COMPOSITES AND METHODS OF FORMING COMPOSITES HAVING TAILORED HARDNESS PROFILE
An aerospace component (100) may comprise a fiber reinforced composite material (102). The fiber reinforced composite material (102) includes a plurality of fiber layers and a carbon matrix (106) surrounding the plurality of fiber layers. A plurality of ceramic particles (108) is dispersed in the ca...
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
30.08.2023
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Subjects | |
Online Access | Get full text |
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Summary: | An aerospace component (100) may comprise a fiber reinforced composite material (102). The fiber reinforced composite material (102) includes a plurality of fiber layers and a carbon matrix (106) surrounding the plurality of fiber layers. A plurality of ceramic particles (108) is dispersed in the carbon matrix (106). A first fiber layer of the plurality of fiber layers may include a carbon fiber (104a), and a second fiber layer of the plurality of fiber layers may include a non-carbon fiber (104b). A hardness of the non-carbon fiber (104b) is greater than a hardness of carbon fiber (104a). |
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Bibliography: | Application Number: EP20220209482 |