| The Super Alloys management team are amongst the most experienced professionals in the market. Supported by professional metallurgists and technicians, Super Alloys not only provide access to the largest range of high-tec metals in Europe, but also access to the broadest range of expertise. The unique combination of access to stock, expertise and rapid delivery reduces lead times and can eliminate costly production delays. The Super Alloys range of materials includes: • Titanium Alloys • Nickel Alloys • Steels Nickel Alloy 718 Nickel Alloy 718 is a precipitation hardenable nickel-chromium alloy. It combines high strength in the aged condition with good corrosion resistance and weldability. 718 NACE indicates material stocked in the heat treated condition to have high strength and meet the maximum hardness (40 Rockwell C) requirements of the NACE MR0175, MR0103, ISO 15156-3 specifications for use in oil tools used for sour service. Features of Nickel Alloy 718 The key features of Nickel Alloy 718 include: • Highly resistant to chloride and sulfide stress corrosion cracking • High strength in the aged condition • Good corrosion resistance Performance Profile for Nickel Alloy 718 Nickel Alloy 718 is a precipitation hardenable nickel-chromium alloy. It combines high strength in the aged condition with good corrosion resistance and weldability. 718 NACE indicates material stocked in the heat treated condition to have high strength and meet the maximum hardness (40 Rockwell C) requirements of the NACE MR0175, MR0103, ISO 15156-3 specifications for use in oil tools used for sour service. Applications of Nickel Alloy 718 Typical Applications for the Nickel Alloy 718 include: • Valves • Well head completion equipment • Fasteners • Blow out preventers (BOPs) • Tubing hangers • Mandrels Composition of Nickel Alloy 718 The composition range for Nickel Alloy 718 is provided in table 1. Table 1. Composition of nickel alloy 718. | | | Nickel | 50.0 | 55.0 | | Chromium | 17.00 | 21.00 | | Molybdenum | 2.80 | 3.30 | | Carbon | - | 0.045 | | Columbian + Tantalum | 4.87 | 5.20 | | Manganese | - | 0.35 | | Silicon | - | 0.35 | | Phosphorus | - | 0.010 | | Sulfur | - | 0.010 | | Copper | - | 0.230 | | Cobalt | - | 1.00 | | Lead | - | 10 ppm | | Selenium | - | 5 ppm | | Bismuth | - | 30 ppm | | Magnesium | - | 60 ppm | | Iron | - | remainder | Specifications The various forms of nickel alloy 718 are covered by the following standards: • API 6A • API 6A718 • NACE MR0175, MR0103 • ISO 15156-3 • ASTM B 637 Heat Treatments 718 NACE is annealed between 1875-1925°F and water quenched. Subsequently it is aged in the range of 1425°-1475°F for 6-8 hours and air cooled or faster to room temperature. Physical Properties of Nickel Alloy 718 | Density: | 0.297 lb/inch3 | | Melting Range: | 2160 - 2449°F | Thermal Properties of Nickel Alloy 718 The thermal properties of Nickel Alloy 718 are summarised in table 2. Table 2. Thermal properties of Nickel Alloy 718. | | | 70 | - | 6.4 | 29.0 | | 200 | 7.3 | 7.2 | 28.4 | | 400 | 7.5 | 8.2 | 27.6 | | 600 | 7.7 | 9.3 | 26.7 | | 1000 | 8.1 | 11.3 | 24.8 | | 1200 | 8.4 | 12.3 | 23.7 | Typical Mechanical Properties of Nickel Alloy 718 The minimum mechanical properties of nickel alloy 718 are provided in table 3. Table 3. Minimum specified properties of nickel alloy 718, solution annealed and aged condition. | | | Ultimate Tensile Strength | 150 ksi | - | | 0.2% Yield | 125 ksi | 145 ksi | | Elongation | 20% | - | | Reduction of Area | 35% | - | | Impact Strength*
Min Average/Min Single | 40/35 ft-lbs | - | | Hardness | 32 RC | 40 RC | * Charpy V notch impact test performed at -75 ˚F |