TRANSITION DUCT FORMED OF A PLURALITY OF SEGMENTS

A gas turbine engine having a transition duct made of a plurality of segments. Each of the segments is connected to an adjacent segment. The plurality of segments may be made of ceramic material or super alloys.

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Bibliographische Detailangaben
1. Verfasser:	Schiavo, Anthony L
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS 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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Beschreibung
Zusammenfassung:	A gas turbine engine having a transition duct made of a plurality of segments. Each of the segments is connected to an adjacent segment. The plurality of segments may be made of ceramic material or super alloys.