TRANSITION DUCT SYSTEM WITH NON-METALLIC THERMALLY-INSULATING LINERS SUPPORTED WITH SPLITTABLE METALLIC SHELL STRUCTURES FOR DELIVERING HOT-TEMPERATURE GASSES IN A COMBUSTION TURBINE ENGINE

A transition duct system (10) for delivering hot-temperature gases from a plurality of combustors in a combustion turbine engine is provided. The system includes an exit piece (16) for each combustor. A non-metallic thermally-insulating liner (22), as may be made from a ceramic-based material, such...

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Bibliographische Detailangaben

Hauptverfasser:	MORRISON, Jay A, WALL, Andrew, PORTILLO BILBAO, Juan Enrique, SHIPPER, Jonathan E, SMITH, Kyle
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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