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

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Bibliographische Detailangaben
1. Verfasser:	BAHADOR, MEHDI
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBINED OPERATIONS ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINE TOOLS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES OTHER WORKING OF METAL PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS
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Beschreibung
Zusammenfassung:	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 manufactured from a second material. The external part is manufactured in a final shape (21) of the external part. Subsequently, the external part in the final shape is fixedly connected to the base part such that at least a part (14) of a surface (12) of the base part is covered by the external part. The first material has a first thermal conductivity and the second material has a second thermal conductivity. The first thermal conductivity is greater than the second thermal conductivity.