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1.4534 (X3CrNiMoAl13-8-2) Forged Parts | China Jiangsu Manufacturer

ⓘ Key Facts: 1.4534 / X3CrNiMoAl13-8-2 at a Glance

EN Material Number 1.4534
EN Short Name X3CrNiMoAl13-8-2
UNS Equivalent S13800 (13-8 Mo PH)
AMS Specifications AMS 5629 / AMS 5864
Steel Type Precipitation Hardening Martensitic Stainless Steel
Standard EN 10088-3
Max Yield Strength (H950) 1,413 MPa (205,000 psi)
Max Operating Temp. 593 °C (1,100 °F)
Manufacturer Jiangsu Liangyi Co., Limited
Factory Location Jiangyin, Jiangsu, China
Certification ISO 9001:2015
Single-Piece Max Weight 30,000 kg

Introduction to 1.4534 (X3CrNiMoAl13-8-2) Steel

, located in Chengchang Industry Park, Jiangyin City, Jiangsu Province, China, is a professional ISO 9001:2015 certified manufacturer of 1.4534 (X3CrNiMoAl13-8-2) open die forging parts and seamless rolled steel forged rings. Also known as X 3 CrNiMoAl 13-8-2, X3CrNiMoAl1382, X3CrNiMoAl13.8.2, UNS S13800, and commonly referred to as 13-8 Mo PH stainless steel, this material is an acid-resistant special steel with a martensitic structure that undergoes precipitation hardening. It exhibits excellent mechanical properties including high hardness, exceptional strength, and relatively high corrosion resistance, making it ideal for components subjected to dynamic loads and cracking resistance.

Compared to other high-alloyed corrosion-resistant grades, 1.4534 steel has much stricter limits on sulfur and phosphorus content in its chemical composition (P ≤ 0.01%, S ≤ 0.008%). This results in a more challenging manufacturing process but ensures exceptionally high purity and quality of the final product. As a leading 1.4534 China manufacturer, Jiangsu Liangyi has mastered the complex production techniques required to deliver consistent, high-quality X3CrNiMoAl13-8-2 forgings to customers worldwide from our advanced facility in Jiangyin, Jiangsu.

Available 1.4534 (X3CrNiMoAl13-8-2) Forged Products

As a premier X3CrNiMoAl13-8-2 Jiangsu supplier, Jiangsu Liangyi manufactures a comprehensive range of 1.4534 (X3CrNiMoAl13-8-2) forging steel products in various shapes and sizes, from 30 kg to 30,000 kg single-piece weight:

1.4534 X3CrNiMoAl13-8-2 forged round bars manufactured in Jiangyin China
Figure 1: High-quality 1.4534 (X3CrNiMoAl13-8-2) forged round bars produced at our Jiangyin factory

Forged Bars & Rods

  • Round bars (up to 2000 mm diameter), square bars, flat bars, and rectangular bars
  • Custom diameters and lengths up to 15 meters to meet your specifications
  • Available in all standard and custom sizes with EN 10204 3.1 mill test certificates as standard; 3.2 (third-party witnessed) available upon request
  • Precision machined to tight tolerances for immediate use in your production

Seamless Rolled Rings

  • Seamless rolled rings and open die forged rings up to 6 meters in diameter
  • Ideal for critical rotating and pressure applications in power generation and oil & gas
  • Large diameter capabilities up to industry standards with uniform grain structure
  • Produced on our advanced 1-meter and 5-meter seamless rolling machines in Jiangyin, China

Hollow Forgings & Sleeves

  • Hubs, housings, shells, sleeves, and bushes up to 3000 mm outer diameter
  • Hollow bars and casing components with heavy wall thickness options
  • Precision-machined to tight tolerances for hydraulic and pressure vessel applications
  • Manufactured using advanced open die forging techniques at our Jiangsu factory

Discs, Plates & Blocks

  • Forged discs, disks, blocks, and plates up to 3000 mm in diameter
  • Uniform material structure for enhanced performance under high pressure
  • Suitable for turbine discs, valve bodies, and pressure vessel components
  • Produced using our 2000T, 4000T, and 6300T hydraulic forging presses

Pipes & Tubes

  • Forged steel pipes, tubes, tubings, and piping for high-pressure applications
  • Shells, casings, case barrels, and housings for nuclear and petrochemical industries
  • Designed to withstand extreme temperatures and corrosive environments
  • Manufactured in accordance with international standards including ASTM, EN, and DIN; fully tested and documented per applicable standard requirements

Chemical Composition of 1.4534 (X3CrNiMoAl13-8-2)

The precise chemical composition of 1.4534 (X3CrNiMoAl13-8-2) forged steel ensures its superior mechanical properties and corrosion resistance. At our Jiangyin 1.4534 factory, we strictly control every element to meet EN 10088-3 standards:

Table 1: Chemical Composition of 1.4534 (X3CrNiMoAl13-8-2) per EN 10088-3
ElementContent (%)Standard Requirement
Carbon (C)max. 0.05EN 10088-3
Chromium (Cr)12.25 – 13.25EN 10088-3
Manganese (Mn)max. 0.1EN 10088-3
Molybdenum (Mo)2.0 – 2.5EN 10088-3
Nickel (Ni)7.5 – 8.5EN 10088-3
Phosphorus (P)max. 0.01EN 10088-3
Sulfur (S)max. 0.008EN 10088-3
Silicon (Si)max. 0.1EN 10088-3
Titanium (Ti)max. 0.1EN 10088-3
Nitrogen (N)max. 0.01EN 10088-3
Aluminum (Al)0.8 – 1.35EN 10088-3

International Standard Equivalents for 1.4534 Steel

The steel grade 1.4534 is designated under multiple international standards. The table below lists the most widely used equivalent designations to help engineers and procurement specialists specify the correct material globally:

Table 2: International Equivalents of 1.4534 (X3CrNiMoAl13-8-2) Precipitation Hardening Steel
Standard SystemDesignationSpecification / Norm
European (EN)1.4534 / X3CrNiMoAl13-8-2EN 10088-3
UNS (USA)S13800ASTM A564 / ASTM A693
Common Trade Name13-8 Mo PH / Custom 13-8 Mo
AMS (USA)AMS 5629 (Bar, Wire, Forgings, Rings)AMS 5629
AMS (USA)AMS 5864 (Bar, Ring, Forgings)AMS 5864
MIL-SPEC (USA)MIL-S-81591
Japanese (JIS)SUS XM-13 (similar)JIS G4303

Note: While these designations refer to essentially the same alloy system, minor compositional differences may exist between standards. Always verify against the specific standard applicable to your project. As an ISO 9001:2015 certified forging manufacturer with 25+ years of experience, Jiangsu Liangyi is capable of manufacturing to any of the above specifications upon request.

Mechanical Properties of 1.4534 (X3CrNiMoAl13-8-2)

1.4534 (X3CrNiMoAl13-8-2) exhibits excellent mechanical properties at room temperature, with different heat treatment conditions providing varying strength and toughness combinations. All our X3CrNiMoAl13-8-2 forgings are tested in our in-house mechanical testing laboratory in Jiangsu, China:

Table 3: Mechanical Properties of 1.4534 (X3CrNiMoAl13-8-2) by Heat Treatment Condition
ConditionMin. Yield StrengthMin. Tensile StrengthMin. ElongationHardness
H9501,413 MPa (205,000 psi)1,517 MPa (220,000 psi)10%44–48 HRC
H10001,310 MPa (190,000 psi)1,413 MPa (205,000 psi)10%42–46 HRC
H10501,138 MPa (165,000 psi)1,207 MPa (175,000 psi)12%39–43 HRC

High Temperature Performance

 1.4534 (X3CrNiMoAl13-8-2) stainless steel has excellent oxidation resistance up to approximately 1100 °F (593 °C). However, prolonged exposure in the temperature range of 600–900 °F (288–482 °C) may cause toughness degradation in this precipitation-hardening stainless steel. In some cases, this loss of toughness can be minimized by applying higher aging temperatures. Short-term exposure to elevated temperatures is permissible, provided the peak temperature is at least 50 °F (28 °C) below the aging temperature. As an experienced manufacturer of 1.4534 turbine forgings  in China, we can provide tailored heat treatment solutions to optimize your parts for specific high-temperature applications.

Corrosion Resistance

In aggressive environments (excluding moisture resistance), 1.4534 (X3CrNiMoAl13-8-2) exhibits very good resistance to:

  • Sodium Chloride (NaCl) solutions (up to 10% concentration)
  • Nitric Acid (up to 65% concentration at room temperature)
  • Sodium Hydroxide (up to 50% concentration at room temperature)

This makes it the best choice material for parts operating in corrosive industrial environments, particularly in the petrochemical, marine, and nuclear industries. Our X3CrNiMoAl13-8-2 valve parts are widely used in sour service applications where corrosion resistance is important.

Physical Properties of 1.4534 (X3CrNiMoAl13-8-2)

Beyond mechanical strength, the physical and thermal properties of 1.4534 (X3CrNiMoAl13-8-2) directly determine its suitability for precision part design. Values below apply to the alloy in the solution‑annealed condition at room temperature (21 °C / 70 °F) unless otherwise specified. These data align with typical values from EN 10088‑3 and recognized metallurgical references for this alloy group, and have been verified against Jiangsu Liangyi’s internal material test records.

Table 4: Physical Properties of 1.4534 (X3CrNiMoAl13-8-2) — Solution-Annealed Condition
PropertyValueUnitCondition / Notes
Density7.78g/cm³ (0.281 lb/in³)Room temperature
Elastic Modulus (Young's Modulus)197GPa (28.6 × 10⁶ psi)Room temperature
Shear Modulus76GPa (11.0 × 10⁶ psi)Room temperature
Poisson's Ratio0.30Room temperature
Thermal Conductivity14.0W/(m·K)21 °C (70 °F)
Thermal Conductivity17.8W/(m·K)538 °C (1,000 °F)
Mean Thermal Expansion Coefficient10.6 × 10⁻⁶/°C (/°F: 5.9 × 10⁻⁶)0 – 260 °C (32–500 °F)
Mean Thermal Expansion Coefficient11.2 × 10⁻⁶/°C (/°F: 6.2 × 10⁻⁶)0 – 538 °C (32–1,000 °F)
Specific Heat Capacity460J/(kg·K)Room temperature
Electrical Resistivity0.80µΩ·m21 °C (70 °F)
Magnetic Permeability> 1 (ferromagnetic)Annealed condition; becomes more ferromagnetic after aging
Melting Range1,400 – 1,440°C (2,552–2,624 °F)Approximate solidus–liquidus range

Design note on thermal expansion: A notable advantage of 1.4534 (X3CrNiMoAl13-8-2)  is its relatively low coefficient of thermal expansion, measuring 10.6 × 10⁻⁶/°C at moderate temperatures, compared to austenitic stainless steels like 316L at approximately 16 × 10⁻⁶/°C. In assemblies combining 1.4534 with carbon steel or titanium parts, this closer thermal expansion match greatly reduces differential thermal stress under cyclic operating conditions.This is a main reason the alloy is the best choice material for aerospace and nuclear turbine applications.

Heat Treatment of 1.4534 (X3CrNiMoAl13-8-2): Complete Process Guide

The excellent performance of 1.4534 (X3CrNiMoAl13-8-2) relies entirely on a precisely controlled, multi‑stage heat treatment process.Unlike conventional quench‑and‑temper steels, this alloy attains its final properties via a two‑step thermal cycle: first, solution annealing to form a homogeneous martensitic matrix,followed by age hardening (precipitation hardening) to precipitate fine intermetallic strengthening phases. At Jiangsu Liangyi’s Jiangyin plant, all heat treatment is carried out in computer‑controlled gas‑fired or electric resistance furnaces with continuous temperature monitoring.Complete thermal cycle records are included in the material certification documents.

Step 1 — Solution Annealing (Conditioning Treatment)

Solution annealing dissolves all carbides, secondary phases and existing precipitates, restoring a uniform, low‑hardness martensitic structure that is ideal for machining, forming or welding before final aging.

  • Temperature: 927 °C ± 14 °C (1,700 °F ± 25 °F)
  • Soak time: Sufficient to uniformly heat the entire cross-section — typically 30 minutes minimum plus 1 hour per 25 mm of maximum cross-section thickness
  • Cooling: Air cool or accelerated cool (fan-assisted air or water quench for heavy sections) to below 32 °C (90 °F). Rapid cooling through the martensite transformation range (approximately 120 °C / 250 °F to room temperature) is important to guarantee complete conversion of the austenite to martensite before aging begins
  • Result: Hardness typically 28–34 HRC in the solution-annealed condition — ideal for machining large forged blanks before final aging

Step 1A — Optional Sub-Zero Treatment (Cryogenic Conditioning)

For demanding aerospace and nuclear applications, Jiangsu Liangyi can apply an optional cryogenic sub-zero treatment between solution annealing and aging:

  • Temperature: −73 °C (−100 °F) or colder, typically in liquid nitrogen
  • Hold time: Minimum 8 hours
  • Purpose: Drives retained austenite content to near-zero by completing the martensite transformation; improves dimensional stability and fatigue life in critical rotating parts
  • Note: Parts must return to room temperature before aging

Step 2 — Aging (Precipitation Hardening)

Aging precipitates fine NiAl (β‑NiAl) and Ni₃Al intermetallic particles within the martensitic matrix, creating the pronounced strengthening effect typical of this alloy family.The selected aging temperature directly controls the final balance between strength and toughness:

Table 5: Aging Conditions for 1.4534 (X3CrNiMoAl13-8-2) — Full H-Condition Specification
ConditionAging Temp.Hold TimeCoolingTypical HardnessCharacteristics
H950510 °C (950 °F)4 hAir cool44–48 HRCMaximum strength; lowest toughness; best for static high-load applications
H1000538 °C (1,000 °F)4 hAir cool42–46 HRCHigh strength with improved impact toughness; widely used for aerospace structural parts
H1025552 °C (1,025 °F)4 hAir cool40–45 HRCIntermediate condition; good balance for valve bodies and pump shafts
H1050566 °C (1,050 °F)4 hAir cool39–43 HRCOptimum toughness-to-strength ratio; preferred for dynamic and impact-loaded parts
H1100593 °C (1,100 °F)4 hAir cool35–40 HRCBest toughness; suitable for components requiring maximum impact resistance
H1150621 °C (1,150 °F)4 hAir cool31–36 HRCBest corrosion resistance in the aged family; used post-welding to restore properties

Critical process control note:The aging soak time shall be calculated only when the entire cross‑section of the forging reaches the target temperature, not when the furnace itself reaches temperature. For large cross‑section 1.4534 forgings such as rings with wall thickness exceeding 500 mm, Jiangsu Liangyi employs calibrated thermocouples embedded in the heaviest section to record the actual metal temperature, guaranteeing full compliance with soaking requirements.This method prevents under‑aging in the core, a failure mode that can reduce core toughness by up to 30% relative to surface properties in heavy forgings.

Industrial Applications of 1.4534 (X3CrNiMoAl13-8-2) Forgings

1.4534 (X3CrNiMoAl13-8-2) is widely used for the aerospace, nuclear, and petrochemical industries for parts subject to corrosion and heavy loads. Additional applications include medical technology, high-pressure pumps, valves, and high-strength bolts. As a leading 1.4534 China manufacturer, we have supplied parts for many important projects in over 50 countries worldwide from our Jiangyin production facility.

Aerospace Industry Applications

  • Gas compressor and turbine blades for commercial and military aircraft
  • Turbine disks, impellers, and blisks for jet engines
  • Aircraft structural components requiring high strength-to-weight ratio
  • Landing gear parts and hydraulic system parts
  • Engine parts needing high strength and corrosion resistance

Power Generation Industry Applications

  • Gas and steam turbine parts for thermal and nuclear power plants
  • Turbine guide rings, seal rings, and labyrinth rings
  • Packing seal diaphragms and rotor end rings
  • Contours and casing rings for turbine assemblies
  • Nuclear power reactor coolant pump parts including rotors, impellers, and casings
  • Nuclear reactor containment seal chambers and pressure vessel parts

Oil & Gas and Petrochemical Industry Applications

  • High-pressure valves including balls, bonnets, bodies, stems, closures, seat rings, cores, and discs
  • H-type two-way and one-way back pressure valves, ball valves, check valves, and gate pumps
  • Ultra-high pressure water jet cutting machine parts for offshore platforms
  • Hydraulic cylinders, accumulators, and attenuators for subsea applications
  • Intensifier pump sealing heads and high-pressure piping parts
  • Boiler and heat exchanger parts including tube sheets, nozzles, and channel flanges
  • Pressure vessels, reactors, and heaters for chemical processing plants

Marine Industry Applications

  • Ship and boat propeller shafts for commercial and naval vessels
  • Marine engine parts and propulsion system parts
  • Offshore platform equipment and subsea valve parts
  • Marine hydraulic system parts needing corrosion resistance

Downhole Drilling Applications

  • Mud motor splined drive shafts for oil and gas exploration
  • Downhole electric submersible pump (ESP) motor splined shafts
  • Integral mud flanges, flanged outlets, and studded crosses for wellhead assemblies
  • Drill string parts and downhole tooling

General Industrial Applications

  • Injection molding parts, molds, and die blocks for plastic manufacturing
  • Tooling and fixtures for high-precision machining operations
  • Turbomachinery and turbo centrifugal compressor impellers
  • Compressor shrouded impellers and rotor parts
  • Pump parts including casings, covers, barrels, impellers, shafts, housings, shells, bodies, and wear rings

1.4534 vs Other Precipitation Hardening Stainless Steels: Grade Selection Guide

 Engineers specifying precipitation-hardening stainless steels for new projects often need to compare  1.4534 (X3CrNiMoAl13-8-2 / S13800) with three closely related grades: 17-4PH (1.4542 / S17400), 15-5PH (1.4545 / S15500), and 17-7PH (1.4568 / S17700).The table below summarizes main compositional and performance differences to support material choice.All comparative data represents typical room-temperature properties of forged products.

Table 6: 1.4534 vs 17-4PH / 15-5PH / 17-7PH — Precipitation Hardening Grade Comparison
Property / Parameter1.4534 (S13800) ★17-4PH (S17400 / 1.4542)15-5PH (S15500 / 1.4545)17-7PH (S17700 / 1.4568)
Steel FamilyMartensitic PHMartensitic PHMartensitic PHSemi-austenitic PH
Chromium (Cr)12.25–13.25%15.0–17.5%14.0–15.5%16.0–18.0%
Nickel (Ni)7.5–8.5%3.0–5.0%3.5–5.5%6.5–7.75%
Hardening AgentMolybdenum + Aluminum (2.0–2.5% Mo; 0.8–1.35% Al)Copper (3.0–5.0% Cu)Copper (2.5–4.5% Cu)Aluminum (0.75–1.5% Al)
Max Yield Strength (highest H-cond.)1,413 MPa (H950)1,172 MPa (H900)1,172 MPa (H900)1,241 MPa (RH950)
Toughness (impact) vs 17-4PHHigher — improved Ni content and Mo addition reduce delta-ferrite, increasing fracture toughness by ~20–35% at comparable strength levelsBaseline referenceSimilar to 17-4PHHigher in austenitic range; lower after hardening
Corrosion Resistance in Cl⁻ EnvironmentsSuperior — Mo addition (2–2.5%) significantly improves pitting resistance; better than 17-4PH and 15-5PH in chloride-containing mediaGoodGood (slightly better than 17-4PH in some media due to lower Co)Good in austenitic condition; reduces after hardening
Pitting Resistance Equivalent (PRE = Cr + 3.3Mo)~19.5 (12.75Cr + 3.3×2.25Mo)~16.3 (16.3Cr; no Mo)~14.8 (14.8Cr; no Mo)~17.0 (17.0Cr; no Mo)
WeldabilityGood — lower delta-ferrite content than 17-4PH reduces hot cracking tendencyModerate — delta-ferrite in weld can cause toughness issuesModerate — similar to 17-4PHComplex — requires strict process control
Max Continuous Service Temp.~316 °C (600 °F) in H1000/H1050~315 °C (600 °F) in H1025~315 °C (600 °F)~315 °C (600 °F)
Typical ApplicationsNuclear, aerospace turbines, downhole drilling, high-pressure valves in sour serviceGeneral aerospace, oil & gas, food processing equipmentAerospace forgings, nuclear, marine (lower delta-ferrite than 17-4PH)Springs, diaphragms, flat-rolled strip applications
Relative Price LevelHigher (Mo + strict P/S limits)Reference (most common)Similar to 17-4PHSlightly higher

When to Choose 1.4534 Over 17-4PH

Based on Jiangsu Liangyi's 25+ years of forging experience across these four grades, the engineering scenarios where 1.4534 (X3CrNiMoAl13-8-2) should be specified over 17-4PH (1.4542) are:

  • Chloride or sour-service environments: The 2–2.5% molybdenum content gives 1.4534 a pitting resistance equivalent (PRE) of ~19.5 versus ~16.3 for 17-4PH, so that  it is the best choice material for subsea valves, downhole drilling tools, and marine shaft applications where chloride-induced pitting is the primary failure mode.
  • High-fracture-toughness requirements: The higher nickel content (7.5–8.5% vs 3–5%) and near-zero delta-ferrite structure of 1.4534 provide measurably superior Charpy impact values at equivalent strength levels — critical for parts subject to shock loading or low-temperature service.
  • Nuclear applications with strict impurity limits: The tighter P ≤ 0.01% and S ≤ 0.008% limits in EN 10088-3 for 1.4534 meet nuclear quality requirements that 17-4PH typically cannot satisfy without special melting practice.
  • Weldable assemblies at high strength: The lower delta-ferrite content in 1.4534 welds reduces hot cracking susceptibility, so that it is easier to achieve sound, high-toughness weld joints in thick-section assemblies.

Weldability and Machinability of 1.4534 (X3CrNiMoAl13-8-2)

Welding 1.4534 (X3CrNiMoAl13-8-2)

1.4534 (X3CrNiMoAl13-8-2) is regarded as weldable using conventional fusion welding processes.However, due to its precipitation-hardening characteristics, strict control over pre-weld preparation, in-process parameters and post-weld procedures is required to maintain the alloy’s outstanding mechanical properties in the heat-affected zone (HAZ).The guidelines below are based on Jiangsu Liangyi’s internal welding procedure specifications (WPS) qualified for repair and assembly welding of 1.4534 forged parts.

Recommended Welding Processes

  • GTAW (TIG / Gas Tungsten Arc Welding): Preferred process for precision joints and thin sections. Provides the best arc control, lowest heat input, and cleanest weld pool — essential for keeping corrosion resistance. Use pure argon shielding gas (99.999%) at 10–15 L/min.
  • GMAW (MIG / Gas Metal Arc Welding): Acceptable for larger section fillets and build-up applications. Use pulse-spray transfer mode to minimise heat input. Argon + 2% O₂ or Ar + 2% CO₂ shielding blend.
  • PAW (Plasma Arc Welding): Used for precision keyhole welding of pipe and ring butt joints where full penetration is needed without a backing bar.
  • Electron Beam Welding (EBW) & Laser Beam Welding (LBW): Best choice for highly controlled, low-distortion welds in aerospace parts where the narrowest possible HAZ is needed.

Filler Metal Selection

  • Matching filler (preferred): ER13-8Mo (AWS A5.9 classification) — produces welds with near-matching composition and allows post-weld precipitation hardening to achieve ≥85% of base metal strength.
  • Dissimilar joints: For joints to carbon steel or low-alloy steel, ER309L or ER309LMo austenitic filler may be used as a buffer layer; a final capping pass with ER13-8Mo is recommended where corrosion resistance is important.
  • For sour-service welds (NACE MR0175 compliance): Filler hardness must not exceed 22 HRC (≈248 HV10) in the as-welded condition. In this case, H1150 post-weld heat treatment is mandatory to bring weld metal hardness into compliance.

Pre-Heat and Inter-Pass Temperature

  • For sections up to 25 mm thickness: Pre-heat not required, but parts should be at ≥ 10 °C (50 °F) to prevent moisture condensation
  • For sections 25–75 mm: Pre-heat to 65–93 °C (150–200 °F)
  • For sections > 75 mm: Pre-heat to 93–150 °C (200–300 °F)
  • Maximum inter-pass temperature: 150 °C (300 °F) — exceeding this causes excessive softening of the adjacent aged base metal

Post-Weld Heat Treatment (PWHT)

After welding 1.4534 parts, a full post-weld heat treatment is strongly recommended for structural and pressure-retaining applications:

  • Full re-solution + re-age: Solution anneal at 927 °C followed by aging to H950–H1050 — restores full base metal properties in both weld metal and HAZ. This is the preferred PWHT for critical aerospace and nuclear parts.
  • Age-only PWHT (H1150 condition): For situations where re-solution is impractical (e.g., large assemblies), aging at 621 °C (1,150 °F) for 4 hours will recover a significant portion of weld zone properties and guarantees NACE-compliant hardness levels. This option sacrifices some strength but is widely accepted for oil & gas valve assemblies.

Machinability of 1.4534 (X3CrNiMoAl13-8-2)

 1.4534 (X3CrNiMoAl13-8-2) is a low‑carbon martensitic alloy, not an austenitic grade, so it does not show the severe work‑hardening behavior of 304 or 316L.Even so, its high hardness in the aged condition and molybdenum‑enhanced strength make tool selection and cutting parameter optimization important. The guidance below is based on Jiangsu Liangyi’s practical experience in rough and finish machining large forged blanks.

Machinability Rating and Comparison

  • Relative machinability (solution-annealed): about 45% of AISI 303 free-machining stainless (used as 100% reference)
  • Relative machinability (aged H950–H1050): about 25–35% of AISI 303 — significantly harder to machine but still achievable with correct tooling
  • Preferred machining sequence: perform all major material removal in the solution-annealed condition, then age to final hardness, then perform only finish machining passes to final dimensions

Cutting Tool and Parameter Recommendations

  • Tool material: Uncoated or TiAlN-coated submicron carbide grade (ISO M20–M30) for turning; CBN inserts for hard turning aged condition above 45 HRC
  • Cutting speed (turning, annealed): 60–100 m/min; aged condition: 30–60 m/min
  • Feed rate: 0.10–0.25 mm/rev for roughing; 0.05–0.12 mm/rev for finishing
  • Depth of cut: Roughing up to 4 mm; finishing 0.25–0.5 mm
  • Coolant: Flood coolant (soluble oil at 8–10% concentration) is mandatory — dry cutting causes rapid tool wear and surface work hardening
  • Surface finish achievable: Ra 0.8 µm with carbide tools; Ra 0.4 µm or better with CBN inserts in aged condition — meets shaft sealing surface requirements without grinding
  • Key caution: Avoid rubbing passes or insufficient feed rates — these cause surface work hardening that dramatically reduces tool life on subsequent cuts

Quality Forging Process at Our Jiangyin, China Factory

 Jiangsu Liangyi applies a strict quality control system throughout the full manufacturing cycle of 1.4534 (X3CrNiMoAl13-8-2) forgings at our 80,000 ㎡ production base in Chengchang Industrial Park, Jiangyin, Jiangsu Province, China.

X3CrNiMoAl13-8-2 seamless rolled forged rings from Jiangsu Liangyi
Figure 2: Precision X3CrNiMoAl13-8-2 seamless rolled forged rings manufactured in Jiangsu
  1. Raw Material Inspection: Steel ingot received into warehouse with chemical content testing using our in-house spectrometer
  2. Cutting: Precision cutting to required dimensions using advanced sawing equipment
  3. Forging Process: Controlled open die forging using our 2000T, 4000T, and 6300T hydraulic presses
  4. Post Forging Heat Treatment: Normalizing and tempering (N+T) in our computer-controlled heat treatment furnaces
  5. Ultrasonic Testing (UT): First round of non-destructive testing per ASTM A388 standards
  6. Rough Machining: Initial machining to near-final dimensions using CNC equipment
  7. Second Ultrasonic Testing (UT): Additional quality verification to detect any internal defects
  8. Quenching and Tempering (QT): Final heat treatment for improved mechanical properties
  9. Comprehensive Inspection: UT, mechanical properties testing, hardness testing, and grain size analysis
  10. Grooving: Precision grooving as required by customer drawings
  11. Stress Relieve Tempering: To relieve residual stresses from machining operations
  12. Machining Holding Positions: For rotor parts during high-speed testing (HST)
  13. High-Speed Testing (HST): For rotating parts to guarantee dynamic balance
  14. Final Dimensional Inspection: Verification of all critical dimensions using CMM equipment
  15. Packing and Marking: Steel stamping and proper marking for identification and traceability
  16. Storage and Shipment: Careful handling and timely delivery to customers worldwide

Why Choose Jiangsu Liangyi as Your 1.4534 Forging Partner in China?

  • 25+ Years of Experience: Established in 1997, we have a lot of experience of producing high-quality 1.4534 forged parts
  • ISO 9001:2015 Certified: Our quality management system guarantees consistent product quality meeting international standards
  • Advanced Equipment: We operate state-of-the-art forging, machining, and testing equipment at our Jiangyin factory
  • Comprehensive Testing: In-house chemical analysis, mechanical testing, metallography, and non-destructive testing facilities
  • Custom Solutions: We make custom parts according to your drawings and technical specifications
  • Global Delivery: We supply to customers in over 50 countries worldwide with reliable shipping options
  • Complete Traceability: All products come with EN 10204 Type 3.1 mill test certificates as standard; EN 10204 3.2 (third-party witnessed) available upon request
  • Competitive Pricing: As a direct X3CrNiMoAl13-8-2 China manufacturer, we offer competitive prices without compromising quality
  • Fast Lead Times: Our efficient production process allows us to meet tight delivery schedules
  • Technical Support: Our experienced engineering team provides technical support throughout the entire project

Frequently Asked Questions (FAQ)

Q: What is 1.4534 (X3CrNiMoAl13-8-2) steel?
A: 1.4534 (X3CrNiMoAl13-8-2) is a precipitation hardening martensitic stainless steel with excellent mechanical properties and corrosion resistance. Designated as UNS S13800 and commonly known as 13-8 Mo PH stainless steel, it is widely used in aerospace, nuclear, and petrochemical applications where high strength and corrosion resistance are required simultaneously.
Q: What is the UNS equivalent of 1.4534 (X3CrNiMoAl13-8-2)?
A: The UNS equivalent of 1.4534 (X3CrNiMoAl13-8-2) is UNS S13800, also widely known as 13-8 Mo PH stainless steel or Custom 13-8 Mo. The relevant AMS specifications are AMS 5629 and AMS 5864. These designations refer to essentially the same precipitation hardening martensitic stainless steel alloy system.
Q: What are the main advantages of 1.4534 steel?
A: 1.4534 (X3CrNiMoAl13-8-2) has a lot of good qualities, such as very high yield strength (up to 1,413 MPa in H950 condition), good corrosion resistance, excellent toughness, oxidation resistance up to 593 °C (1,100 °F), and good weldability compared to other high-strength steels.  it has very little sulfur (≤0.008%) and phosphorus (≤0.01%), so that it is also a very pure material that can withstand a lot of stress.
Q: What is the difference between H950, H1000, and H1050 heat treatment conditions?
A: H950, H1000, and H1050 are different temperatures used for aging (precipitation hardening) after solution annealing. H950 is aged at about 510 °C (950 °F), which gives it the highest strength (1,413 MPa yield). H1000 is aged at about 538 °C (1,000 °F). It is a little weaker (1,310 MPa yield) but tougher. H1050 is aged at about 566 °C (1,050 °F), which gives it the best toughness and ductility with a minimum yield strength of 1,138 MPa. The condition you choose depends on how strong and tough the application needs to be.
Q: Can you produce custom 1.4534 forgings according to our drawings?
A: Yes, we can produce custom parts according to your drawings and technical requirements. We can open files in DXF, DWG, PDF, and STEP formats. Our engineering team will review DFM (Design for Manufacturability) before we start making anything.
Q: What is the maximum size of 1.4534 forgings you can produce?
A: We can make 1.4534 forged parts that weigh up to 30,000 kg, seamless rolled rings that are up to 6 meters in diameter, and shafts and bars that are up to 15 meters long.
Q: Do you provide third-party inspection services?
A: Yes, third-party inspection conducted by reputable organizations such as SGS, Bureau Veritas (BV), or TÜV  is available upon request for our 1.4534 forgings.
Q: What is your typical lead time for 1.4534 forgings?
A: Our normal lead time is 4–6 weeks for standard products and 6–8 weeks for custom parts. We can also speed up production for urgent orders from our Jiangsu facility.
Q: What mill test certificates do you provide with 1.4534 forgings?
A: All 1.4534 (X3CrNiMoAl13-8-2) forgings are supplied with EN 10204 Type 3.1 mill test certificates as standard. EN 10204 3.2 (witnessed by an independent third-party inspector such as SGS, BV, or TÜV) is available upon request. The MTC includes full chemical analysis, mechanical test results, heat treatment records, and non-destructive test reports.
Q: Where is your factory located?
A: Our factory is located in Chengchang Industry Park, Jiangyin City, Jiangsu Province, China (postal code 214400), about 1.5 hours away from Shanghai. Benefiting from this strategic location, we enjoy efficient global shipping access through nearby Taicang Port and Shanghai Port.
Q: What is the difference between 1.4534 (X3CrNiMoAl13-8-2) and 17-4PH (1.4542)?
A: While both are precipitation hardening martensitic stainless steels, 1.4534 (S13800) and 17-4PH (1.4542 / S17400) differ in several important ways. 1.4534 contains more nickel (7.5–8.5% vs 3–5%) and uses molybdenum (2–2.5%) and aluminum as hardening agents, whereas 17-4PH uses copper (3–5%).Because of its higher nickel and molybdenum content ,1.4534 has more excellent pitting resistance equivalent (PRE ~19.5 vs ~16.3), significantly better toughness at equivalent strength levels, improved weldability, and better corrosion resistance in chloride and sour-service environments. However, 17-4PH is more widely available and lower in cost. 1.4534 is the best choice material for nuclear, aerospace turbine, and subsea valve applications where toughness and corrosion resistance cannot be compromised.
Q: Is 1.4534 (X3CrNiMoAl13-8-2) suitable for NACE MR0175 / ISO 15156 sour service applications?
A: Yes, 1.4534 (X3CrNiMoAl13-8-2 / UNS S13800) can be qualified for sour service based on NACE MR0175 / ISO 15156-3, subject to specified hardness restrictions.The standard allows the use of this precipitation-hardening stainless steel in the H1150 condition (max. 36 HRC / 352 HV10 as delivered), provided the in-service hardness does not exceed 36 HRC.For parts needing higher strength, an Engineering Critical Assessment (ECA) may permit use in the H1050 condition, within defined limits for H₂S partial pressure and temperature. Jiangsu Liangyi regularly supplies 1.4534 forgings for NACE-compliant applications including downhole valve parts and ESP motor shafts.Always refer to NACE MR0175 / ISO 15156-3 Table B.3 for the specific alloy designation, heat treatment condition, and environmental limits applicable to your project.
Q: What welding process is recommended for 1.4534 (X3CrNiMoAl13-8-2) forgings?
A: GTAW (TIG welding) using ER13-8Mo matching filler wire is the primary recommended process for 1.4534 (X3CrNiMoAl13-8-2) forgings, delivering optimal heat control, weld cleanliness and overall quality.Preheating is generally unnecessary for sections thinner than 25 mm, but is advised at 65–93 °C for heavier sections.The maximum inter-pass temperature shall not exceed 150 °C (300 °F). For structural or pressure-retaining welds, post-weld heat treatment (PWHT) is highly recommended:either a full re-solution anneal followed by aging, or an H1150 aging treatment at 621 °C for 4 hours when full re-solution is not feasible.To meet NACE MR0175 requirements, H1150 PWHT is mandatory to ensure weld metal hardness is ≤ 36 HRC.

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Jiangsu Liangyi is committed to providing the best price and superior quality 1.4534 / X3CrNiMoAl13-8-2 forged steel parts for global clients. As a trusted X3CrNiMoAl13-8-2 Jiangsu supplier with over 25 years of experience, we welcome your inquiries for custom forgings tailored to your specific requirements.

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