The present work is focused on the fabrication of long fibre reinforced titanium composites by hot pressing of plasma-sprayed preforms. Thermal spraying of two different metallic matrices [Ti-6Al-2Sn-4Zr-2Mo-0.08Si (Ti6242S) and Ti-4.5Al-3V-2Mo-2Fe (SP700)] onto prearranged silicon carbide long fibres was performed using controlled-atmosphere plasma spraying equipment (CAPS), allowing deposition processes also in the high-pressure range. After optimization of the plasma spraying procedure, composite multilayers were fabricated by hot pressing at 1200 bar with different combinations of process parameters (temperature in the range 850-940 °C, and application time from 30 to 45 min). Consolidated samples were characterized by microstructural investigation and tensile testing at room and high temperature (up to 600 °C). Push-out and push-back tests were performed to investigate interfacial properties.

Titanium matrix reinforced composites produced by hot pressing of plasma-sprayed preforms / Valente, Teodoro; S., Picchiotti; Bartuli, Cecilia; C., Testani. - In: PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS. PART L, JOURNAL OF MATERIALS, DESIGN AND APPLICATIONS.. - ISSN 1464-4207. - STAMPA. - 217:4(2003), pp. 257-268. [10.1243/146442003322814132]

Titanium matrix reinforced composites produced by hot pressing of plasma-sprayed preforms

VALENTE, Teodoro;BARTULI, Cecilia;
2003

Abstract

The present work is focused on the fabrication of long fibre reinforced titanium composites by hot pressing of plasma-sprayed preforms. Thermal spraying of two different metallic matrices [Ti-6Al-2Sn-4Zr-2Mo-0.08Si (Ti6242S) and Ti-4.5Al-3V-2Mo-2Fe (SP700)] onto prearranged silicon carbide long fibres was performed using controlled-atmosphere plasma spraying equipment (CAPS), allowing deposition processes also in the high-pressure range. After optimization of the plasma spraying procedure, composite multilayers were fabricated by hot pressing at 1200 bar with different combinations of process parameters (temperature in the range 850-940 °C, and application time from 30 to 45 min). Consolidated samples were characterized by microstructural investigation and tensile testing at room and high temperature (up to 600 °C). Push-out and push-back tests were performed to investigate interfacial properties.
2003
controlled-atmosphere plasma spraying; plasma spraying; push-out; titanium alloys; hot pressing; push-back; high-pressure plasma spraying; controlled-atmosphere; silicon carbide; mmc; push out; tensile tests; composites; titanium alloy
01 Pubblicazione su rivista::01a Articolo in rivista
Titanium matrix reinforced composites produced by hot pressing of plasma-sprayed preforms / Valente, Teodoro; S., Picchiotti; Bartuli, Cecilia; C., Testani. - In: PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS. PART L, JOURNAL OF MATERIALS, DESIGN AND APPLICATIONS.. - ISSN 1464-4207. - STAMPA. - 217:4(2003), pp. 257-268. [10.1243/146442003322814132]
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/255364
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