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Inconel 718

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Published: 01 January 1986
Fig. 10 X-ray elastic constant determination for Inconel 718, (220) planes. Δψ = 45°, d o = 1.1272Å More
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Published: 01 June 2016
Fig. 10 Transformation diagram for vacuum-melted and hot-forged Inconel 718 bar. Source: Ref 12 More
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Published: 01 June 2016
Fig. 30 Effect of forging temperature on direct-age-processed Inconel 718. (a) At room temperature. (b) At 650 °C (923 K). Source: Ref 39 More
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Published: 01 June 2016
Fig. 20 Transformation diagram for vacuum-melted and hot-forged Inconel 718 bar. Source: Ref 12 More
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Published: 01 June 2016
Fig. 38 Typical properties of Inconel 718 as a function of processing. (a) Ultimate tensile strength. (b) Rupture stress. (c) Fatigue at 540 °C (1000 °F). Source: Ref 24 More
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Published: 01 January 1990
Fig. 4 Transformation diagram for vacuum-melted and hot-forged Inconel 718 bar. Source: Ref 8 More
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Published: 01 January 2000
Fig. 7 Method of creating master Larson-Miller curve for Inconel 718 from experimental stress-rupture curves More
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Published: 01 January 1996
Fig. 25 Crack growth rates in TMF OP and TMF IP cases for Inconel 718. Source: Ref 177 More
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Published: 01 January 1989
Fig. 2 Drill time with a Nd:YAG laser. Workpiece: Inconel 718; pulse energy, 40 J More
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Published: 01 January 1989
Fig. 5 Inconel 718 chips formed at increasingly higher cutting speed. Units are given in surface feet per minute. Source: Ref 1 More
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Published: 01 December 2004
Fig. 13 Transverse section of an as-forged billet of UNS N07718 (Inconel 718) alloy. The rim of coarse grains was produced by hammer blows during finish rounding. Etchant: 1 to 1 HCl in water. Courtesy of F. Warmuth, Warmuth-Gordon More
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Published: 01 December 2004
Fig. 39 Inconel 718 (UNS N07718) heat treated 100 h at 870 °C (1600 °F) to produce needlelike orthorhombic Ni 3 Nb. (a) Bright-field illumination. (b) Differential interference-contrast illumination. Particles in relief in (b) are niobium carbides; particles flush with the surface are niobium More
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Published: 31 December 2017
Fig. 4 Boride layers in Inconel 718: (a) borided at 760 °C (1400 °F) for 16 h in low B content powder, (b) borided at 800 °C (1470 °F) for 8 h in low B content powder, (c) borided at 800 °C for 8 h in high B content powder, (d) borided at 760 °C for 32 h in low B content powder, (e) borided More
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Published: 01 January 1996
Fig. 3 Effect of precipitate and grain size on FCP rates in Inconel 718 tested in air at 425 °C (800 °F), R = 0.05, 0.33 Hz. (a) Fine grain; underaged versus overaged. (b) Coarse grain; underaged versus overaged. (c) Underaged; fine grain versus coarse grain. (d) Overaged; fine grain versus More
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Published: 01 November 1995
Fig. 55 Typical thermal cycles for sealing glass-ceramics to Inconel 718 and Hastelloy C276 (a) and for sealing glass-ceramics to stainless steel and copper (b) More
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Published: 01 August 2018
Fig. 7 Inconel 718 turbine blade manufactured using AM and inspected by neutron radiography. (a) Two-dimensional radiograph. (b) Volumetric reconstruction. (c) Transverse reconstruction slices. Source: Ref 30 More
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Published: 01 January 2002
Fig. 46 Scanning electron micrographs of the fracture surfaces of Inconel 718 specimens tested at room temperature. (a) Δ K = 30 MPa m (27 ksi in. ), striation spacing ∼0.2 μm, and da / dN ∼ 0.1 μm/cycle. Arrow indicates direction of crack propagation. (b) Δ K = 14 MPa More
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Published: 01 January 1989
Fig. 13 Surface characteristics of cast Inconel 718 (aged, 40 HRC) produced by EDM. (a) Finishing conditions produced a variable recast layer 0.005 mm (0.0002 in.) thick. 860×. (b) Roughing conditions produced an extensively cracked variable recast layer up to 0.05 mm (0.002 in.). The random More
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Published: 01 January 1989
Fig. 15 Surfaces from the laser beam drilling of Inconel 718 shown at magnifications of 185× (a) and 1160× (b). Note the grain structure in the heat-affected zones of the entrance (A) and the exit (B). Source: Ref 9 More
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Published: 01 January 1989
Fig. 25 Effect of EDM and grinding on the fatigue strength of Inconel 718. Fatigue tests involved cantilever bending at room temperature and zero mean stress. Source: Ref 9 More