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Inconel Alloy 718 N07718 2.4668 Nickel Superalloy Wire

Inconel Alloy 718 N07718 2.4668 Nickel Superalloy Wire

Inconel Alloy 718 N07718 2.4668 Nickel Superalloy Wire

Inconel Alloy 718 N07718 2.4668 Nickel Superalloy Wire

With over 35 years of industry expertise, Fushun has the industry knowledge and resources to find you the metal products that you need for your specific industry applications. We are in stock and ready to quickly deliver hard-to-find metals. Our ISO 9001-certified metal supply is one of the most comprehensive selections on the market. We provide timely customer support and quick delivery on all quantities of our in stock products.

 

Contact us for more information regarding our nickel alloy manufacturing and distribution options.  Fushun is your trusted nickel alloy supplier for all types of Nickel alloy material.

Introduce

Inconel 718 is an age-hardenable Alloy-chromium alloy that combines corrosion resistance with high strength and good fabricability. It has high creep-rupture strength at temperatures up to 700 ℃. Its excellent relaxation resistance contributes to its application in springs.

Application

The alloy is used in jet engine and high-speed airframe parts such as wheels, buckets and spacers, and high-temperature bolts and fasteners. Inconel 718 is also used in the oil and gas drilling and production industries due to its high strength and resistance to chlorides, stress corrosion and sulfide stress cracking. Within these industries the alloy has been used for valves, pump shafts and wellhead components.

Heat-Treat Process

Inconel® 718 is typically purchased in the mill- or solution-annealed condition. In some instances, it has a stress-relief operation performed on it prior to fabrication and heat treatment. The solution anneal is followed by a precipitation (age) hardening step. Precipitation of secondary phases (e.g., gamma prime and gamma double-prime) into the metal matrix hardens the material. The precipitation of nickel-aluminum, nickel-titanium and nickel-niobium phases is triggered by aging in the temperature range of 600-815˚C (1100-1500˚F). The key to the heat-treatment process is to be sure these age-hardening constituents are fully in solution at high temperature (i.e., fully dissolved in the matrix), otherwise precipitation will not result in full strength.Two heat treatments are common (although slight temperature variations of these recipes are often employed).Solution anneal at 925-1010˚C (1700-1850˚F) followed by rapid cooling (usually in water). This is followed by precipitation hardening at 720˚C (1325˚F) for 8 hours, furnace cooling to 620˚C (1150˚F) and holding for 10 hours followed by air cooling.
Solution anneal at 1040-1065˚C (1900-1950˚F) followed by rapid cooling (usually in water). This is followed by precipitation hardening at 760˚C (1400˚F) for 10 hours, furnace cool to 650˚C (1200˚F) and holding for 10 hours followed by air cooling.Solution heat treatments are typically done in low-dew-point argon or vacuum furnaces, often with all-metal hot zones to avoid discoloration. The effect of annealing for 30 minutes on the grain size (Fig. 2) of sheet varies with temperature. Also, aging response of Inconel® 718 is rather slow in comparison with that of aluminum-titanium-hardened alloys. Thus, in most sizes, the alloy can be heated and cooled through the aging temperature range at normal speeds yet retain softness and ductility. The effect of aging time and temperature on the hardness of annealed sheet (Fig. 3) reflects this.

Standards

718 Sheet, Coil and Plate: UNS N07718, AMS 5596, ASTM B 670, ASME SB 670, B50TF14,

718 Round Bar: UNS N07718, AMS 5662, ASTM B 637, B50TF15, B50809D (Power Generation)

other:AMS 5662, AMS 5663, AMS 5832, AMS 5962, ASTM B637, GE B14H89, ISO 15156-3, (NACE MR 0175)

Density 8.19g/cm³ 0.296 lb/in³
Melting Point 1336°C 2437°F
Coefficient of Expansion 13.0 μm/m °C (20 – 100°C) 7.2 x 10-6 in/in °F (70 – 212°F)
Modulus of Rigidity 77.2 kN/mm² 11197 ksi
Modulus of Elasticity 204.9 kN/mm² 29719 ksi

 

Properties
Condition Approx. tensile strength Approx. operating temperature depending on load^^ and environment
N/mm² ksi °C °F
Annealed 800 – 1000 116 – 145
No 1 Temper 1000 – 1200 145 – 175
Spring Temper 1250 – 1550 180 – 225
No 1 Temper + Annealed + Aged 1250 – 1450 181 – 210 -200 to +550 -330 to +1020
No 1 Temper + Aged 1520 – 1720 220 – 250 Contact Alloy Wire Technical Dept
Spring Temper + Annealed + Aged 1250 – 1450 181 – 210 -200 to +550 -330 to +1020
Spring Temper + Aged 1700 – 1950 247 – 283 Contact Alloy Wire Technical Dept

Key Features

Good creep rupture strength at high temperatures

Higher strength than Inconel X-750

Better mechanical properties at lower temperatures than Nimonic 90 & Inconel X-750

Age hardenable

High temperature dynamic applications

Chemical Composition

Ni Fe Cr Cu Mo Nb C Mn P S Si Ti Al Co B
50.00-55.00 Remainder 17.00-21.00 .30 max 2.80-3.30 4.75-5.50 .08 max .35 max .015 max .015 max .35 max .65-1.15 .20-.80 1.00 max .006 max

Mechanical Properties

Condition Approx. tensile strength Approx. operating temperature depending on load^^ and environment
N/mm² ksi °C °F
Annealed 800 – 1000 116 – 145
No 1 Temper 1000 – 1200 145 – 175
Spring Temper 1250 – 1500 180 – 225
No 1 Temper + Annealed + Aged 1250 – 1450 181 – 210 -200 to +550 -330 to +1020
No 1 Temper + Aged 1520 – 1720 220 – 250 Contact Alloy Wire Technical Dept
Spring Temper + Annealed + Aged 1250 – 1450 181 – 210 -200 to +550 -330 to +1020
Spring Temper + Aged 1700 – 1950 247 – 283 Contact Alloy Wire Technical Dept

 

Heat Treatment of Finished Parts
Condition as supplied by Alloy Wire Type Temperature Time (Hr) Cooling
°C °F
No. 1 or Spring Temper Anneal
Age Harden
Total Age
980
720
620
1800
1330
1150
1
8
18
Air
Furnace
Air
No. 1 or Spring Temper
(for ISO 15156-3 / NACE MR 0175)
Anneal
Age Harden
1010
790
1850
1455
2
6
Air
Air
No. 1 Temper or Spring Temper Age Harden
Total Age
720
620
1330
1150
8
18
Furnace
Air

 

Quality & Testing

Fushun supply Certification with all shipments, containing full chemical analysis and also mechanical test results if requested.

 

All incoming material is visually inspected and PMI (Positive Material Identification) tested before processing begins and all our production material is checked during each stage of processing.

 

All incoming orders are produced to the individual customer specification, some of which may involve processing sample batches for testing prior to full production.

 

Final Inspection carried out on all finished material to include:

Visual inspection

Dimensional checks

PMI (Positive Material Identification)

Mechanical tests

 

Nickel Alloy Material Available Formats

Fushun offers pure Nickel alloy materials in a variety of forms, including:

Seamless & welded pipe

Seamless & welded tube

Bar

Wire

Sheet

Plate

Forgings

Pipe fittings

Flanges

Weld Rod

 

Nickel Alloy Supply Quantities for Single Items or Full Bills

At Fushun, we can supply single items or full bills of nickel alloy materials for most any project. No inquiry is too small. We offer quick responses to customer inquiries and specialize in the rapid delivery of both large and small quantities of nickel alloy products.

 

Contact Fushun for Nickel Alloy Materials Today

Contact us for more information regarding our nickel alloy material options, or request a quote for further pricing details today. Fushun is your trusted nickel alloy supplier and manufacturer of premium nickel alloy materials.

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