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6 Concluding Remarks

  • Bilge Saruhan
Chapter

Abstract

Oxide CMCs are attractive materials because they are inherently resistant to oxidation. Efforts to develop the oxide CMCs were intensified in the last decade, relying onto these and similar high temperature properties. Previous to oxide CMCs, the non-oxide CMCs were successfully developed, mainly bearing in mind the structural applications. Recently, demanding requirements for the conditions in air were set bringing the need for better materials withstanding even higher temperatures and longer exposure times (i.e. ≥ 1200°C and >10.000 hours) than those initially given. In general, space applications entail higher temperatures (i.e. 1500°C) than those anticipated for gas turbine engines, however, hereby much shorter exposure times are required (< 5 hours) making it bearable for non-oxide CMCs. Thus, the non-oxide CMCs having relatively high ultimate fracture strengths (e.g. 300–600 MPa) found an appropriate use in space applications.

Keywords

Fiber Coating Damage Tolerance Crack Deflection Oxide Fiber Liquid Phase Deposition 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer Science+Business Media New York 2003

Authors and Affiliations

  • Bilge Saruhan
    • 1
  1. 1.German Aerospace Center Institute for Materials ResearchCologneGermany

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