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Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0005337
EISBN: 978-1-62708-187-0
... the product applications of titanium alloy castings. The tensile properties, standard industry specifications, and chemical compositions of various titanium alloy castings are tabulated. titanium alloy castings titanium casting chemical composition corrosion resistance hot isostatic pressing...
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001082
EISBN: 978-1-62708-162-7
...-6AI-4V alloy. It also talks about the chemical milling and weld repair, and describes the product applications of titanium alloy castings. Tensile properties, standard industry specifications, and chemical compositions of various titanium alloy castings are tabulated. alloy types casting design...
Series: ASM Handbook
Volume: 23A
Publisher: ASM International
Published: 12 September 2022
DOI: 10.31399/asm.hb.v23A.a0006857
EISBN: 978-1-62708-392-8
... directly. In this article, the processing of titanium and its alloys by PBF and DED is described, with a specific focus on their use in biomedical devices. The article then covers the density and mechanical properties of both commercially pure titanium and titanium-aluminum-vanadium alloy. Lastly...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006263
EISBN: 978-1-62708-169-6
... Abstract This article provides a detailed discussion on the heat treatment processes for titanium and titanium alloys. These processes are age hardening, solution treatment, aging, and annealing. The article illustrates the characteristics of equilibrium phase diagrams that are important...
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Published: 01 December 2004
Fig. 22 Titanium alloy brazed with an aluminum-silicon brazing alloy. As-polished and vapor deposited with zirconium dioxide. 500×. (R. Crouse) More
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Published: 01 January 1987
Fig. 87 Furrow-type fatigue fracture in a commercially pure titanium alloy IMI 155 tested at room temperature in laboratory air. Δ K = 16 MPa m (14.5 ksi in. ), da/dN = 10 −8 m/cycle. Source: Ref 236 More
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Published: 01 January 1987
Fig. 29, 30 Stress-corrosion fracture in a specimen of the same annealed titanium alloy Ti-8Al-1Mo-1V shown in Fig. 21, 22 23, 24 25, 26 27, 28 . This specimen was subjected to a maximum stress of 170 MPa (25 ksi) while exposed to an environment of 3.5% NaCl in water at room temperature More
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Published: 01 January 1987
Fig. 1141 Fracture surface of a ductile fracture-toughness specimen of titanium alloy Ti-6Al-4V that was solution treated for 40 min at 830 °C (1525 °F), water quenched, aged at 510 °C (950 °F), then loaded in three-point bending (in air). See also Fig. 1142 , 1143 , 1144 , and 1145 . SEM More
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Published: 01 January 1987
Fig. 1150 Fracture surface of a fracture-toughness specimen of titanium alloy Ti-6Al-4V that was heat treated for 40 min at 955 °C (1750 °F), stabilized and then tested at 25 °C (77 °F) in hydrogen. (Stabilizing consisted of furnace cooling to 704 °C (1300 °F) from the heat-treating More
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Published: 01 January 1987
Fig. 1154 Fracture surface of a fracture-toughness specimen of titanium alloy Ti-6Al-4V heat treated 40 min at 955 °C (1750 °F) and water quenched, aged at 510 °C (950 °F), and tested in hydrogen. (Structure is continuous β phase with dispersed α phase.) The fatigue-precrack region is at left More
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Published: 01 January 1987
Fig. 1155 Fracture surface of a fracture-toughness specimen of titanium alloy Ti-6Al-4V heat treated 40 min at 1040 °C (1900 °F), stabilized, and then tested in air at 25 °C (77 °F). (Stabilizing consisted of furnace cooling to 704 °C (1300 °F) from the heat-treating temperature, holding 1 h More
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Published: 01 January 1987
Fig. 1156 Fracture surface of a specimen of titanium alloy Ti-6Al-4V mill-annealed sheet that was fracture-toughness tested in air. (Structure is continuous α phase with dispersed β phase.) At left (dark) is fatigue-precrack region; at right is region of tensile-overload fracture, which More
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Published: 01 January 1987
Fig. 1165 Tensile-overload fracture surface of a notched specimen of titanium alloy Ti-6Al-4V heat treated to the same mechanical properties as specimen in Fig. 1162 and with a notched tensile strength of 1696 MPa (246 ksi). Crack nucleus is below center, at right. See also Fig. 1166 . 9× More
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Published: 01 January 1987
Fig. 1168 Fracture surface of a specimen of titanium alloy Ti-6Al-4V (same mechanical properties as in Fig. 1162 ) broken in low-cycle fatigue (26,000 cycles) in tension-tension ( R = 0.1) at maximum loading of 689 MPa (100 ksi). Several crack origins are visible at bottom. See also Fig More
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Published: 01 January 1987
Fig. 1171 Highly-cycle fatigue fracture in a specimen of titanium alloy Ti-6Al-4V (same mechanical properties as in Fig. 1162 ) that was tested in tension-tension ( R = 0.1) at maximum loading of 345 MPa (50 ksi), breaking in 937,000 cycles. The curved fatigue beach mark can be seen near More
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Published: 01 January 1987
Fig. 1176 Bending fracture in a specimen of titanium alloy Ti-6Al-4V that broke by stress-corrosion cracking in 3.5% NaCl (areas A), but that also exhibits regions of stretching (areas B) and a step containing what appear to be dimples (arrow at C). TEM p-c replica, 2000× More
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Published: 01 January 1987
Fig. 1177 Surface of a fracture in a specimen of titanium alloy Ti-7Al-1Mo-1V that was broken in a drop-weight tear test, consisting mostly of dimples. A feature that apparently is a tear ridge (vertical) is visible at far right. TEM p-c replica, 2000× More
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Published: 01 January 1987
Fig. 1178 Fracture produced by tension over-load in a specimen of titanium alloy Ti-7Al-2Nb-1Ta, showing staining and very large dimples. Vertical band at center is where crack initiated at a second-phase region and propagated to left and right. TEM p-c replica, 6000× More
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Published: 01 January 1987
Fig. 1180 Cleavage fracture in a specimen of titanium alloy Ti-7Al-2Nb-1Ta, produced by stress-corrosion cracking in methanol. Note the regular array of fissures, which are parallel to the crack front. See also Fig. 1181 . TEM p-c replica, 2000× More
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Published: 01 January 1987
Fig. 1182 Cleavage fracture in another specimen of titanium alloy Ti-7Al-2Nb-1Ta, also produced by stress-corrosion cracking in methanol. Note the similarity of the cleavage facets here to those in Fig. 1179 , which were produced in distilled water. TEM p-c replica, 2000× More