Rotor of an axial compressor stage of a turbo machine

The rotor has a rotating body with a rotational, where the rotating body is formed at the periphery of a blade ring (1) having a radially lying rim surface (10). Multiple blades are arranged on the blade ring. The rim surface has a radius based on a rotational axis of the rotating body, where the ra...

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Bibliographische Detailangaben
Hauptverfasser:	HEINICHEN, FRANK, JOHANN, ERIK
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION ENGINE PLANTS IN GENERAL GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Beschreibung
Zusammenfassung:	The rotor has a rotating body with a rotational, where the rotating body is formed at the periphery of a blade ring (1) having a radially lying rim surface (10). Multiple blades are arranged on the blade ring. The rim surface has a radius based on a rotational axis of the rotating body, where the radius changes between two adjacent blades (2) in a portion in the axial direction (x) and in the circumferential direction.