HYBRID CMC COMPONENT HAVING INTEGRAL AND MODULAR SHROUDS

A hybrid CMC component (25) for a gas turbine engine (100) is located in the turbine section (50) of the gas turbine engine (100). The hybrid CMC component takes advantage of features found within modular structures and within integral structures. The hybrid CMC component (25) is able to reduce leak...

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Bibliographische Detailangaben
Hauptverfasser:	MARSH, Jan H, JAMES, Allister William
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Zusammenfassung:	A hybrid CMC component (25) for a gas turbine engine (100) is located in the turbine section (50) of the gas turbine engine (100). The hybrid CMC component takes advantage of features found within modular structures and within integral structures. The hybrid CMC component (25) is able to reduce leakage paths while also accommodating thermal expansion. L'invention concerne un composant CMC hybride (25) pour un moteur à turbine à gaz (100) et qui est situé dans la section de turbine (50) dudit moteur à turbine à gaz (100). Le composant CMC hybride tire parti des caractéristiques trouvées dans des structures modulaires et dans des structures intégrales. Le composant CMC hybride (25) est capable de réduire les trajets de fuite tout en recevant également une expansion thermique.