Improved Performance in Aerospace Structures with Ti and Ni Metal Matrix Composites

Author:

Testani Claudio1,Tului Mario1

Affiliation:

1. Centro Sviluppo Materiali, SpA. (CSM)

Abstract

The external structures of supersonic vehicles are exposed in several critical regions to temperatures that could reach 1000°C. This limit is higher than any safe operative service not only for titanium alloys but also for commercial nickel superalloys. The simplest way to improve titanium and nickel matrices temperature behavior (i.e: strength and fatigue resistance) is to introduce a strengthening phase in its matrix. These class of materials are known as: Metal Matrix Composites (MMC). It is possible reinforce both titanium and nickel superalloys by mean of high temperature resistant ceramic fibers.

Publisher

Trans Tech Publications, Ltd.

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference21 articles.

1. H.E. Debolt: Boron and Other High Strength, Low Density Filamentary Reinforcing Agents, Handbook of Composites, ed. G. Lubin, Van Nostrand Reinhold, 1982, pp.69-76.

2. S. Nourbakhsh and H. Margolin, in: Proc. of Metal & Ceramic Matrix Composites: Processing, Modeling and Mechanical Behavior (1990).

3. M.A. Mittnick: Metal and Ceramic Matrix Composites 605 (1990), in proceedings.

4. S.C. Jha, J.A. Forster, A.K. Pandey and R.G. Delagi, Cold Rolled Titanium Aluminide and Titanium Alloy Foils ISIJ International Vol. 31 10 (1991), p.1267.

5. Structural Materials Handbook, Vol. 2: new advanced materials(section XI), ed. European Space Agency, (1994).

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