Structure of radial turbine scroll and blades

Adaptations for a radial turbine scroll and the radial turbine blades. The scroll structure for the radial turbine is characterized by having a scroll width ratio ranging from ”R/B = 0.3 to 0.7. Further the turbine blades have cut-away areas at the blade corners on the inlet edge.

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Bibliographische Detailangaben
Hauptverfasser:	UTSUMI, RYOJI, OSAKO, KATSUYUKI, EBISU, MOTOKI, MIKOGAMI, TAKASHI, MAEKAWA, SHOZO
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL ENGINE PLANTS IN GENERAL HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS 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 INTERNAL-COMBUSTION PISTON ENGINES 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:	Adaptations for a radial turbine scroll and the radial turbine blades. The scroll structure for the radial turbine is characterized by having a scroll width ratio ranging from ”R/B = 0.3 to 0.7. Further the turbine blades have cut-away areas at the blade corners on the inlet edge.