1-20 of 666 Search Results for

titanium composites

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 2015
Fig. 6.37 The potential advantage of using continuous reinforced titanium composites is demonstrated for engine blades. Data courtesy of Allison More
Image
Published: 01 November 2010
Fig. 20.25 Physical vapor deposition coated silicon carbide/titanium composite. Source: Ref 8 More
Image
Published: 01 October 2012
Fig. 9.28 Jet engine applications of titanium-matrix composites. (a) A nozzle actuator piston rod used on the Pratt & Whitney F119 engine for F-22 aircraft. The part is made of a Ti-6Al-2Sn-4Zr-2Mo alloy reinforced with SiC monofilaments that are 129 μm (5.1 mils) in diameter. The inset More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2012
DOI: 10.31399/asm.tb.lmub.t53550457
EISBN: 978-1-62708-307-2
... and stiffness, among other properties, in preferred directions and locations. This chapter discusses the processes and procedures used in the production of fiber-reinforced aluminum and titanium metal-matrix composites. It explains how the length and orientation of reinforcing fibers affect the properties...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870537
EISBN: 978-1-62708-314-0
... and slurry casting, liquid metal infiltration, spray deposition, powder metallurgy, extrusion, hot rolling, and forging. The chapter also provides information on continuous-fiber aluminum and titanium composites as well as particle-reinforced titanium and fiber metal (glass aluminum) laminates...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.bcp.t52230163
EISBN: 978-1-62708-298-3
... Abstract This chapter discusses the composition, properties, and uses of the most common beryllium alloys and composites. It provides information on beryllium-aluminum, beryllium-copper, and beryllium-titanium as well as beryllium-antimony and beryllium-iron systems. alloying elements...
Image
Published: 01 June 2016
Fig. 2.13 SEM micrograph of a titanium-molybdenum composite cold sprayed with nitrogen at a process gas pressure of 4.2 MPa (610 psi) and a process gas temperature of 930 °C (1700 °F). The volume content of 50% Mo in the powder blend was reduced to 41% in the final coating at an overall More
Image
Published: 01 November 2010
Fig. 20.6 Silicon carbide monofilament/titanium matrix composite More
Image
Published: 01 November 2010
Fig. 20.21 Silicon carbide monofilament/titanium matrix composite More
Image
Published: 01 November 2010
Fig. 20.28 Secondary diffusion bonding of titanium matrix composite (TMC) spars. HIP, hot isostatic pressing More
Image
Published: 01 November 2010
Fig. 20.30 Abrasive waterjet cutting of titanium matrix composite. Source: The Boeing Company More
Image
Published: 01 November 2010
Fig. 20.32 Diamond core drilling of a titanium matrix composite component. Source: The Boeing Company More
Image
Published: 01 November 2010
Fig. 20.33 Spot welding titanium matrix composite hat stiffeners. Source: The Boeing Company More
Image
Published: 01 January 2015
Fig. 3.24 Compositional relationship of several terminal titanium alloys by increasing or decreasing the percentage of alpha and beta phases of an alloy More
Image
Published: 01 January 2015
Fig. 3.25 The titanium-aluminum phase diagram showing the temperature-composition in which Ti 3 Al and TiAl are stable More
Image
Published: 01 January 2015
Fig. 6.32 Titanium-aluminum phase diagram showing the temperature-composition in which TiAl, Ti 3 Al, and TiAl 3 are stable. More
Image
Published: 01 January 2015
Fig. 8.37 Titanium metal-matrix composite golf club head (reinforced with TiB). Courtesy of Toyota Central R&D Labs, Inc. More
Image
Published: 01 November 2010
Fig. 15.11 Area sectioned 1.5 mm (0.06 in.) from the titanium fastener/composite interface showing the effects of interply arcing in the composite. (a) Bright-field illumination, 25× objective. (b) Epi-fluorescence, 390– 440 nm excitation, 25× objective More
Image
Published: 01 November 2010
Fig. 4.6 Montage showing a polished titanium fastener/polymer composite assembly. Bright-field illumination, 65 mm macrophotograph More
Image
Published: 01 November 2010
Fig. 4.7 A carbon fiber composite with a titanium fastener is clamped in a fixture and aligned for sectioning. In this figure, the alignment is performed using a straight edge. This sample will be sectioned through the fastener, with the straight edge providing alignment of the edge of the saw More