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Ti-6Al-4V
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in Wrought Titanium and Titanium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 24 Fracture toughness of Ti-6Al-4V castings compared to Ti-6Al-4V plate and to other Ti alloys. Sources: Ref 1 and 15
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in Mechanically Assisted Corrosion of Metallic Biomaterials
> Corrosion: Environments and Industries
Published: 01 January 2006
Fig. 7 SEM micrographs of Ti-6Al-4V/Ti-6Al-4V modular connections for a total hip replacement device from a retrieved device (due to ceramic head fracture). This modular connection consisted of a femoral neck taper onto which was placed a Ti-6Al-4V “thimble” to allow a ceramic head to attach
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Published: 31 December 2017
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Published: 01 December 1998
Fig. 5 Fracture toughness of Ti-6Al-4V castings compared with that of Ti-6Al-4V plate and of other titanium alloys
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Published: 01 June 2012
Fig. 7 SEM micrographs of Ti-6Al-4V/Ti-6Al-4V modular connections for a total hip replacement device from a retrieved device (due to ceramic head fracture). This modular connection consisted of a femoral neck taper onto which was placed a Ti-6Al-4V “thimble” to allow a ceramic head to attach
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in Titanium and Titanium Alloy Castings
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 11 Comparison of wrought (I/M) annealed Ti-6Al-4V scatterband with (a) Ti-6Al-4V investment castings subjected to various thermal and hydrogen treatments (see Table 5 ) and (b) heat-treated β titanium alloy castings. For data in (a), smooth axial fatigue measured at room temperature
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Published: 01 January 1996
Fig. 27 Notch effects on (a) Ti-6Al-4V and (b) Ti-10V-2Fe-3Al. Source: MIL HDBK-697A, 1974, and Ref 40
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Published: 01 January 2005
Fig. 10 Highly configured (twisted) alloy Ti-6Al-4V and alloy Ti-8Al-1Mo-1V turbine engine fan and compressor blades that were forged in screw presses
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Published: 01 January 1993
Fig. 6 Microstructure of Ti-6Al-4V joint vacuum-brazed using BTi-1 (Ti-15Cu-15Ni wt%) brazing foil. Original magnification: 200×. Source: Ref 19
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Published: 01 January 1994
Fig. 5 Surgical prostheses of Ti-6Al-4V alloy of types being commercially ion implanted for wear benefits
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Published: 01 January 1994
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Published: 01 January 1994
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Published: 01 January 1994
Fig. 6 Influence of feed rate on hardness profile for laser gas nitrided Ti-6Al-4V, 6.6 × 10 4 W/cm −2 , 40:60 N2:Ar, 75% track overlap. Source: Ref 15
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Published: 01 January 1994
Fig. 8 Hardness profile from electron beam SiC alloyed Ti-6Al-4V after surface grinding to remove rippling. Source: Ref 16
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Published: 01 January 1994
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in Introduction to Titanium and Titanium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 4 Forged Ti-6Al-4V jet engine fan disks are 890 mm (35 in.) in diameter and weigh 249 kg (548 lb). Courtesy of Wyman-Gordon Company
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in Wrought Titanium and Titanium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
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in Wrought Titanium and Titanium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 13 Microstructures of alloy Ti-6Al-4V after cooling from different areas of the phase field shown in (a). The specimens represented in micrograph (e) provided the best combination of strength and ductility after aging. See the text and Table 9 . Etchant: 10 HF, 5 HNO 3 , 85 H 2 O. All
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in Wrought Titanium and Titanium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 19 Forging pressure and flow stress of Ti-6Al-4V. (a) Effect of die temperature at various strain rates. (b) Effect of grain size distribution on flow stress versus strain rate data for Ti-6Al-4V at 927 °C (1700 °F). Lot A, average grain size of 4 μm and grain size range of 1 to 10 μm
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in Wrought Titanium and Titanium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 25 LCF life of Ti-6Al-4V alloy with different structures: beta forged (100% transformed beta); 10% primary alpha (balance transformed beta); 50% primary alpha
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