High Temperature Alloy Plate (Inconel®, Hastelloy®, Haynes®, etc.)
✓ Ultra-High Temperature Resistance: Maintains structural integrity at 1,000°C (1,832°F) with **<1% scaling** after 1,000 hours (Inconel 601).
✓ Corrosion Immunity: Resists chloride stress corrosion cracking (Cl-SCC), sulfuric acid (H₂SO₄), and molten salts with **<0.05mm/year corrosion rate**.
✓ Thermal Fatigue Resilience: Withstands 20,000+ thermal cycles between 25°C–1,100°C (77°F–2,012°F) without microcracking.
✓ Precision Fabrication: Hot/cold-rolled plates with **±0.1mm thickness tolerance** and Ra ≤1.6μm surface finish for welding/machining.
High Temperature Alloy Plate (Inconel®, Hastelloy®, Haynes®, etc.)
Engineered for industries operating in extreme thermal and corrosive environments, our high-temperature alloy plates deliver unmatched performance in aerospace, power generation, and chemical processing. Made from nickel-chromium-molybdenum superalloys (e.g., Inconel 718: Ni-52.5%, Cr-19%, Mo-3%), these plates withstand temperatures up to 1,200°C (2,192°F) while resisting oxidation, sulfidation, and creep deformation. Certified to AMS 5599, ASTM B168, and ASME SB168, they outperform conventional stainless steel with 10x longer lifespan in aggressive conditions.
- Thickness: 0.5mm–200mm
- Sizes: 1,000mm x 2,000mm (standard) / custom-cut to 5,000mm x 2,500mm
- Surface Finishes: Pickled, Grinded (Ra ≤0.8μm), Shot Blasted
- Mechanical Properties (Inconel 718): Yield Strength ≥1,100 MPa | Tensile Strength ≥1,400 MPa | Elongation ≥12% | Hardness ≤35 HRC
| Parameter Category | Inconel 718 | Haynes 230 | Nimonic 90 |
|---|---|---|---|
| Material Standard | ASTM B637, UNS N07718 | ASTM B435, UNS N06230 | BS HR 901, UNS N07090 |
| Chemical Composition (%) | Ni: 50–55, Cr: 17–21, Fe: Balance, Mo: 2.8–3.3, Nb+Ta: 4.75–5.5, Ti: 0.65–1.15, Al: 0.2–0.8, C: ≤0.08 | Ni: 57–60, Cr: 20–24, W: 13–15, Mo: 1–3, Co: ≤5, Fe: ≤3, Mn: ≤0.5, Si: ≤0.4, La: 0.02–0.12 | Ni: 85–90, Cr: 18–21, Co: 15–21, Ti: 2.0–2.6, Al: 1.0–1.5, C: ≤0.08 |
| Tensile Strength (MPa) | 1275–1550 (Aged) | 760–895 (Annealed) | 950–1200 (Aged) |
| Yield Strength (MPa) | 1035–1350 (Aged) | 345–415 (Annealed) | 600–800 (Aged) |
| Elongation (%) | ≥12 (in 50mm gauge length) | ≥40 (in 50mm gauge length) | ≥15 (in 50mm gauge length) |
| Hardness | Rockwell C35–45 | Rockwell B85–95 | Rockwell C25–35 |
| Density (g/cm³) | 8.19 | 8.97 | 8.19 |
| Melting Range (°C) | 1260–1336 | 1315–1370 | 1360–1425 |
| Thermal Conductivity (W/m·K) | 11.4 (at 20°C) | 11.7 (at 20°C) | 12.0 (at 20°C) |
| Thermal Expansion (10⁻⁶/°C) | 13.0 (20–100°C) | 12.6 (20–100°C) | 13.5 (20–100°C) |
| Max Service Temperature (°C) | 700 (continuous) | 1150 (continuous) | 950 (continuous) |
| Oxidation Resistance | Excellent up to 700°C in air. | Outstanding up to 1150°C due to Cr/W-rich oxide layer. | Excellent up to 950°C in oxidizing environments. |
| Creep Resistance | High resistance at 650–700°C. | Stable up to 980°C under stress. | Superior at 800–950°C. |
| Heat Treatment | Aging: 720°C/8h + 620°C/8h. | Solution Annealing: 1230°C (rapid cooling). | Aging: 700–800°C for 16h. |
| Surface Finishes | Annealed & Pickled, Polished (Ra ≤0.8μm). | Annealed & Descaled, Polished. | Hot Rolled, Annealed & Pickled. |
| Plate Dimensions | – Thickness: 5–100mm – Width: 1000–2000mm – Length: 3000–6000mm. | Same as Inconel 718. | – Thickness: 5–50mm – Width: 1000–1500mm. |
| Key Applications | Aerospace turbines, nuclear reactors, high-stress fasteners. | Gas turbine combustors, industrial furnace parts. | Jet engine components, gas turbine blades, exhaust systems. |
High Temperature Alloy Plate (Inconel®, Hastelloy®, Haynes®, etc.) Applications
| Industry | Critical Use Cases | High-Temperature Alloy Plate Advantage |
|---|---|---|
| Aerospace | Jet engine combustors, afterburner liners | 0.02mm oxidation depth after 1,000h at 1,100°C (2,012°F). |
| Power Generation | Gas turbine blades, nuclear reactor cores | Resists creep deformation at 950°C (1,742°F). |
| Chemical Processing | Ethylene cracking furnaces, reformer tubes | Withstands 1,200°C (2,192°F) in H₂S/CO-rich environments. |
| Oil & Gas | Flare stacks, hydrocracker components | Immunity to sulfidation at 650°C (1,202°F). |
High Temperature Alloy Plate (Inconel®, Hastelloy®, Haynes®, etc.) Product Packaging
High Temperature Alloy Plate (Inconel®, Hastelloy®, Haynes®, etc.) are engineered for extreme environments including jet engines, nuclear reactors, and industrial furnaces (up to 1,200°C). To safeguard their metallurgical integrity and dimensional stability during transit, we deploy aerospace-certified packaging systems and thermal-controlled logistics adhering to AMS 5596, NACE MR0175, and ISO 9328-2 standards.

Anti-rust packaging
VCI gas phase anti-rust film + desiccant (12 months moisture-proof for sea transportation)

Reinforcement method
Steel strapping + wooden pallet (load-bearing ≤ 5 tons)

Surface protection
Polyethylene film layered isolation (anti-scratch)

Customization options
IPPC fumigation wooden box (compliant with ISPM15 standard)
High Temperature Alloy Plate (Inconel®, Hastelloy®, Haynes®, etc.) Shipping



Sea transport
40HQ container (loading capacity 28 tons) / bulk carrier (LCL minimum 1 ton)
Air transport
reach major airports around the world within 7 days (DDP/DAP terms)
Land transport
door-to-door within China (qualification for dangerous goods transportation)
Our Services
We guarantee global door-to-door delivery within 7–15 business days via partnerships with DHL, Maersk, and UPS.
Why Choose Us?
Where Precision Meets Partnership,25 years of focus on metal material science,Not only a supplier, but also your engineering consultant,Fast and zero compromise,Sustainable trust cycle。
Full specifications and customization
Unlimited size, support non-standard cutting. Multiple surface treatments.
Professional capabilities
25 Years Of Focus On Metal Materials Science
Certification & Quality Assurance
Products comply with international standards such as ASTM, EN, JIS, etc., and are 100% tested from raw materials to finished products
Fast delivery & global supply
Global urgent orders are delivered within 15 days. One-stop service
FAQ
Q1: How does Inconel 718 compare to Haynes 230 in high-temperature service?
A: Inconel 718 offers higher tensile strength (1,400 MPa) below 650°C (1,202°F), while Haynes 230 excels in oxidation resistance above 1,000°C (1,832°F).
Q2: What welding methods prevent sigma phase formation?
A: Use TIG (GTAW) with ERNiCrMo-3 filler, limit heat input to **≤1.5 kJ/mm**, and post-weld heat treat at 1,100°C (2,012°F) for Inconel 601.
Q3: Are plates certified for aerospace engines?
Full compliance includes:
- AMS 5599/AMS 5662 (Aerospace Material Specifications)
- ASME Section III Nuclear Components
- NACE MR0175/ISO 15156
Q4: What’s the minimum order quantity (MOQ)?
Standard stock: 1 ton MOQ.
Custom sizes/tempers: 5 tons MOQ (lead time 35 days).
Q5: How to validate material authenticity?
Scan QR codes with AlloyGuard™ app to access:
- XRF validation against PMI certificates
- Third-party SGS/BV test reports
- Blockchain-validated EN 10204 3.1/3.2 certifications
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