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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
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Published: 01 November 2010
Fig. 20.25 Physical vapor deposition coated silicon carbide/titanium composite. Source: Ref 8 More
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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...
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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
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Published: 01 October 2012
Fig. 9.24 Foil-fiber-foil method for titanium-matrix composite fabrication. HIP, hot isostatic pressing; P, pressure; T, temperature. Source: Ref 9.8 More
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Published: 01 October 2012
Fig. 9.26 Silicon carbide monofilament/titanium-matrix composite. Source: Ref 9.16 More
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Published: 01 October 2012
Fig. 9.27 Green tape method for titanium-matrix composite fabrication. Source: Ref 9.8 More
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Published: 01 October 2012
Fig. 9.29 Secondary diffusion bonding of titanium-matrix composite (TMC) spars. HIP, hot isostatic pressing. Source: Ref 9.16 More
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Published: 01 November 2010
Fig. 4.6 Montage showing a polished titanium fastener/polymer composite assembly. Bright-field illumination, 65 mm macrophotograph More
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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
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Published: 01 November 2010
Fig. 4.8 Photographs showing the section of the titanium fastener/composite assembly prepared for mounting. (a) The cut titanium fastener/composite assembly is facing down, with a piece of glass fabric to be placed on the bottom of the mold to ensure impregnation of the face. (b) Mold More
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Published: 01 November 2010
Fig. 4.9 Photograph of the titanium fastener/composite lap joint specimen mounted in Rhodamine-B-dyed epoxy resin. The mount is numbered on the sides for documentation. More
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Published: 01 November 2010
Fig. 4.11 Titanium fastener/polymer composite assembly etched with oxalic acid for 15 s. A gap of 59 μm can be seen between the composite and the etched titanium. Slightly uncrossed polarized light, 10× objective More
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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
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Published: 01 June 2008
Fig. 33.12 Silicon carbide monofilament/titanium-matrix composite More
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Published: 01 June 2008
Fig. 33.15 Green tape method for titanium-matrix composite fabrication. Source: Ref 2 More
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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