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Nickel alloys can offer enhanced corrosion resistance, toughness, strength at high and low temperatures, and interesting magnetic, thermal and electronic properties compared with other metals. Due to their higher nickel content compared with stainless steels, they can be appreciably more expensive, but find uses in more demanding applications from gas turbines to chemical plants and oil & gas industry components.
Nickel – copper alloys such as Alloy 400 and Alloy K-500, also known as Monel K500, (Special Metals Corporation’s family of Nickel-Copper alloys is known as Monel®) are based predominantly on nickel and copper, with smaller additions of manganese and iron. They are used where a higher strength is required compared to pure nickel, and resist corrosion in a wide range of environments. They can be fabricated readily by hot and cold working, machining, and welding. Nickel-Copper alloys find wide application in oil refining and marine applications where long corrosion-free life is required. Due to the good thermal conductivity of the alloys, they are also frequently used for heat exchangers where sea water is one of the fluids concerned.
Nickel-Iron-Chromium alloys such as Alloy 825, also known as Incoloy 825, (Special Metals Corporation’s family of Nickel-Iron-Chrome alloys is known as Incoloy® ) were developed to provide a more cost-effective solution for applications requiring high-temperature and corrosion resistance – achieved by lowering the nickel content. Selectively alloying with other elements can greatly improve their performance in certain environments. For instance, Alloy 825 also contains molybdenum and copper to improve resistance to strongly reducing environments, such as those containing sulphuric and phosphoric acids.
Nickel-Chromium super alloys such as Alloy 625, also known as Inconel 625, and Alloy 718, also known as Inconel 718, (Special Metals Corporation’s family of Nickel-Chromium alloys is known as Inconel®) are typically used in high-temperature applications. When heated, they form a thick and stable passivating oxide layer protecting the surface from further attacks. These alloys retain their strength over a wide temperature range, particularly at elevated temperatures where aluminium and steel would otherwise succumb to creep failure. Varying levels of high-temperature strength can be developed by solid solution strengthening or precipitation strengthening (with niobium additions).
Alloy | Common Name | Related Specifications | Tensile Strength | Proof Test | Elongation | ||
British | European | United States | N/mm2 (ksi) | N/mm2 (ksi) | (%) | ||
Alloy 400 | UNS N04400 | BS 3076 NA13 | 2.4360 | ASTM A164 UNS N04400, N04405 QQ - N - 281 | 483 (70) | 172 (25) | 35 |
Alloy K500 | UNS N05500 | BS3076 NA18 | 2.4375 UNS N05500 | ASTM B865 | 965 (140) | 724 (105) | 20 |
Alloy 625 (AMS5666) | UNS N06625 | BS 3076 NA21 | 2.4856 | ASTM B564 SAE AMS 5666 ASTM B466 UNS N06625 Nace MR01-75 / ISO 15156 ASME SB466 | 830 (120) | 415 (60) | 30 |
Alloy 718 | UNS N07718 | 2.4668 | ASTM B637 UNS N07718 API 6CRA 718 NACE MR 01-75 / ISO 15156-3 | 1138 (165) | 965 (140) | 20 | |
Alloy 725 | UNS N07725 | ASTM B637 UNS N07725 API 6CRA 725 | 1137 (165) | 827 (125) | 20 | ||
Alloy 825 | UNS N08825 | BS 3076 NA16 | 2.4858 NFe 32 C 20 DU NiCr 21 Mo | ASTM B425 UNS N08825 API 6CRA 825 | 590 (85) | 220 (32) | 30 |
Alloy 825 (Tube) | UNS N08825 | BS 3076 NA16 | 2.4858 NFe 32 C 20 DU NiCr 21 Mo | ASTM B425 UNS N00825 API 6CRA 825 | 518 (75) | 241 (35) | 30 |
Alloy 825 HS110 | UNS N08825 110ksi | BS 3076 NA16 | 2.4858 NiCr 21 Mo NFe 32 C 20 DU | ASTM B425 UNS N08825 API 6CRA 825 | 793 (115) | 758 (110) | 30 |
Alloy 925 | UNS N09925 | UNS N09925 | ASTM B805 API 6A CRA NACE MR0175-3 API 6CRA 925 | 965 (140) | 758 - 965 (110 - 140) | 18 |
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Up to 40 sizes per alloy available
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