A TURBOMACHINE COMPONENT FOR HOT GAS PATH OF A GAS TURBINE

The present invention provides a turbomachine component (1) suitable to be positioned in a hot gas path (5) of a gas turbine engine (6). The turbomachine component includes a base part (10) and an external part (20). The base part is manufactured from a first material and the external part is manufa...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	BAHADOR, MEHDI
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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