| Brand Name: | DLX |
| Model Number: | GH4098 |
| MOQ: | 5kg |
| Payment Terms: | L/C,D/A,D/P,T/T,VTB |
| Supply Ability: | 1200 tons per month |
Engineered for extreme thermal environments, our 5mm GH4098 heat resistant nickel alloy plate delivers unmatched creep rupture strength, hot corrosion resistance, and structural stability up to 1050°C. Custom dimensions, precision cutting, and specialized surface finishes available.
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High temperature engine components, gas turbine flame rings, and aerospace exhaust structures operate under extreme mechanical stress, localized vibration, and continuous hot gas corrosion. Standard stainless steels and basic nickel alloys experience microstructural degradation, rapid thermal fatigue, and catastrophic creep deformation above 850°C.
Our 5mm GH4098 heat resistant nickel alloy plate solves these high-stress challenges through an engineered balance of tungsten, molybdenum, aluminum, and titanium. These alloying elements create dense, stable gamma-prime intermetallic precipitates that pin grain boundaries, preventing structural sagging, grain coarsening, and micro-cracking across prolonged exposure to operating temperatures up to 1050°C.
Manufactured via continuous Vacuum Induction Melting followed by Electroslag Remelting (VIM + ESR), our GH4098 heat resistant nickel alloy plates maintain ultra-low gas content, zero non-metallic inclusions, and uniform isotropic mechanical properties across all rolling directions. Advanced hot pack rolling, precision cold finishing, and computerized roller leveling ensure tight thickness tolerances, minimal internal residual stress, and optimal flatness for automated laser cutting and deep forming.
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| Parameter | Standard Value / Specification Range |
|---|---|
| Material Grade | GH4098 / High-Strength Precipitation-Hardening Nickel Superalloy |
| Nominal Thickness | 5.00mm (Custom precision thickness from 1.0mm to 25.0mm available) |
| Standard Width & Length | 1000×2000mm, 1219×2438mm, 1500×3000mm (Custom cut-to-size available) |
| Delivery Condition | Solution Treated (Bright Annealed / Descaled & Pickled / Precision Ground) |
| Major Chemical Elements (wt%) | Ni (Bal), Cr (17.5-19.5%), Co (5.0-8.0%), W (5.5-7.0%), Mo (3.5-5.0%), Al (2.5-3.2%), Ti (1.0-1.6%) |
| Trace Element Control | C (0.08-0.15%), Fe (<= 2.0%), B (<= 0.010%), Ce (<= 0.020%), Ultra-low P/S/Pb |
| Density | 8.45 g/cm³ |
| Melting Range | 1320°C to 1365°C |
| Thermal Conductivity | 12.8 W/(m·K) at 100°C | 24.6 W/(m·K) at 900°C |
| Tensile Strength (Rm at 20°C) | >= 1050 MPa |
| Yield Strength (Rp0.2 at 20°C) | >= 700 MPa |
| Elongation (A5 at 20°C) | >= 18% |
| High-Temp Tensile Strength (900°C) | >= 480 MPa |
| Creep Rupture Life (900°C / 180 MPa) | >= 40 Hours |
| Hardness Range | 280 - 340 HBW (Fully Heat Treated State) |
| Ultrasonic Inspection Level | 100% Volumetric Ultrasonic Testing (Class A Internal Soundness) |
The high-density precipitation of gamma-prime phases combined with refractory solid-solution strengthening from tungsten and molybdenum provides exceptional creep rupture life. It maintains dimensional geometry and load-bearing strength under continuous mechanical stresses at temperatures ranging from 900°C to 1050°C.
A high chromium and aluminum matrix promotes the rapid formation of a self-healing, adherent chromia-alumina protective barrier. This surface scale resists hot sulfur gases, cyclic thermal oxidation, and high-velocity gas erosion typical of aircraft propulsion exhausts and industrial combustors.
Utilizing VIM + ESR dual-vacuum melting, our GH4098 plates feature exceptional chemical homogeneity and ultra-clean grain boundaries. The absence of macro-segregation and brittle intermetallic phases eliminates premature fatigue cracking during cyclic thermal shock.
Advanced multi-roll tension leveling ensures superior flatness and balanced residual stress distribution. This dimensional stability guarantees accurate CNC machining, clean laser/waterjet cutting, and minimal distortion during subsequent welding and heat treatment.
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Serves as the primary structural material for combustion chamber outer shells, turbine exhaust nozzle fairings, afterburner heat shields, and turbine casing reinforcement rings requiring high-temperature strength and thermal fatigue resistance.
Applied in heavy-duty gas turbine transition ducts, combustor flame tubes, stator shroud segments, and exhaust diffuser housings subjected to continuous thermal cycling and high-velocity gas flows.
Utilized for furnace muffles, radiant tube baffles, high-temperature heat treatment fixture plates, and structural load-bearing components operating in oxidizing and carburizing atmospheres.
Deployed in nuclear thermal exchange plates, coal gasification reactor internal components, and petrochemical pyrolysis furnace supports requiring high creep rupture limits.
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DLZ controls the entire production chain from vacuum induction melting (VIM) and electroslag remelting (ESR) to hot rolling, cold finishing, precision leveling, and heat treatment. This integrated workflow ensures tight control over chemical purity, microstructure, and batch-to-batch consistency.
Equipped with high-precision fiber laser cutting, CNC abrasive waterjet cutting, and heavy-duty shearing lines, DLZ provides cut-to-size plates, custom CAD blanks, and edge-beveled profiles tailored to client engineering drawings to minimize customer fabrication scrap.
With a robust manufacturing capacity of 1,200 tons per month across superalloy and nickel alloy product lines, DLZ supports dynamic MOQs for qualification prototyping as well as stable, continuous supply for international tier-one aerospace and industrial OEMs.
Every plate is tested in our in-house metallurgical laboratory. Deliverables include full chemical analysis via direct-reading spectrometry, room- and high-temperature tensile verification, micro-hardness mapping, metallographic grain structure assessment, and 100% Class A ultrasonic non-destructive testing.
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Standard nickel-chromium solid-solution alloys soften and lose mechanical strength rapidly above 800°C. GH4098 contains high additions of aluminum, titanium, tungsten, and molybdenum, creating a dense precipitation-hardened matrix that provides superior yield strength and creep rupture endurance up to 1050°C.
Through precision rolling and computerized tension leveling, our 5mm GH4098 heat resistant nickel alloy plates achieve thickness tolerances within +/- 0.05mm and a flatness deviation of less than 2mm per meter, ensuring seamless integration into automated laser cutting and CNC machining centers.
The standard treatment involves solution annealing at 1140°C to 1180°C followed by rapid air cooling, and a subsequent multi-step precipitation aging treatment at 760°C to 800°C to achieve maximum gamma-prime phase strengthening and high-temperature creep resistance.
Yes. We offer custom-sized rectangular plates, circular blanks, perforated baffle plates, and beveled weld-ready edges utilizing advanced CNC waterjet and laser profiling based on your engineering CAD/DXF specifications.
Every batch is accompanied by comprehensive quality verification reports, including chemical composition certificates, room-temperature and elevated-temperature mechanical test data, microstructural grain size assessments, and non-destructive ultrasonic flaw detection reports.
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