Development of Filament Reinforced Titanium Alloys

670862

02/01/1967

Event
Aeronautic and Space Engineering and Manufacturing Meeting
Authors Abstract
Content
Titanium and its alloys can be used successfully as matrix material for continuous filaments, such as boron or silicon carbide. The single limiting factor in fabrication and life of the composites is the interaction between filament and matrix. Several attempts have been made to manufacture filament-reinforced titanium alloys; however, methods such as powder metallurgy, creep controlled diffusion bonding, and plasma arc spraying have been unsuccessful because interaction has led to reaction layers in excess of 1 micron in thickness. Compound thicknesses of such magnitudes render composites useless because cracks form in the compound at low strains and cause subsequent failure of the filaments. Recent developments in manufacturing techniques have made it possible to control formation of boride or sili-cide so that prolonged life is obtained. This paper describes properties of such composites.
Meta TagsDetails
DOI
https://doi.org/10.4271/670862
Pages
10
Citation
Metcalfe, A., and Schmitz, G., "Development of Filament Reinforced Titanium Alloys," SAE Technical Paper 670862, 1967, https://doi.org/10.4271/670862.
Additional Details
Publisher
Published
Feb 1, 1967
Product Code
670862
Content Type
Technical Paper
Language
English