1-20 of 1916

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Published: 01 June 2016
Fig. 21 Effect of solution-treating temperature on the solution-treated and aged properties of Ti-6Al-4V. Age cycle: 540 °C (1000 °F) for 8 h More
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Published: 01 June 2016
Fig. 20 Effect of solution-treating temperature on the tensile properties of Ti-6Al-4V More
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Published: 01 June 2016
Fig. 26 Microstructures after solution treating below, near, and above the β-transus temperature; forged and aged prior to solution treatments. Etch: Kroll’s reagent. Ti-6Al-2Sn-4Zr-6Mo, β-transus temperature: 935 °C (1715 °F). Prior treatment: forged below β transus at 870 °C (1600 °F), water More
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Published: 01 June 2016
Fig. 8 Tensile properties of alloy QE22A-T6 as functions of solution-treating temperature. Data were obtained from test bars of casting alloy QE22A-T6 machined from 25 mm (1 in.) diam cast specimens. The bars were held at temperature for 4 h. More
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Published: 01 June 2016
Fig. 18 Fixture for solution treating and end quenching of 18 depleted uranium bars More
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Published: 01 June 2016
Fig. 61 Effect of stretching (after solution treating and quenching) on the number and size of precipitation platelets on aged 2024. All specimens aged 12 h at 190 °C (375 °F). (a) 2024-T6, no stretching after quenching. (b) 2024-T81 stretched 1.5% before aging, resulting in smaller and more More
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Published: 15 June 2020
Fig. 4 Example of a solution treating and aging cycle for Inconel 718 that uses a double aging treatment. Source: Ref 8 More
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Published: 01 January 1987
Fig. 42 Examples of TTS fracture in Ti-6Al-4V α-β alloys. (a) Solution treated and aged microstructure consisting of about 10-μm diam primary α particles in a matrix of about 70 vol% of fine Widmanstätten α and β. The microstructural constituents are not evident on the fracture surface More
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Published: 01 January 1987
Fig. 872 Fracture surface of a specimen of Duranickel, vacuum solution treated and quenched, aged 1 h at 500 °C (930 °F) and cooled in air. The specimen, which was notched, precracked, and slow-bend fracture-toughness tested in hydrogen, broke by combined cleavage and intergranular fracture More
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Published: 01 January 1987
Fig. 1088 Transgranular corrosion-fatigue crack propagation in a solution-treated and peak-aged Al-5.6Zn-1.9Mg sample tested in humid nitrogen gas. Compare with Fig. 1091 and 1092 . SEM, 5000× (R.E. Ricker, University of Notre Dame, and D.J. Duquette, Rensselaer Polytechnic Institute) More
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Published: 01 January 2002
Fig. 50 Stress-corrosion cracking of a solution-treated and aged Ti-6Al-4V Apollo service propulsion system (SPS) fuel pressure vessel during a system checkout test. Fluid test medium was methanol. (a) Cross section adjacent to weld in cracked vessel. 65×. (b) Another crack near the same weld More
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Published: 01 January 1990
Fig. 1 Aging curves for cast and solution-treated C81800 More
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Published: 01 January 1990
Fig. 2 Aging curves for cast and solution-treated C82000 More
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Published: 01 January 1990
Fig. 3 Hot hardness of C82000, TF00 temper. Cast specimens were solution treated, then aged at 480 °C (900 °F). Useful design range is up to about 400 °C (750 °F). More
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Published: 01 January 1990
Fig. 6 Aging curves for solution-treated C82500 or beryllium-copper alloy 21C More
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Published: 01 January 1990
Fig. 7 Hot hardness of C82500, TF00 temper. Specimens were solution treated, then aged at 345 °C (650 °F). More
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Published: 01 January 1990
Fig. 9 Aging curves for solution-treated C82800 More
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Published: 01 January 1990
Fig. 10 Hot hardness of 82800, TF00 temper. Specimens were solution treated, then aged at 345 °C (650 °F). More
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Published: 01 January 1989
Fig. 7 Effect of cutting speed and feed in the face milling of solution-treated and aged Ti-6Al-2Sn-4Zr-2Mo having 321 HB hardness. Feed rate: A, 0.25 mm/tooth (0.010 in./tooth) and B, 0.13 mm/tooth (0.005 in./tooth). The cutter was a 100 mm (4 in.) diam single-tooth face mill with a C-2 (883 More
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Published: 01 January 1989
Fig. 9 Effect of cutting speed and cutting fluids in drilling solution-treated and aged Ti-6Al-4V having 375 HB hardness. Cutting fluids, wear rates, and tool life: A, chemical emulsion (1:15), 0.15 mm (0.006 in.) wear at 13 m/min (43 sfm), 250 holes; B, heavy-duty soluble oil (1:15), 0.15 mm More