiMo6 (1.6582)AISI 4340X12CrMoWVNbN10-1-1 (1.4939)
Carbon (wt%)0.22–0.320.27–0.340.30–0.380.37–0.430.10–0.15
Nickel (wt%)2.40–3.100.80–1.501.30–1.701.65–2.00
Chromium (wt%)1.20–1.802.50–3.001.30–1.700.70–0.909.5–11.0
Molybdenum (wt%)0.25–0.450.35–0.550.15–0.300.20–0.300.90–1.10
Vanadium (wt%)0.05–0.150.20–0.300.15–0.25
Min. Tensile Strength (MPa)850900900930720
Min. Yield Strength Rp0.2 (MPa)750760710830550
Min. Charpy KV Impact (J)403535~3540
Max. Recommended Service Temp.~550°C~580°C~450°C~400°C~620°C
Hardenability (large sections)ExcellentVery GoodGoodGoodModerate
Low-Temperature ToughnessExcellentGoodGoodGoodVery Good
Temper Embrittlement RiskModerate (high Ni)ModerateLowLowLow
Relative Raw Material CostHighMedium-HighMediumMediumVery High
Primary ApplicationHP/IP turbine rotors, large shaftsHP turbine rotors, compressor shaftsGears, shafts, general engineeringAerospace shafts, US marketUSC/advanced turbines >580°C

Which Grade Should You Choose? — A Practical Decision Framework

Based on our experience manufacturing all of these grades, here is the honest decision framework we share with our customers' engineers:

Choose 26NiCrMoV11-5 (1.6948) when: If your turbine or rotating equipment runs at 450–550°C, needs strong full-depth hardening for large-size parts over 400mm in diameter, needs great low-temperature toughness for cold or cryogenic working conditions, or needs official EN standard paperwork, this grade is the best option. Its high nickel content from 2.40% to 3.10% is its main strength, delivering unmatched hardening ability and toughness that standard turbine rotor steel grades cannot equal, especially for extra large cross-section parts.

Choose 30CrMoNiV5-11 (1.6946) when: operating temperatures stay above 550°C or near 580°C, and the working scene needs better high-temperature creep strength. More chromium and vanadium help keep the part stable at high heat, but cut down nickel content, which weakens its toughness in low-temperature environments.

Choose 34CrNiMo6 (1.6582) when: the application is a general engineering shaft, gear or structural parts operating below 450°C, and the cost differential of 26NiCrMoV11-5's high nickel content is not justified by the application requirements. This is a common and economical choice for industrial gearbox shafts, crane parts and heavy machinery.

Choose 9–12% Cr steels (such as X12CrMoWVNbN10-1-1) when: operating temperatures go above 580°C in ultra-supercritical (USC) steam turbines, where high-chromium ferritic steels are needed for better oxidation resistance. The downside is much lower strength and hardening performance, which calls for careful design work to guarantee solid material properties at the inner bore of large rotor parts.

26NiCrMoV11-5 (1.6948) Industrial Applications & Case Studies

 26NiCrMoV11-5 steel is widely used for extreme industries globally because it has excellent high strength, toughness, heat resistance and fatigue properties. Following are some of our successful application case studies from satisfied customers around the world:

Power Generation Industry

Project Reference: We have delivered over 50 full sets of 26NiCrMoV11-5 high-pressure and intermediate-pressure turbine rotors for large thermal power plants across China, India, Thailand, Vietnam and Indonesia. These well-made rotors run steadily under steam temperatures up to 550°C and working pressures up to 16 MPa, with a designed service life of more than 30 years.

Products Manufactured: Gas turbine rotor shafts, steam turbine rotors, generator shafts, turbine blades, vanes, valve spindles and important power generation parts

Oil & Gas Industry

Project Reference: We have produced large volumes of 1.6948 forged valve parts and wellhead equipment for major oil and gas projects in Saudi Arabia, UAE, Qatar, Kuwait and Oman. These key parts are used in wellhead systems, high-pressure pipeline systems and refinery facilities, holding up against extreme working pressures up to 15,000 psi and harsh service environments with corrosive hydrogen sulfide.

Products Manufactured: Valve spindles, valve seats, valve bodies, studs, bolts, flanges, tubing hangers and casing hangers

Marine & Shipbuilding Industry

Project Reference: We have supplied high-quality 26NiCrMoV11-5 forged parts for marine power systems used in global shipbuilding projects across Germany, South Korea, Japan and China. All key marine parts meet strict rules from major marine certification bodies, including DNV, GL, ABS, LR, BV and RINA.

Products Manufactured: Propeller shafts, crankshafts, gear shafts, marine turbine parts, rudder stocks and marine propulsion system parts

Heavy Machinery & Industrial Equipment

Project Reference:  We have provided large amounts of 1.6948 forged shafts, gears and rotating parts for industrial compressors, mining gear and construction machinery working in Australia, Brazil, the United States, Canada and Chile. These heavy-duty parts run steadily under heavy loads and tough working conditions.

Products Manufactured: Compressor rotors, gear shafts, heavy-duty axles, crusher parts, rolling mill parts and structural parts

Quality Assurance & Certification

At Jiangsu Liangyi, uncompromising quality is embedded in every single stage of our production process. All our 26NiCrMoV11-5 (1.6948) forged parts are given rigorous and full quality control procedures from initial raw material inspection through to final testing, protective coating and secure packaging.

Comprehensive Quality Control Process

  • Raw material chemical composition analysis using spectrometry
  • 100% ultrasonic testing (UT) per ASTM A388 and EN 10228 standards
  • Magnetic particle testing (MT) and liquid penetrant testing (PT)
  • Full mechanical property testing (tensile, impact, hardness)
  • Metallographic examination and grain size analysis
  • High-temperature mechanical testing (when specified by client)
  • Dimension test and precision machining verification
  • Final visual inspection and surface quality assessment

Our Certification

Jiangsu Liangyi holds the following quality management certification:

  • ISO 9001:2015 — Quality Management System certification, covering design, manufacturing, inspection and delivery of open die forgings and seamless rolled rings

Material Test Certificate Types We Issue

For every shipment of 26NiCrMoV11-5 forged parts, we issue material test certificates documenting full traceability of chemical composition, heat treatment records and mechanical test results:

  • EN 10204-3.1 — Manufacturer's Inspection Certificate (standard): Issued and signed by our own authorized quality representative. Included as standard with all orders. Covers chemical analysis, mechanical properties, heat treatment records and dimensional data.
  • EN 10204-3.2 — Third-Party Witnessed Inspection Certificate (on request): Outside third-party inspectors watch all testing work at our factory and sign material papers together with our in-house quality staff. We fully support third-party checks and make the whole process easy for buyers. Customers can choose their own inspection company, and we will fully arrange site access, testing times and on-site witness work.

Third-Party Inspection — How It Works

We regularly cooperate with independent inspection groups chosen by our customers. These teams visit our factory to watch all material tests and issue their own inspection reports. Well‑known groups that have completed on-site checks at our Jiangyin site include TÜV, Bureau Veritas (BV), DNV, ABS, Lloyd's Register (LR) and RINA. It should be noted that we offer third-party inspection support as a customer service, and we do not hold standalone certification from these organizations. If your contract or project rules need a certain inspection provider, please tell us when you send your inquiry, and we will check and confirm available scheduling.

Important note for procurement teams: If your project specification needs a named classification society or inspection body (such as DNV, BV, ABS or LR), please specify this clearly in your purchase order. We will confirm availability and coordinate the inspection visit. Any costs associated with third-party inspection agency fees are typically for the buyer's account unless otherwise agreed in the commercial terms.

Delivery & Global Logistics

 As a top maker of 26NiCrMoV11-5 forged parts based in Jiangyin, China, we have built fast and stable global shipping routes. This lets us deliver our high-quality forged goods to customers around the world on time and with full reliability.

  • Standard production lead time: 4-8 weeks for standard products, 8-12 weeks for custom engineered parts
  • Expedited delivery service: Available upon request for urgent customer orders
  • Professional export packaging: Standard seaworthy export packaging with full rust prevention and shock protection
  • Convenient shipping ports: Shanghai, Ningbo, Qingdao and other major Chinese international ports
  • Flexible shipping methods: Sea freight, air freight and land transportation options
  • Door-to-door delivery service: Available to most countries worldwide
  • Export documentation: Complete set of export documents including commercial invoice, packing list, bill of lading, certificate of origin, etc.

We partner exclusively with leading international logistics companies to make sure that your valuable 26NiCrMoV11-5 forged parts arrive safely, securely and on schedule, no matter where you are located globally.

Frequently Asked Questions About 26NiCrMoV11-5 Forgings

 26NiCrMoV11-5 (1.6948) steel is mainly used to make key working parts that need high strength, strong toughness and good heat resistance. Common uses include gas and steam turbine rotor shafts, valve stems, gears, crankshafts and heavy-load shafts. These parts serve the power generation, oil and gas, marine and heavy machinery fields, where stable performance is the top priority.

Though both are high-grade alloy steels for turbine use, 26NiCrMoV11-5 has much higher nickel content at 2.40–3.10%, compared to 0.80–1.50%. So  that it has better overall toughness and improved performance at low temperatures. By contrast, 30CrMoNiV5-11 (1.6946)  contains more chromium and carbon, so that it has slightly stronger mechanical strength under high-temperature working conditions. The best material choice depends entirely on how you plan to use it and the conditions at the site.

 Surely. We focus on custom open die forgings made to your exact needs. We can make 26NiCrMoV11-5 parts in nearly any shape and size, following your technical drawings, CAD files and technical rules. Our skilled engineering team will cooperate with you from design to production, to make sure the final finished part fully meets or exceeds your actual demands.

We provide EN 10204-3.1 material test certificates as standard for every shipment. These documents are signed by our official quality staff, and include full chemical makeup, mechanical test data and heat treatment records. For projects needing outside check, we offer EN 10204-3.2 witnessed inspection service. A third-party inspector chosen by you will come to our factory, watch all tests, and sign the test papers together with our team. We allow full site access for common inspection groups such as TÜV, BV, DNV, ABS and LR. Please state your needed inspection group when you send an inquiry, so we can check time plans and make proper arrangements.

We can make single 26NiCrMoV11-5 forgings with a maximum weight of 30 tons, solid shafts up to 15 meters long and 2 meters in diameter. For seamless rolled rings, we produce these parts with an outer diameter as large as 6 meters. If you need sizes beyond these limits, reach out to our engineering team to talk through production feasibility.

 EN 10204-3.1 is a factory inspection document, confirmed and signed by our qualified quality staff to prove the material meets all stated needs. This certificate is issued by quality engineers at Jiangsu Liangyi, and works well for most common commercial and industrial purchase orders. It covers complete chemical makeup, mechanical test data, heat treatment logs and full size checks for every part.

EN 10204-3.2  is a higher-grade document that needs an independent third-party inspector chosen by the customer. This inspector visits our factory, watches all real material tests, and signs the certificate together with our quality staff. We fully support and arrange all on-site work for this process. The buyer books and pays for the third-party inspector, while we handle site entry and time planning. We suggest choosing 3.2 paperwork for 26NiCrMoV11-5 turbine rotor shafts used in grid power plants over 100 MW. It is important to know that Jiangsu Liangyi keeps ISO 9001:2015 approval. EN 10204-3.2 is just a standard document form, not a company certification owned by us or inspection groups.

This is a great technical question that shows the well‑thought‑out design of this alloy. Silicon strongly helps form ferrite, and it also makes steel more likely to face reversible temper embrittlement (RTE), also called 475°C brittleness. This issue is extra common in steel that contains nickel. For alloys such as 26NiCrMoV11-5 with 2.40–3.10% nickel, high nickel levels paired with silicon work together to cause brittleness. When the material cools slowly between 375–575°C, harmful impurities like phosphorus and tin gather along old grain lines and weaken the steel structure. This alloy limits silicon to no more than 0.15%, much lower than the 0.40% to 0.60% seen in regular structural steel. This strict rule greatly cuts down grain boundary brittleness risks. The grade also keeps phosphorus below 0.015% and sulfur below 0.010%. These trace harmful elements are the main cause of brittleness, and silicon speeds up their buildup on grain lines. With these tight controls, the finished steel keeps strong toughness for many years at working temperatures of 450–550°C, even after repeated heating and cooling cycles from frequent start and stop use.


Contact Us for 26NiCrMoV11-5 Forging Quotation

Jiangsu Liangyi Co., Limited is your trusted global partner for high-quality 26NiCrMoV11-5 (1.6948) forging parts. As an experienced direct manufacturer strategically located in Jiangyin, Jiangsu Province, China, we offer highly competitive pricing, fast delivery times and comprehensive customized solutions to meet your most demanding project requirements.

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Please send us your custom engineering drawings, material specifications, quantity requirements and any special technical requirements for a detailed, competitive quotation. Our experienced technical and sales team will respond to your inquiry within 24 hours.

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