Compressor rotor blade

A compressor rotor blade ( 1 ) includes a rotor blade ( 2 ), a platform ( 3 ) that adjoins the rotor blade ( 2 ) and blade footing ( 4 ) that adjoins the platform ( 3 ). The rotor blade ( 4 ) is embodied so as to be massive, without an internal cooling system, and exhibits a leading and a trailing e...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	BACHOFNER RENE, KAPPIS WOLFGANG
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL 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 NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A compressor rotor blade ( 1 ) includes a rotor blade ( 2 ), a platform ( 3 ) that adjoins the rotor blade ( 2 ) and blade footing ( 4 ) that adjoins the platform ( 3 ). The rotor blade ( 4 ) is embodied so as to be massive, without an internal cooling system, and exhibits a leading and a trailing edge ( 5, 6 ), a suction and a compression side, as well as a blade tip ( 7 ). The compressor rotor blade ( 1 ) is distinguished by virtue of the fact that the rotor blade ( 2 ) of the compressor rotor blade ( 1 ) exhibits a recess ( 8 ) on the trailing edge ( 6 ) of the blade tip ( 7 ).