HIGH-TEMPERATURE RESISTANT TILES AND MANUFACTURING METHOD THEREOF

A tile (1), in particular a high-temperature resistant tile for lining internal surfaces of gas turbines, having a body (2) made of a CMC material consisting of ceramic fibers embedded in a ceramic matrix; the body (2) comprising a hollow CMC structure (6) between a lower solid CMC layer (7) and an...

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Bibliographische Detailangaben
Hauptverfasser: Stefanis, Vasileios, Pievaroli, Marco, Paul, Anish
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A tile (1), in particular a high-temperature resistant tile for lining internal surfaces of gas turbines, having a body (2) made of a CMC material consisting of ceramic fibers embedded in a ceramic matrix; the body (2) comprising a hollow CMC structure (6) between a lower solid CMC layer (7) and an upper solid CMC layer (8); wherein the lower solid CMC layer (7) and the upper solid CMC layer (8) are solid homogeneous layers, having no cavities or void spaces inside the CMC material; and the hollow CMC structure (6) comprises a cell pattern (9), extending between opposite faces (12, 13), facing each other and substantially parallel to each other, of the layers (7, 8), and consisting of a plurality of cells (10) defined by respective cavities and delimited by lateral walls (14) and arranged side-by-side on at least one cell layer (11).