Vorrichtung zum Kühlen des Rotors einer Gasturbine

This device embodies a centrifugal compressor secured to a joint-carrier disk secured to an upstream flange of the rotor disk to be cooled. The recompressed air is ejected through channels near the roots of the blades of the disk.

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Bibliographische Detailangaben
Hauptverfasser:	CARUEL, JACQUES EMILE JULES, MAINCY, FR, BARBOT, ANDRE MAURICE, CESSON, FR, SOLIGNY, MARCEL ROBERT, CHEVILLY LA RUE, FR
Format:	Patent
Sprache:	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:	This device embodies a centrifugal compressor secured to a joint-carrier disk secured to an upstream flange of the rotor disk to be cooled. The recompressed air is ejected through channels near the roots of the blades of the disk.