Transition Duct Exit Holder and Inlet Ring Support Arrangement

A gas turbine engine has a transition duct supporter that is able to support and accommodate the operation of the gas turbine engine. The transition duct supporter is located between a metallic integrated exit piece and a transition duct that is made of ceramic matrix composites.

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Bibliographische Detailangaben
1. Verfasser:	Schiavo Anthony L
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A gas turbine engine has a transition duct supporter that is able to support and accommodate the operation of the gas turbine engine. The transition duct supporter is located between a metallic integrated exit piece and a transition duct that is made of ceramic matrix composites.