1-20 of 988 Search Results for

Ti-6Al-4V

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Image
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 More
Image
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 More
Image
Published: 31 December 2017
Fig. 7 Cumulative mass loss curves for Ti-6Al-4V and laser-nitrided Ti-6Al-4V. Source: Ref 22 More
Image
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 More
Image
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 More
Image
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 More
Image
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 More
Image
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 More
Image
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 More
Image
Published: 01 January 1994
Fig. 5 Surgical prostheses of Ti-6Al-4V alloy of types being commercially ion implanted for wear benefits More
Image
Published: 01 January 1994
Fig. 1 Ti-6Al-4V alpha case. 250× More
Image
Published: 01 January 1994
Fig. 2 Cleaning and belt grinding sequences for Ti-6Al-4V sheet More
Image
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 More
Image
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 More
Image
Published: 01 January 1994
Fig. 11 Hardness profile (Vickers, 0.3 kg load) from plasma-nitrided Ti-6Al-4V. Source: Ref 16 More
Image
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 More
Image
Published: 01 January 1990
Fig. 11 Beta transus approach curves of IMI 834, IMI 829, and Ti-6Al-4V. Source: Ref 9 More
Image
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 More
Image
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 More
Image
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 More