Turbomachine component

The turbomachine component has an auxiliary portion (16) that is formed on a base component (10) and comprised of an inner cavity enclosed by outer walls (11,12). The base component and auxiliary portion are connected by the connecting surfaces (15,17) in a connecting region (18). An intermediate pi...

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Bibliographische Detailangaben
Hauptverfasser:	Mahler, Alexander, Hähnle, Hartmut
Format:	Patent
Sprache:	eng ; fre ; ger
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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Beschreibung
Zusammenfassung:	The turbomachine component has an auxiliary portion (16) that is formed on a base component (10) and comprised of an inner cavity enclosed by outer walls (11,12). The base component and auxiliary portion are connected by the connecting surfaces (15,17) in a connecting region (18). An intermediate piece (14) is provided in the base component and/or auxiliary portion, and extended from the outer walls into the inner cavity. A straight line transition contour is arranged in transition region of intermediate piece and outer walls.