SAE AMS 5666: 2016 [pdf] Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, Extrusions, and Rings 62Ni – 21.5Cr – 9.0Mo – 3.65 Cb (Nb) Annealed, Revision H Shipping

Rundstång / AMS 5662 & AMS 5663: 3mm - 4mm - 7,5mm - 12,7mm - 15,88mm - 16mm - 20mm - 22mm - 25,4mm - 28,6mm - 30mm - 35mm 31,8mm - 41,28mm

Properties. Material. EOS NickelAlloy IN718 chemical composition corresponds to UNS N07718, AMS 5662, AMS. 5664, W.Nr 2.4668, DIN NiCr19Fe19NbMo3. This material is ideal ASTM B637, ASTM B670, AMS 5596, AMS 5597, AMS 5662,. AMS 5662, AMS 5664, GE B50TF14, GE B50TF15, PWA. 1009, PWA 1010, PWA 1033, UNS N06625, AMS 5599, AMS 5666,.

1 Nb+Ta I 5.24 1 t Ti .79 I in AMS 5662 (3.5.1.2.3.3): “The load required to produce an initial axial stress of 689 MPa (100 ksi) shall be used to rupture or for 23 hours, whichever occurs irst. After the 23 hours and at intervals of 8 hours minimum, thereafter, the stress shall be increased in increments of 34.5 MPa (5 ksi).” AMS 5662, AMS 5663, AMS 5664, AMS 5832, AMS 5962, ASME SB-637, ASTM B637, AWS A5.14, NACE MR0175 (ISO 15156-3). Typical Mechanical Properties – Spring Applications Condition Heat Treatment Tensile Strength Suggested Operating Conditions Annealed 1800oF (980oC) 115 – 145 ksi (790-1000 MPa) -330°F to 1200°F (-200°C to 650°C) Spring Temper SPS-M-275 718 Sol TR (AMS-5662) (Chems Only) SPS-M-637 718 Cold Reduced SPS-M-646 4MP 35N VOI SHAN: VS-71001 2Waspaloy Cold Reduced, (Exc. Hardness) DEPT OF DEFENSE: M254 (AMS 6304) 180,000 1000 plating required M INCONEL® 718 (AMS 5662) 180,000 1200 excellent NM 400 Series Stainless Steel 160,000 600 excellent M A286 (AMS 5853) 160,000 1000 excellent NM Titanium Alloy (AMS 4967) 160,000 500 excellent NM WASPALOY® (AMS 5708) 150,000 1600 excellent NM A286 (AMS 5731) 140,000 1200 excellent NM *Plus cold work A brief history of Inconel 718. Inconel 718 (® Special Metals) is a modern superalloy, first patented on July 24th, 1962. The creation of this alloy was a direct offshoot of nearly a decade of research to create a Nickel Chromium Molybdenum Niobium (Ni-Cr-Mo) superalloy – Inconel 625. as the following data indicate.

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Both alloys are widely used in the aerospace, chemical, petrochemical, food processing, paper and general in AMS 5662 (3.5.1.2.3.3): “The load required to produce an initial axial stress of 689 MPa (100 ksi) shall be used to rupture or for 23 hours, whichever occurs irst. After the 23 hours and at intervals of 8 hours minimum, thereafter, the stress shall be increased in increments of 34.5 MPa (5 ksi).” AMS 5662, AMS 5663, AMS 5664, AMS 5832, AMS 5962, ASME SB-637, ASTM B637, AWS A5.14, NACE MR0175 (ISO 15156-3). Typical Mechanical Properties – Spring Applications Condition Heat Treatment Tensile Strength Suggested Operating Conditions Annealed 1800oF (980oC) 115 – 145 ksi (790-1000 MPa) -330°F to 1200°F (-200°C to 650°C) Spring Temper AMS 5662 is a designation of Nickel Inconel 718, itself a nickel-chromium alloy with high strength, corrosion and oxidation resistance, and excellent tensile and impact strength at cryogenic temperatures..

Amsterdam, AMS. 63.6. Frankfurt 5,662. 3,163. Capitalized leasing costs, net. 21,210 19,754 17,535 14,287 11,970 10,654. 9,527 10,318

Chemical Composition. Chemical Element % Present; Nickel (Ni) AMS 5662, AMS 5663, AMS 5664, AMS 5832, AMS 5962, ASME SB-637, ASTM B637, AWS A5.14, NACE MR0175 (ISO 15156-3). Typical Mechanical Properties – Spring Applications Condition Heat Treatment Tensile Strength Suggested Operating Conditions Annealed 1800oF (980oC) 115 – 145 ksi (790-1000 MPa) -330°F to 1200°F (-200°C to 650°C) Spring Temper Alloy 718 Round Bar, Plate, Sheet and Coil - AMS 5596, 5662, N07718 AMS 5662 is an excellent choice for parts where there is a concern of rupture life, notch rupture life, and rupture ductility. Efficiency when welding is about 100% with the gas tungsten-arc process and using the proprietary Nickel Filler Metal 718. Nickel Inconel 718 AMS 5662 can be age-hardened directly, without stress relief. 15-5PH (AMS 5862) covers sheet, strip and plate (supplied in Cond A as standard).

It can be heat treated into AMS 5663; this heat treatment can be done in two ways to achieve specific outcomes such as optimum impact properties, or optimum tensile and creep-rupture properties.
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These values are properties specified for sheet, strip and plate in AMS 5596 and AMS 5597. Yield Strength Max (0.2% Offset) Ultimate Tensile Strength Max Elongation (% in 2”) Sheet and Strip 80,000 psi (550 MPa) 14,000 (965 MPa) 30 (min) Btu/(hr/ft²/in/°F) 30 (min) Solution Treatment (AMS 5662 Bar / AMS 5596 Sheet): 1725°F - 1850°F + Air Cool. Heat Treatment (AMS 5663 Bar) : 1325°F for 8 hrs, cooling 100°F/hr to 1150°F, hold at 1150°F for 8hrs min, + Air Cool .

32. AMS 5662, AMS 5664 AMS. DIN. Аналог. Металлопорошки на основе Ni и Co. LPW. CoCr-1LC +.
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buy sae ams 5661 : 2012 nickel-iron alloy, corrosion and heat resistant, bars, forgings, and rings - 42.5ni - 12.5cr - 5.8mo - 2.9ti - 0.015b - 35fe - consumable electrode or vacuum induction melted solution, stabilization, and precipitation heat treated from sai global

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AMS-5662 Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50AI - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenable

Chemical Composition, % AMS 5662 / AMS Solution Treatment (AMS 5662 Bar / AMS 5596 Sheet): 1725°F - 1850°F + Air Cool.

R4140. R4144. R3154. R6020. 1570390.