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High-Temperature Resistant Inconel 617 Plate for Industrial Furnace & Aerospace Applications

Luogo di origine CINA
Marca DELTA
Certificazione ISO
Numero di modello Inconel 617
Quantità di ordine minimo 500 kg
Prezzo 40-45 USD/Kg
Imballaggi particolari imballaggio standard per l'esportazione
Tempi di consegna 5 - 12 giorni in base alla quantità
Termini di pagamento L/C, T/T, Western Union
Capacità di alimentazione 3 tonnellate a settimana

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Dettagli
Prodotti Lamierino & lamiera della lega di nichel Grado Inconel 617
Spessore 0.5 - 30.0mm Dimensioni standard 1000*2000mm 1219*2438mm
Standard Astm en Servizio TAGLIO
Porta di caricamento Shanghai Port Superficie 2B NO.1 NO.4 NO.8
Evidenziare

Inconel 617 high-temperature plate

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Nickel alloy aerospace plate

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Industrial furnace resistant plate

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High-Temperature Resistant Inconel 617 Plate for Industrial Furnace & Aerospace Applications

 

Products Specification

 

Products Name Inconel 617 Nickel Alloy Sheet Plate
Thickness Cold rolled: 0.5 - 3.0mm   Hot rolled 4.0 - 30.0mm
Standard Size 1000*2000mm 1219*2438mm 1219*3048mm 1500*6000mm
Surface 2B NO.1
MOQ 50 kgs
Service Cutting, Surface Finishing
Packing  Waterproof paper and wooden pallets
Loading Port Shanghai Port
Price term FOB  CFR CIF EXW
Payment term 30% TT in advance , 70% TT balance against copy of B/L
Other Grade Hastelloy C22 C4 X  C276
Monel 400 K500
Incoloy 800 800H 800HT 825  925
Inconel 600 601 617 625 716 718
Stainless  Steel Grade 201 202 301 304L 309S 310S 316L 316Ti 317L 321 347 409L 410 410S 420J1 420J2 430 431 436L 439 440A/B/C 441 443 444 2205 2507 904L 254SMO 253MA

 

High-Temperature Resistant Inconel 617 Nickel Alloy Plate for Industrial Furnace & Aerospace Applications


In the demanding realms of advanced industrial processing and aerospace engineering, materials are pushed to their absolute limits. Extreme temperatures, corrosive environments, and significant mechanical loads necessitate the use of superalloys capable of withstanding such punishing conditions. Inconel® 617 alloy plate stands as a premier solution in this arena. This nickel-chromium-cobalt-molybdenum alloy is specifically engineered to offer an exceptional combination of high-temperature strength, outstanding oxidation and carburization resistance, and excellent metallurgical stability. This document provides a detailed overview of Inconel 617 plate, its chemical composition, mechanical and physical properties, key characteristics, and its pivotal applications in industrial furnace and aerospace sectors.


1. Introduction to Inconel 617

Inconel 617 is a solid-solution strengthened, nickel-based superalloy. Its development was driven by the need for a material that could perform reliably in high-temperature environments where other alloys, such as stainless steels, would rapidly degrade. The "solid-solution" strengthening mechanism means that its high-temperature strength is derived from the deliberate addition of various alloying elements (like chromium, cobalt, and molybdenum) into the nickel matrix, which distorts the crystal lattice and impedes the movement of dislocations, thereby strengthening the material without the need for precipitation hardening heat treatments.

This alloy is particularly renowned for its ability to maintain integrity in temperatures ranging from 1000°C to 1200°C (1832°F to 2192°F). It is available in various forms, including plate, sheet, bar, and wire, with plate being the primary form for structural components in furnace construction and aerospace engines.

2. Chemical Composition

The superior properties of Inconel 617 are a direct result of its meticulously balanced chemical composition. Each element plays a critical role in the alloy's performance.

Table 1: Typical Chemical Composition of Inconel 617 (Weight %)

 
 
Element Percentage (%) Primary Function
Nickel (Ni) Balance Provides the austenitic matrix, ensuring ductility, toughness, and base corrosion resistance.
Chromium (Cr) 20.0 - 24.0 Confers exceptional resistance to oxidation and sulfidation by forming a protective, adherent Cr₂O₃ scale.
Cobalt (Co) 10.0 - 15.0 Enhances solid-solution strength at elevated temperatures and improves resistance to carburization.
Molybdenum (Mo) 8.0 - 10.0 Provides solid-solution strengthening and improves resistance to pitting and crevice corrosion.
Aluminum (Al) 0.8 - 1.5 Along with Chromium, forms a stable, self-healing Al₂O₃ layer for superior high-temperature oxidation resistance.
Carbon (C) 0.05 - 0.15 Enhances high-temperature creep strength through carbide formation.
Iron (Fe) ≤ 3.0 Residual element, kept low to prevent the formation of detrimental phases.
Silicon (Si) ≤ 1.0 Aids in oxidation resistance.
Manganese (Mn) ≤ 1.0 Aids in manufacturability and hot workability.
Boron (B) ≤ 0.006 Enhances creep ductility and strength by segregating to grain boundaries.
Titanium (Ti) ≤ 0.6 Contributes to strengthening.

3. Key Characteristics and Properties

3.1 Exceptional High-Temperature Strength
Inconel 617 retains a significant portion of its tensile and creep-rupture strength at temperatures exceeding 1000°C (1832°F). Its solid-solution strength, augmented by cobalt and molybdenum, allows it to withstand continuous mechanical loads where most other alloys would soften and fail. This makes it ideal for load-bearing components in high-heat environments.

3.2 Superior Oxidation and Corrosion Resistance
The synergistic effect of chromium and aluminum allows Inconel 617 to form a dense, continuous, and self-repairing layer of mixed chromium and aluminum oxides (Cr₂O₃ and Al₂O₃) on its surface. This layer acts as a barrier, drastically slowing down further oxidation, making it resistant to scaling in air environments up to 1150°C (2100°F). Furthermore, it exhibits excellent resistance to carburization (carbon absorption) and nitriding (nitrogen absorption), which are common failure mechanisms in hydrocarbon-rich furnace atmospheres.

3.3 Metallurgical Stability
Prolonged exposure to high temperatures can cause many alloys to become brittle through the precipitation of undesirable intermetallic phases. Inconel 617 is formulated for long-term stability, maintaining its ductility and toughness over extended service life, which is critical for component reliability and safety.

3.4 Good Fabricability
Despite its high strength, Inconel 617 plate can be hot-formed, machined, and welded using standard techniques, though they require more power and specialized parameters compared to stainless steels.

Table 2: Typical Room Temperature Mechanical Properties for Annealed Inconel 617 Plate

 
Property Typical Value Test Standard
Tensile Strength 710 MPa (103 ksi) ASTM E8
Yield Strength (0.2% Offset) 270 MPa (39 ksi) ASTM E8
Elongation (in 2 inches) 70% ASTM E8
Hardness (Rockwell B) 75 HRB ASTM E18

Table 3: Typical Physical Properties of Inconel 617

 
Property Value
Density 8.36 g/cm³ (0.302 lb/in³)
Melting Range 1332 - 1377°C (2430 - 2510°F)
Thermal Expansion Coefficient (20-1000°C) 14.0 μm/m·°C
Thermal Conductivity (100°C) 13.5 W/m·K
Specific Heat (100°C) 420 J/kg·K

4. Applications in Industrial Furnaces

The industrial furnace sector is a primary beneficiary of Inconel 617 plate's capabilities. Components are subject to radiant heat, aggressive atmospheres, and thermal cycling.

  • Radiant Tubes: Used in carburizing, neutral hardening, and annealing furnaces. The alloy's resistance to creep, oxidation, and carburization ensures long service life and consistent process quality.

  • Muffles and Retorts: These enclosures protect the workload from furnace gases. Inconel 617 prevents contamination and withstands the internal and external thermal gradients.

  • Fans and Impellers: For circulating high-temperature atmospheres within the furnace. The alloy's strength at temperature is crucial to prevent blade deformation and failure.

  • Fixtures, Baskets, and Trays: Used to hold components during heat treatment. They must not sag or corrode, ensuring the integrity of the workload and the furnace structure.

  • Heat Exchangers: For recovering waste heat from high-temperature furnace exhausts, improving overall system efficiency.

5. Applications in Aerospace

In the aerospace industry, the push for higher efficiency leads to higher operating temperatures in propulsion and power generation systems. Inconel 617 is a key material in several advanced applications.

  • Combustion Liners and Chambers: These components contain the burning fuel-air mixture in gas turbine engines. Inconel 617's strength and oxidation resistance at temperatures up to 1150°C make it a suitable candidate for sections of these highly stressed parts.

  • Afterburner Components: Parts of the afterburner system in military jets, where temperatures are extreme, benefit from the alloy's short-term high-temperature capability.

  • Turbine Stator Vanes: While not typically for the most highly-stressed rotating blades, it can be used for static vanes that guide airflow, requiring good creep and oxidation resistance.

  • Advanced Rocket Engine Components: Inconel 617 is considered for various structural and fluid-handling components in liquid-fueled rocket engines where cryogenic temperatures and high heat fluxes are encountered.

  • Heat Shields and Thermal Protection Systems: Its ability to form a stable oxide layer makes it useful for protecting sensitive structures from radiant and convective heat.

6. Fabrication and Handling of Inconel 617 Plate

Working with Inconel 617 requires an understanding of its characteristics.

  • Hot Forming: Forming should be performed in the range of 1175°C - 1230°C (2150°F - 2250°F). The material should then be rapidly cooled to retain its optimal properties.

  • Cold Forming: Possible but requires higher forces. Intermediate annealing may be necessary due to rapid work hardening.

  • Machining: It is a gummy and work-hardening material. Use positive rake angles, sharp and rigid tooling, slow speeds, and heavy feeds to shear the material beneath the work-hardened layer. Carbide tools are recommended.

  • Welding: Inconel 617 is readily weldable using common techniques like Gas Tungsten Arc Welding (GTAW/TIG) and Gas Metal Arc Welding (GMAW/MIG). Matching filler metal, such as ERNiCrCoMo-1, is typically used. Preheating is generally not required, and interpass temperature should be controlled below 150°C (300°F). Post-weld heat treatment is not usually necessary for stress-relief due to the alloy's high hot strength, but it can be applied for specific applications.

  • Heat Treatment: The standard heat treatment for Inconel 617 is a solution anneal at 1175°C (2150°F) followed by rapid cooling (water quench or fast air cool) to dissolve secondary phases and achieve optimal properties.

7. Comparison and Conclusion

When compared to other high-temperature alloys, Inconel 617 occupies a unique position. It offers a better combination of very high temperature strength and oxidation resistance than alloys like 800H/HT. While alloys like Haynes 230 may offer superior oxidation resistance at the very highest end of the temperature spectrum, Inconel 617 often provides a more favorable balance of cost, fabricability, and performance for a wide range of applications.

In conclusion, Inconel 617 nickel alloy plate is a versatile and highly reliable engineering material designed to overcome the most challenging thermal and corrosive environments. Its robust combination of mechanical strength, exceptional oxidation and carburization resistance, and long-term stability makes it an indispensable material for critical components in modern industrial furnaces and advanced aerospace systems. By enabling higher operating temperatures and longer service life, it contributes significantly to improved process efficiency, reduced maintenance downtime, and the advancement of high-performance technologies.

 

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