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Book ChapterDOI

Cost Effective Processing of CMC Composites by Melt Infiltration (LSI-Process)

TLDR
In this article, a cost efficient manufacturing route has been developed by DLR based on the infiltration of a reactive fluid phase into porous carbon fiber preforms, where Molten silicon is used as the reactive fluid which replaces the initial pore volume of the preform and reacts subsequently with the carbon matrix to form silicon carbide.
Abstract
High performance ceramics are still largely produced via powder routes. The main disadvantage of these monlithic materials is their brittle failure behaviour and the thus dissatisfactory damage tolerance of ceramic components. The most favourable way to improve the fracture toughness of ceramics is the reinforcement with thermally stable continuous fibres. However, long manufacturing times, multiple reinfiltration steps and expensive raw materials lead to high material costs of these fibre reinforced ceramic matrix composites (CMC) which have prevented their breakthrough to terrestrial applications up until now. To overcome these restrictions and widen the applicability of CMCs - in particular, to enter in fields of mechanical engineering - a novel cost efficient manufacturing route has been developed by DLR. The process is based on the infiltration of a reactive fluid phase into porous carbon fibre preforms. Molten silicon is used as the reactive fluid which replaces the initial pore volume of the preform and reacts subsequently with the carbon matrix to form silicon carbide. A one-shot infiltration is sufficient for the densification of the matrix for this liquid silicon infiltration (LSI) process. Therefore short processing times can be achieved which lead, in addition to the use of commercially available uncoated to carbon fibres and cheap raw materials like phenolics and granules of silicon, to the lowest manufacturing costs of all CMC materials. This paper deals with the fabrication of so-called C/C-SiC composites and with design and cost aspects for the manufacture of C/C-SiC components.

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Citations
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Journal ArticleDOI

C/C–SiC composites for space applications and advanced friction systems

TL;DR: In this article, C/C-SiC composites are considered as the primary materials for hot structures of future launch vehicles and their suitability under extreme thermo-mechanical environments in different structural parts like nose caps, nozzle jet vanes and engine flaps.
Journal ArticleDOI

C/C-SiC Composites for Advanced Friction Systems

TL;DR: Ceramic Matrix Composites (CMC) as discussed by the authors is a type of composite material based on carbon fibres and silicon carbide matrices, which have superior tribological properties in comparison to grey cast iron or carbon/carbon.
Journal ArticleDOI

Carbon Fiber Reinforced CMC for High‐Performance Structures

TL;DR: An overview of the design, manufacture, properties, and applications of C/C-SiC ceramics, produced with the liquid silicon infiltration (LSI) process, is given in this article.
Journal ArticleDOI

C/C–ZrC composite prepared by chemical vapor infiltration combined with alloyed reactive melt infiltration

TL;DR: In this paper, a high performance and low cost C/C-ZrC composite was prepared by chemical vapor infiltration combined with zirconium-silicon (Zr: 91.2 at%; Si: 8.8 at).
Journal ArticleDOI

Measurement of in-plane diffusivity in non-homogeneous slabs by applying flash thermography

TL;DR: In this article, a grid-like mask is placed in front of the flash lamp so that heat is absorbed over a series of periodic parallel strips and the signal-to-noise ratio is increased thereby.
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