Haynes Alloy 25 (Udimet L605 / UNS R30605) Cobalt Alloy Forgings | China Manufacturer

By Jiangsu Liangyi Co., Limited · Jiangyin, Jiangsu, China · Last updated: April 2025

⚡ Haynes Alloy 25 (L605) — Key Facts at a Glance

Also Known AsUdimet L605 · AMS 5759 · UNS R30605
Alloy SystemCo-20Cr-15W-10Ni (cobalt base)
Max Continuous Service Temp.2150°F (1176°C)
Oxidation Resistance to1900°F (1038°C)
Density9.13 g/cm³ (0.330 lb/in³)
Melting Range1329–1410°C (2425–2570°F)
Tensile Strength (RT min.)125,000 psi / 862 MPa
Yield Strength (RT min.)45,000 psi / 310 MPa
DIN Material No.2.4964 (CoCr20W15Ni10)
Governing StandardAMS 5759 (bars & forgings)
Max Forging Weight30 tons per single piece
Max Ring Diameter6,000 mm (seamless rolled)
WeldabilityGood — GTAW preferred, no preheat
Supplier CertificationISO 9001:2015 · EN 10204 3.1/3.2
Lead Time (raw forgings)4–6 weeks
MOQ100 kg (standard) · 500 kg (custom)

What Is Haynes Alloy 25 (L605)? — Material Overview & main Properties

Jiangsu Liangyi, a top ISO 9001:2015 certified China Haynes Alloy 25 manufacturer strategically located in Jiangyin, Jiangsu Province, specializes in producing high-quality Udimet L605 forged parts, Alloy L-605 open die forgings, and AMS 5759 cobalt alloy parts. With over 25 years of specialized forging experience and a global customer base spanning more than 50 countries, we deliver premium UNS R30605 Cobalt Alloy 25 products that meet the strictest international standards.

China Haynes Alloy 25 forged round bars manufacturer Jiangsu Liangyi
Haynes Alloy 25 / Udimet L605 forged round bars — Jiangsu Liangyi, Jiangyin China
Udimet L605 seamless rolled rings Jiangyin factory
L605 cobalt alloy seamless rolled rings — Jiangyin forging factory


Haynes Alloy 25 , also known as Udimet L605, Alloy L-605, AMS 5759 or UNS R30605, is a non‑magnetic, wrought cobalt‑chromium‑tungsten‑nickel superalloy, strengthened mainly by solid‑solution hardening.Its tungsten content of 14–16% is the main strengthening element at high temperatures, while chromium at 19–21% delivers excellent oxidation and corrosion resistance, making it the best material choice for harsh service conditions. Unlike many other superalloys, Haynes 25 is not age‑hardenable. Its performance comes entirely from its chemical composition and thermomechanical processing. This gives it stable and consistent mechanical properties over a wide temperature range, with no risk of degradation from over‑aging.

 Haynes 25 retains excellent tensile and yield strength up to 2150°F (1176°C) and provides excellent oxidation resistance up to 1900°F (1038°C). This combination of properties cannot be reached by conventional austenitic stainless steels, low‑alloy steels, or even many nickel‑based superalloys at the same temperatures.The cobalt base also gives Haynes 25 naturally better wear and galling resistance than nickel‑based alloys. This is a main advantage for rotating turbine parts, bearing races and valve seats that face surface contact pressure during operation.

💡 Why the Cobalt Base Matters: Haynes Alloy 25’s cobalt‑chromium‑tungsten composition forms a stable FCC matrix that resists phase changes even when exposed to long-term high temperatures — an issue common in nickel‑base alloys with high γ′ content.This thermodynamic stability means L605 parts do not need regular re‑heat treatment in service and can withstand thermal cycling without the risk of embrittlement from sigma‑phase formation at normal operating temperatures.

Additionally, Cobalt Alloy 25 exhibits outstanding corrosion resistance across a wide range of chemically aggressive environments, including resistance to oxidizing mineral acids at moderate concentrations, wet chlorine at ambient conditions, and sulfur-bearing combustion gases at elevated temperatures. Detailed corrosion resistance data by specific environment is provided in the Corrosion & Oxidation Resistance section below.

Why Choose Jiangsu Liangyi as Your L605 Forging Supplier

As a trusted Jiangsu L605 forging supplier with deep expertise in cobalt-based superalloys, we offer unmatched quality, reliability, and customer service for all your Haynes Alloy 25 requirements:

Advanced Manufacturing Capabilities

Our 80,000 m² modern factory has 2000–6300 ton hydraulic presses, 1–5 meter seamless ring rolling machines, and ten computer-controlled heat treatment furnaces. We can produce L605 forgings from 30 kg up to 30 tons with an annual manufacturing capacity of 120,000 tons.

Premium Material Quality

All our Haynes Alloy 25 forgings are made using only VIM/ESR or VIM/VAR double-melting processes to guarantee great material cleanliness, consistent fine-grained microstructure, and consistent mechanical properties that meet or exceed AMS 5759 and UNS R30605 requirements.

Comprehensive Quality Control

We carry out 100% non‑destructive testing including UT, MT and PT, and supply full EN 10204 3.1/3.2 mill test certificates with every shipment. Third‑party witness inspection by internationally recognized agencies such as SGS, Bureau Veritas, TÜV Rheinland or a customer‑appointed inspector can be arranged at an extra cost upon request.

Custom Solutions & In-House Machining

We specialize in producing custom L605 forgings according to your exact drawings, specifications, and tolerance requirements. Our in-house CNC machining capabilities provide finished parts ready for immediate assembly, reducing your lead time and logistics costs.

Available Haynes Alloy 25 Forged Product Shapes & Sizes

Our Jiangyin Cobalt Alloy 25 forging factory produces a full range of L605 forged products in all kinds of standard and custom shapes and sizes:

Forged Bars & Rods

  • Round bars (up to 2000mm diameter)
  • Square bars and flat bars
  • Rectangular bars and step shafts
  • Valve spindles and turbine rods
  • Custom length and diameter options

Seamless Rolled Rings

  • Seamless rolled rings (up to 6000mm OD)
  • Contoured rings and bearing races
  • Turbine guide rings and seal rings
  • Labyrinth rings and casing rings
  • Single-piece weight up to 30 tons

Hollow Forgings

  • Sleeves, bushes, and bushings
  • Hubs, housings, and shells
  • Casings and barrels (up to 3000mm OD)
  • Hollow bars and heavy-wall cylinders
  • Pipes and tubings for high-temperature service

Other Forged Components

  • Discs, disks, and plates (up to 3000mm diameter)
  • Blocks and flanged blanks
  • Turbine blades and impellers
  • Valve seats, cores, and bonnets
  • Custom forgings per customer drawings

Industrial Applications of L605 Cobalt Alloy Forgings

 Haynes Alloy 25 forgings are preferred over other superalloys when designers need a material that combines non‑magnetic properties, thermal stability above 900°C, hot gas corrosion resistance, and consistent long‑term strength without the complexity of precipitation hardening. These key application areas directly leverage these advantages:

Aerospace & Defense

Aerospace is still the largest user of Haynes Alloy 25 forgings. The alloy’s non‑magnetic property is essential for parts near navigation and guidance systems, while its oxidation resistance in combustion environments enables thin‑section designs that cannot be achieved with heavier or lower‑performance alloys.

Power Generation

In both gas turbine power plants and steam turbine stations, L605 parts must withstand tens of thousands of operating hours under cyclic thermal and mechanical loading. The alloy has resistance to thermal fatigue cracking and predictable creep behavior ,making it the best material choice for long-life power generation parts.

Industrial & Process Manufacturing

Oil & Gas

Marine

Manufacturing Process for Haynes Alloy 25 Forgings

Producing high-quality Haynes Alloy 25 forgings is far more demanding than manufacturing conventional stainless steels or low-alloy steels.L605’s high tungsten content (14–16%) greatly increases its flow resistance during hot forming, requiring larger forging press capacities, stricter temperature control, and more precise die design than similar nickel-based superalloys.The process sequence below shows our proven and validated production method for AMS 5759 cobalt alloy forgings.

Step 1 — Premium Double-Melting Process

The starting point for all our Haynes Alloy 25 forgings is double-melted ingot stock, produced by one of two proven routes:

Both routes guarantee a non-metallic inclusion content well below the limits that would be achievable with single-melt processing. This directly translates into superior fatigue life, reproducible mechanical properties, and reliable ultrasonic testing (UT) inspectability in the finished forging.

Step 2 — Controlled Hot Working & Open Die Forging

We heat L605 ingots to the forging temperature range — usually 1093°C to 1204°C (2000°F to 2200°F) — and shape them using our 2000–6300 ton hydraulic presses. The main goal at this step is to reach a minimum forging ratio of 3:1 (reducing the cross-sectional area) to fully break down the original cast structure and create a consistent, fine-grained forged matrix. For important rotating parts, we regularly achieve forging ratios of 5:1 to 7:1, which makes the material much better at bending without breaking and more resistant to fatigue crack initiation, compared to material that’s only lightly forged. We monitor the hot working temperature using calibrated contact thermometers and infrared thermal cameras at multiple points during each press movement. If the surface temperature drops below 982°C (1800°F), we stop forging and put the piece back in the furnace. This prevents forging at temperatures where the metal doesn’t fully recrystallize — which would leave a mixed structure of large and small grains that harms the material’s fatigue performance.


Step 3 — Seamless Ring Rolling

For seamless rolled ring production, pierced blanks are rolled on our 1–5 meter diameter radial-axial ring rolling machines. The ring rolling process adds extra shaping around the ring’s circumference, further refining the grain structure and directing the metal flow to follow the ring’s circular direction — the main direction stress acts in most turbine ring parts. This gives stronger mechanical properties in the key load direction compared to rings cut from solid material or machined discs.

Step 4 — Solution Annealing Heat Treatment

After forging, all Haynes Alloy 25 parts undergo the following standardized solution annealing heat treatment:

This treatment dissolves any carbide deposits formed during cooling after forging, restores the fully recrystallized grain structure, and removes leftover forging stresses. The result is a consistent, fine-grained austenitic matrix with steady mechanical properties across the entire section, confirmed by structural tests on samples taken from test pieces forged at the same time as the production part.

✅ Quality Guarantee: All Jiangsu Liangyi Haynes Alloy 25 forgings are guaranteed to be free from cracks, laps, seams, segregation bands, and non-metallic inclusions of a size that would cause rejection under the applicable UT acceptance criteria (ASTM A388, AMS 2630 class, or customer-specified criteria).

Chemical Composition of Haynes Alloy 25 (UNS R30605 / AMS 5759)

The chemical composition limits below apply to Haynes Alloy 25 bars and forgings per AMS 5759 and UNS R30605. The "Role in Alloy" column explains the metallurgical function of each element — useful context for engineers performing failure analysis, weldability assessments, or alloy substitution evaluations:

Table 1 — Chemical Composition of Haynes Alloy 25 / Udimet L605 / UNS R30605 (per AMS 5759)
ElementSymbolWeight % RangeMetallurgical Role
CobaltCoBalance (~49–53%)FCC matrix; provides non-magnetic behavior, high melting point, and wear resistance
ChromiumCr19.0 – 21.0Forms Cr₂O₃ protective scale; primary contributor to oxidation and corrosion resistance
TungstenW14.0 – 16.0Principal solid-solution strengthener; dramatically increases high-temperature strength and creep resistance
NickelNi9.0 – 11.0Stabilizes the FCC phase; improves ductility, formability, and weldability
IronFe3.0 MaxControlled residual; limited to avoid reducing high-temperature stability
ManganeseMn1.0 – 2.0Deoxidizer during melting; improves hot workability by binding sulfur
CarbonC0.05 – 0.15Forms M₆C and M₂₃C₆ carbides at grain boundaries; contributes to high-temperature strength; critical for creep resistance
SiliconSi0.40 MaxDeoxidizer; limited to control effect on hot corrosion resistance
PhosphorusP0.040 MaxControlled impurity; excess reduces hot ductility
SulfurS0.030 MaxControlled impurity; excess causes hot shortness and reduces fatigue life

Room-Temperature Mechanical Properties of Haynes Alloy 25 Forgings (AMS 5759)

The table below lists minimum guaranteed mechanical properties per AMS 5759 at room temperature (21°C / 70°F) in the annealed condition, alongside typical achieved values for reference. The AMS minimums represent the acceptance threshold; our production forgings consistently exceed these values.

Table 2 — Room-Temperature Mechanical Properties of Haynes Alloy 25 / L605 Forgings (AMS 5759, Annealed)
PropertyAMS 5759 MinimumTypical Achieved ValueSI Units (Min.)
Ultimate Tensile Strength (UTS)125,000 psi~145,000–155,000 psi862 MPa
0.2% Proof Strength (Yield)45,000 psi~70,000–80,000 psi310 MPa
Elongation (in 2")30%~55–65%30%
Reduction of AreaNot specified~50–60%
Hardness (Rockwell B)Not specified~95–100 HRB
Note: The large difference between the AMS minimum yield strength of 310 MPa and our typical actual value shows the strong strengthening effect from tungsten, which is fully realized in properly processed forged material. Real mechanical test results are recorded in the EN 10204 3.1 mill test certificate supplied with each shipment.

Elevated-Temperature Mechanical Properties of Haynes Alloy 25 (L605)

The room-temperature values listed in AMS 5759 are the contractual minimums — but for design engineers working on gas turbine parts, the high-temperature strength data is what really determines material choice. The data below shows typical tensile properties at operating temperatures  for annealed Haynes Alloy 25 forgings. These are the important values when setting wall thicknesses, determining creep limits, or comparing L605 with other materials for a specific operating temperature.

How to read this table: All values are typical tensile test results, not specification minimums. Actual values from individual heats will vary by ±10–15%. For design calculations in safety-critical applications, apply appropriate design allowables from approved design data sources (e.g., MIL-HDBK-5 / MMPDS or equivalent).
Table 3 — Elevated-Temperature Tensile Properties of Haynes Alloy 25 / L605 (Typical, Annealed Forging, 25mm diameter bar)
TemperatureUTS — Typical (MPa)0.2% YS — Typical (MPa)Elongation — Typical (%)UTS vs. Room Temp
21°C (70°F) — Baseline~1005~505~62100% (reference)
315°C (600°F)~880~440~57~88%
538°C (1000°F)~800~395~51~80%
649°C (1200°F)~735~365~47~73%
760°C (1400°F)~585~305~43~58%
871°C (1600°F)~370~255~48~37%
982°C (1800°F)~195~140~55~19%
1093°C (2000°F)~95~70~65~9%

Several patterns in this data are worth highlighting for designers unfamiliar with Haynes Alloy 25 behavior:

💡 Creep & Stress Rupture: For applications in the 650°C–900°C range where creep limits lifetime, the 100-hour stress rupture strength of annealed Haynes Alloy 25 is about 415 MPa at 649°C (1200°F) and 97 MPa at 871°C (1600°F). These values are clearly better than most nickel-solid-solution alloys in the same temperature range, making L605 the preferred choice for long-life turbine parts working in this temperature window. Contact our engineering team for a full creep rupture dataset at your specific operating temperature.

Physical & Thermal Properties of Haynes Alloy 25 (L605 / UNS R30605)

The following physical and thermal properties are typical values for Haynes Alloy 25 in the annealed condition. These values are needed for thermal modeling, stress analysis, and heat exchanger design calculations. Note that all thermal properties are temperature-dependent; values at 871°C are included where available to illustrate the behavior at operating temperature:

Table 4 — Physical & Thermal Properties of Haynes Alloy 25 / L605 (Typical, Annealed)
PropertyValueTemperature / Condition
Density9.13 g/cm³ (0.330 lb/in³)Room temperature
Melting Range (Solidus–Liquidus)~1329–1410°C (2425–2570°F)
Specific Heat Capacity0.385 J/g·°C (0.092 BTU/lb·°F)Room temperature
Thermal Conductivity9.8 W/m·KRoom temperature (21°C)
Thermal Conductivity~17.8 W/m·K871°C (1600°F)
Mean CTE (Thermal Expansion)12.3 µm/m·°C (6.8 µin/in·°F)21–538°C (70–1000°F)
Mean CTE (Thermal Expansion)13.5 µm/m·°C (7.5 µin/in·°F)21–871°C (70–1600°F)
Modulus of Elasticity (Young's Modulus)233 GPa (33.8 × 10⁶ psi)Room temperature
Modulus of Elasticity~159 GPa (23 × 10⁶ psi)871°C (1600°F)
Poisson's Ratio0.31Room temperature
Shear Modulus~88 GPa (12.8 × 10⁶ psi)Room temperature
Electrical Resistivity0.89 µΩ·mRoom temperature
Magnetic PermeabilityNon-magnetic (<1.05 µ)Annealed; remains non-magnetic after deformation

Corrosion & Oxidation Resistance of Haynes Alloy 25 in Specific Environments

The corrosion resistance of Haynes Alloy 25 is very different from nickel-base corrosion-resistant alloys such as Hastelloy C276. While C276 is designed to resist reducing acid environments as much as possible, L605 is optimized for high-temperature corrosion, including high-temperature gas oxidation, sulfidation, and hot corrosion, rather than liquid corrosion at room temperature. Understanding this difference helps avoid costly mistakes in material selection.

High-Temperature Oxidation

Haynes Alloy 25 forms a dense, stable chromium oxide (Cr₂O₃) layer in air and combustion gases. This layer repairs itself and protects the material up to about 1038°C (1900°F) in continuous use. Above this temperature, the oxide layer grows faster and may flake off during repeated heating and cooling. That is why the safe maximum continuous service temperature is set at 1176°C (2150°F) — the annealing temperature — instead of the temperature where the oxide layer stays stable.Most austenitic stainless steels such as 304, 316 and 310 lose their protective oxide layer above 900°C, and Inconel 625 performs well only up to around 1000°C. L605 clearly offers better oxidation resistance in the 900°C–1100°C range.


Sulfidation Resistance

One often overlooked benefit of the cobalt base is better sulfidation resistance than nickel-base alloys. In sulfur-containing atmospheres, such as combustion gases from fuels with sulfur or refinery settings, cobalt-base alloys usually perform better than nickel-base alloys with similar chromium content. This is because cobalt sulfides are less stable and form more slowly than nickel sulfides. Haynes Alloy 25 shows good resistance to sulfidation damage at temperatures up to about 870°C (1600°F) under the sulfur levels found in normal combustion conditions.

Aqueous Corrosion — Environment-by-Environment Summary

Table 5 — Corrosion Resistance of Haynes Alloy 25 (L605) in Aqueous Environments (General Guidance)
Environment / MediumConcentration / Temp.Resistance RatingNotes
Nitric Acid (HNO₃) — oxidizing<65%, <80°CGoodCr₂O₃ passive film stable in oxidizing acid; acceptable corrosion rate in moderate concentrations
Nitric Acid (HNO₃) — fuming>65% or >80°CLimitedAccelerated attack at high concentration/temperature; consult corrosion engineer
Hydrochloric Acid (HCl) — dilute<1%, <25°CLimitedOnly marginal resistance; acceptable only for brief contact in non-structural applications
Hydrochloric Acid (HCl) — concentrated>5% any temp.Not RecommendedHigh corrosion rate; use Hastelloy C276 or C22 instead
Sulfuric Acid (H₂SO₄)<10%, <25°CLimitedMarginal resistance in dilute cold acid only; not suitable for process service
Wet Chlorine / Chlorine WaterAmbient temp.GoodBetter resistance than stainless steels; suitable for dilute chlorine-containing streams at ambient temperature
Sodium Hydroxide (NaOH)All conc., <100°CGoodPassive in alkaline environments; low corrosion rates
Seawater / Saline solutionsAmbient, staticModerateSusceptible to crevice corrosion and pitting in stagnant chloride at ambient temperature; better in flowing conditions
Hydrofluoric Acid (HF)AnyNot RecommendedAggressive attack; use specialist alloys (e.g., Monel 400) for HF service
⚠️ Important: The table above is for general reference only. Actual corrosion rates depend on temperature, concentration, flow speed, galvanic coupling, and specific impurities present. Always perform corrosion testing under real working conditions or consult a qualified corrosion engineer before choosing the material for critical parts.

Welding, Machining & Fabrication Guide for Haynes Alloy 25 (L605)

L605 is a difficult material to machine and form. Its high tungsten content and quick work-hardening trait need special tools, settings, and strict process control, which are very different from those used for stainless steels or nickel alloys. The advice below shows current best practices for making Haynes Alloy 25 / UNS R30605 parts:

🔥 Welding — Process Selection

  • Preferred process: GTAW (TIG / Gas Tungsten Arc Welding)
  • Alternative: GMAW (MIG) for high-deposition applications; SMAW is possible but not preferred
  • Filler metal: ERCoCr-E (cobalt-chromium matching filler) preferred; ER-3 (Haynes 25 / L605 matching) for highest property match
  • Shielding gas: 100% Argon or Ar/He (75/25) blend for improved fusion on heavy sections
  • Preheat: Not needed — one of L605's practical advantages over many ferritic and martensitic alloys
  • Interpass temperature: Keep below 150°C (300°F) to minimize hot cracking sensitivity
  • Post-weld treatment: Solution anneal at 1176–1232°C (2150–2250°F) followed by rapid quench is recommended to restore ductility and relieve residual stress; may be omitted for minor repair welds at customer's discretion
  • Weld joint cleanliness: Remove all oxide scale from heat affected zone before welding; use stainless steel wire brush (dedicated to cobalt alloys, not shared with stainless tools)

⚙️ CNC Machining — Turning & Milling

  • Key challenge: L605 work-hardens rapidly; tool rubbing without active cutting will harden the surface and accelerate tool wear
  • Tooling: Uncoated or TiAlN-coated carbide (C2/C3 grade); ceramic tools are not recommended due to interrupted cutting behavior
  • Turning speed: 15–25 m/min (50–80 sfm) for roughing; 20–35 m/min (65–115 sfm) for finishing with sharp tooling
  • Feed rate: 0.10–0.30 mm/rev (0.004–0.012 in/rev); heavier feeds are preferable to light finishing passes to prevent work hardening
  • Depth of cut: Engage material positively; avoid very shallow cuts that generate heat without removing material
  • Coolant: Flood coolant (water-soluble oil, ≥8% concentration) is mandatory; dry machining will cause rapid tool failure and surface damage
  • Do not stop mid-cut: Always disengage the tool before stopping feed to avoid a hardened spot on the workpiece surface

🔩 Drilling

  • Tooling: M42 HSS-Co or solid carbide drills; avoid standard HSS
  • Speed: 5–12 m/min (15–40 sfm)
  • Feed: 0.05–0.15 mm/rev — keep positive chip-breaking feed
  • Peck drilling: Use peck drilling for holes deeper than 3× diameter to clear chips and reduce heat buildup
  • Coolant: Flood or through-tool coolant mandatory for deep holes
  • Tip geometry: 135° split-point geometry preferred for better self-centering and reduced thrust force

🔄 Cold Working & Forming

  • L605 can be cold worked, but its high work-hardening rate means significantly more force is needed per unit reduction compared to austenitic stainless steel (304/316)
  • Intermediate anneals at 1176–1232°C are required after every 15–25% reduction in cross-section to restore ductility for further working
  • Spring-back must be accounted for in bend tooling design; L605 has a higher spring-back than stainless steel
  • All cold-worked material should be solution-annealed after final forming to restore stress-corrosion resistance and stabilize mechanical properties

🌡️ Hot Working Temperature Range

  • Recommended hot working window: 982–1204°C (1800–2200°F)
  • Minimum working temperature: 982°C (1800°F) — do not work below this; incomplete recrystallization produces mixed grain matrix
  • Maximum starting temperature: 1232°C (2250°F) — approaching the annealing temperature; excessive temperature causes incipient melting risk in segregated areas
  • Allow full furnace soak time (minimum 1 hr per 25mm section thickness) before extracting for hot working
  • Cobalt alloys cool faster than steel due to lower thermal conductivity; work quickly and return to furnace promptly

🧹 Surface Finishing & Cleaning

  • Surface oxide scale from hot working or heat treatment must be removed by grit blasting, grinding, or pickling before further processing
  • Pickling solution: HNO₃/HF mixture (15% HNO₃ + 3% HF by volume at 60°C) — standard cobalt alloy pickle; follow all safety precautions for HF handling
  • Do not use tools contaminated with iron (e.g., carbon steel wire brushes, grinding wheels used on steel) on L605 surfaces — embedded iron particles cause rust staining and can initiate corrosion
  • Final surface finish: Ra 1.6–3.2 µm achievable with carbide tooling; Ra 0.8 µm achievable with grinding

International Standards Cross-Reference for Haynes Alloy 25 (L605)

Haynes Alloy 25 is recognized and specified under multiple national and international standards. The table below provides a comprehensive cross-reference to help procurement engineers, quality managers, and inspection bodies identify equivalent designations across different standards systems:

Table 6 — International Standards and Designations for Haynes Alloy 25 / Udimet L605 / UNS R30605
Standard / SystemDesignation / NumberProduct Form CoveredIssuing Body
UNS NumberR30605All product forms (generic designation)ASTM / SAE (USA)
AMS SpecificationAMS 5759Bars, rods, wire, and forgingsSAE International (USA)
AMS SpecificationAMS 5537Sheet, strip, and plateSAE International (USA)
AMS SpecificationAMS 5538Welding wire (filler metal)SAE International (USA)
ASTMASTM B815Cobalt alloy forgings (general)ASTM International (USA)
DIN Material Number2.4964All product formsDIN / DIN EN (Germany / Europe)
European Compositional DesignationCoCr20W15Ni10All product forms (EN-style)EN (European Standard)
Common Trade NameHaynes Alloy 25Haynes International, Inc. (USA)
Common Trade NameUdimet L605 / Alloy L-605Special Metals / Precision Castparts (USA)
Mill Test Certificate StandardEN 10204 Type 3.1 (standard) / Type 3.2 (with 3rd party)All product formsEN (European Standard)
NDT Standard (UT)ASTM A388 / AMS 2630Forgings and bar stockASTM International / SAE (USA)
NDT Standard (PT)ASTM E165 / AMS 2647All product formsASTM International / SAE (USA)
Customer-Specified Standards: We can produce Haynes Alloy 25 forgings according to customers’ proprietary material specifications and purchase order requirements. When a customer’s specification refers to specific OEM material standards, we will carefully review the requirements and confirm our ability to meet them before accepting the order. Please provide your full specification documents and we will advise on their applicability.

Haynes Alloy 25 vs. Other High-Temperature Alloys — Side-by-Side Comparison

The following comparison is intended for engineers evaluating Haynes Alloy 25 against other commonly specified superalloys for high-temperature forging applications. Values are typical for annealed/solution-treated wrought product unless otherwise noted:

Table 7 — Haynes Alloy 25 (L605) vs. Inconel 625, Inconel 718, Hastelloy X, and Nimonic 90
Property / CriterionHaynes 25 (L605)Inconel 625 (N06625)Inconel 718 (N07718)Hastelloy X (N06002)Nimonic 90 (N07090)
Base ElementCobaltNickelNickelNickelNickel
Strengthening TypeSolid solution (W, Cr)Solid solution (Nb, Mo)Precipitation (γ″ Ni₃Nb)Solid solution (Mo, W)Precipitation (γ′ Ni₃(Al,Ti))
Max Continuous Service Temp.1176°C (2150°F)~1000°C (1830°F)~704°C (1300°F)~1200°C (2200°F)~920°C (1690°F)
UTS at Room Temp. (Typical)~1005 MPa~930 MPa~1380 MPa~785 MPa~1240 MPa
UTS at 871°C / 1600°F (Typical)~370 MPa~310 MPa~170 MPa~255 MPa~145 MPa
Density9.13 g/cm³ (heaviest)8.44 g/cm³8.19 g/cm³8.22 g/cm³8.18 g/cm³
Non-Magnetic✅ Yes✅ Yes✅ Yes✅ Yes✅ Yes
Sulfidation ResistanceExcellentGoodModerateGoodModerate
Wear / Galling ResistanceExcellent (Co base)ModerateGoodModerateGood
Machinability (relative)Difficult (work hardens fast)DifficultModerate (aged)ModerateDifficult (aged)
Governing AMS StandardAMS 5759AMS 5666AMS 5662 / 5663AMS 5754AMS 5829
Relative Material Cost (approximate)High (W content drives cost)High (Nb, Mo)Moderate-HighHigh (Mo, W)High (Co alloyed)
Selection Guidance:  Choose Haynes Alloy 25 (L605) if your part needs (a) operation above 900°C under load, (b) non-magnetic properties at high temperatures, (c) excellent resistance to sulfidation or hot gas corrosion, or (d) long-lasting bearing or wear surfaces at high temperatures. For uses below 700°C where high room-temperature strength is most important, Inconel 718 is usually stronger and less expensive.

Comprehensive Quality Inspection & Testing

To guarantee the highest quality standards for every UNS R30605 forged part, we perform a full range of inspection and testing procedures in our in-house quality control laboratory. All test procedures are carried out by trained and experienced quality personnel based on the applicable ASTM, AMS, and EN standards:

Minimum Order Quantity (MOQ), Packaging & Commercial Terms

The following commercial information applies to standard export orders for Haynes Alloy 25 / L605 / AMS 5759 forgings from Jiangsu Liangyi Co., Limited. All terms are subject to confirmation at the time of order placement and may vary for large-volume or long-term supply agreements:

📦 Minimum Order Quantity (MOQ)

  • Standard product shapes (round bars, flat bars, standard rings): 100 kg per order, per size
  • Custom open die forgings (per drawing): 500 kg minimum per part number
  • Trial/sample orders: Negotiable for new customers — contact our sales team to discuss your specific requirement
  • Long-term blanket orders: Preferred for aerospace and power generation OEM customers; lower per-shipment minimums available with annual volume commitment

🗃️ Export Packaging Standard

  • Primary wrap: Individual parts wrapped in VCI (Vapor Corrosion Inhibitor) polyethylene film to prevent surface oxidation and contamination during sea freight
  • Secondary packaging: ISPM 15 certified heat-treated wooden cases or plywood crates for all sea shipments
  • Identification marking: Each piece marked with heat number, part number, material grade (AMS 5759 / UNS R30605), weight, and dimensions according to EN 10204 requirements
  • Case marking: Gross weight, net weight, dimensions, and country of origin marked on all exterior surfaces per destination country import requirements

📋 Documentation Included

  • Commercial invoice and packing list
  • EN 10204 Type 3.1 mill test certificate (standard — included in price)
  • EN 10204 Type 3.2 certificate with SGS, BV, or TÜV (available at additional cost)
  • Dimension test report / CMM report
  • NDT test reports (UT, PT, MT as applicable)
  • Certificate of Conformance (CoC)
  • Country of Origin Certificate (for customs purposes)
  • REACH / RoHS declaration (upon request)

🚢 Lead Time & Shipping

  • Standard raw forgings: 4–6 weeks from order confirmation and receipt of approved drawings
  • Fully machined parts: 6–8 weeks
  • Rush/expedited orders: Subject to capacity — contact us to check availability; surcharge may apply
  • Shipping modes: Sea freight (FCL or LCL) for most orders; air freight available for urgent small shipments
  • Incoterms: EXW, FOB Qingdao/Shanghai, CIF, DAP — as agreed per order
  • Payment terms: T/T (wire transfer); L/C accepted for orders above USD 50,000

🏅 Certifications & Qualifications

  • ISO 9001:2015 quality management system (current, third-party certified)
  • EN 10204 3.1 / 3.2 mill certificate issuance capability
  • Third-party witness inspection by customer-nominated agencies (SGS, Bureau Veritas, TÜV Rheinland, or equivalent) arrangeable upon request
  • Customer-specific material specification review and compliance confirmation available — please provide your specification documents at time of inquiry
  • 25+ years of export experience; established relationships with freight forwarders and customs brokers in more than 50 countries

🛠️ Value-Added Services

  • In-house CNC turning, milling, and grinding to finished dimensions
  • Rough machining to customer-specified allowances (e.g., +3mm machining stock per side)
  • In-house heat treatment (annealing, solution treating) with furnace temperature charts included
  • Third-party NDT witness inspection coordination
  • DFM (Design for Manufacturability) consultation for new part development
  • Reverse engineering support from sample parts or worn parts

Frequently Asked Questions (FAQ)

What is Haynes Alloy 25 (L605), and how does it differ from nickel-based superalloys?
Haynes Alloy 25 (UNS R30605 / AMS 5759) is a cobalt-chromium-tungsten-nickel solid-solution superalloy, unlike most high-performance superalloys that use nickel as the base metal. The cobalt base gives L605 three clear advantages over nickel alloys: (1) a higher melting point (around 1410°C, compared to about 1350°C for Inconel 718), (2) better sulfidation resistance in hot sulfur-containing gas environments, and (3) stronger wear and galling resistance thanks to cobalt’s natural hardness. The trade-offs are higher density (9.13 g/cm³) and higher raw material costs due to the tungsten content. L605 cannot be strengthened by heat treatment aging — all its strength comes from solid-solution hardening — which simplifies heat treatment but lowers the maximum room-temperature strength compared to precipitation-hardened alloys such as Inconel 718.
What are the high-temperature mechanical properties of Haynes Alloy 25?
Haynes Alloy 25 retains useful mechanical properties to temperatures well above those of most nickel and stainless steel alloys. Typical tensile strength values (annealed) at main temperatures are: ~1005 MPa at room temperature, ~800 MPa at 538°C, ~585 MPa at 760°C, ~370 MPa at 871°C, and ~95 MPa at 1093°C. The 100-hour stress rupture strength is about 415 MPa at 649°C and 97 MPa at 871°C. Please see the Elevated-Temperature Properties table above for the full dataset, and contact our engineering team for creep rupture data at your specific operating temperature.
Can Haynes Alloy 25 (L605) be welded, and what filler metal should be used?
Yes, L605 welds well. The best welding method is GTAW (TIG welding) with ERCoCr-E cobalt-base filler metal, which matches the material’s properties most closely. Preheating is not needed. Keep the interpass temperature below 150°C to lower the chance of hot cracking near the weld. After welding, we suggest a solution anneal at 1176–1232°C followed by quick cooling to bring back full ductility and remove leftover welding stresses. For repair welding on parts already in use, post-weld annealing may not always be possible; talk to our engineering team about qualified welding steps for your specific repair needs.
What is the minimum order quantity (MOQ) for Haynes Alloy 25 forgings?
The minimum order quantity is 100 kg for standard product shapes (round bars, flat bars, standard ring sizes) and 500 kg for custom open die forgings made to customer-supplied drawings. Trial orders for new customers can be discussed — please contact our sales team with your specific part requirements and quantity. For established customers with annual volume commitments, lower per-shipment minimums and shorter lead times are available through blanket order arrangements.
What is the DIN or European equivalent of Haynes Alloy 25 / UNS R30605?
The European / DIN equivalent of Haynes Alloy 25 (UNS R30605) is material number 2.4964, with the compositional designation CoCr20W15Ni10. In the US, the governing specification for bars and forgings is AMS 5759 (SAE/AMS), and the generic UNS designation is R30605. For sheet and plate, the equivalent AMS specification is AMS 5537. We can supply material to any of these specifications and provide mill test certificates referencing the applicable standard.
Is Haynes Alloy 25 suitable for sour gas (H₂S) service in oil and gas applications?
Haynes Alloy 25 works well in high-temperature sulfur-containing environments, including combustion gases with H₂S. However, for room-temperature sour gas (H₂S) use as defined by NACE MR0175 / ISO 15156, choosing cobalt alloys needs careful review of the actual H₂S partial pressure, total pressure, chloride level, and temperature. L605 is not listed in ISO 15156-3 tables as an approved material for all sour service conditions without testing. For HPHT wellhead and downhole parts in sour environments, we suggest consulting an ISO 15156-qualified materials engineer to decide if L605 fits your service conditions, or if another alloy such as Inconel 718 (which is listed in ISO 15156-3) is more suitable.
What is the typical lead time for Haynes Alloy 25 forgings?
Standard lead time for L605 raw forgings is 4–6 weeks after we receive the confirmed purchase order and approved drawings. Fully machined and tested parts usually take 6–8 weeks. We can accept rush orders with faster production based on our current capacity — please contact our sales team with your needed delivery date and we will let you know if it is possible when you inquire.
Do you provide mill test certificates with your L605 forgings?
Yes, we include full EN 10204 Type 3.1 mill test certificates (MTC) with every shipment of Haynes Alloy 25 forgings as standard. EN 10204 Type 3.2 certificates, which include on-site inspection and countersignature from an independent third-party inspector, are also available at an extra cost if requested by the customer, using either the customer’s chosen inspection agency or one agreed by both sides. The MTC covers all chemical analysis results, mechanical test results, heat treatment records, and NDT reports, all traceable to the original heat number of the ingot used.
Can you manufacture custom L605 forgings according to our drawings?
Absolutely. Custom open die forgings and seamless rolled rings in Haynes Alloy 25 and other superalloys are made to meet customer-supplied 2D or 3D drawings.Please send your detailed drawings (PDF, DXF, STEP, or IGES format), material specifications, needed standards, quantity, and any special requirements (surface finish, tolerances, NDT acceptance criteria, third-party inspection) to sales@jnmtforgedparts.com and our engineering team will review them and provide a detailed quotation within 24–48 hours.
What is the maximum size and weight you can forge in Haynes Alloy 25?
 We can make Haynes Alloy 25 (L605) forgings up to 30 tons per single piece. For round bars and solid discs, the maximum forged diameter is 2000 mm. For seamless rolled rings, we can produce outer diameters up to 6000 mm. Hollow forgings such as cylinders and barrels can be made up to 3000 mm in outer diameter. Custom shapes beyond these standard dimensions can be evaluated individually — please contact our engineering team to discuss your specific geometry and weight requirements.
What other superalloy materials do you offer besides Haynes Alloy 25?
In addition to Haynes Alloy 25 / L605, we produce forgings in a wide range of other nickel- and cobalt-base superalloys, including Inconel 625 (UNS N06625), Inconel 718 (UNS N07718), Hastelloy C276 (UNS N10276), Hastelloy C22, Nimonic 80A (UNS N07080), Nimonic 90 (UNS N07090), Waspaloy (UNS N07001), and many others. Please visit our Materials page for the full list of alloys we offer.

Contact Us for a Free Haynes Alloy 25 Forging Quotation

Jiangsu Liangyi Co., Limited is your trusted China L605 cobalt alloy manufacturer for high-quality Haynes Alloy 25, Udimet L605, and UNS R30605 forgings. Whether you need standard bars and rings or custom intricate parts, we have the expertise, capabilities, and more than 25 years of experience to meet your exact requirements.To get a detailed, competitive quotation, please send us your detailed 2D/3D drawings, material specifications, quantity requirements, required standards, and any special instructions. Our experienced engineering team will review your request and provide a quotation within 24–48 hours.

📧 Get Your Free Quotation Now

Contact Information:

📧 Inquiry Email: sales@jnmtforgedparts.com

📞 Phone / WhatsApp: +86-13585067993

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

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