Turbine with radial inlet and outlet rotor for use in bi-directional flows

A turbine arrangement for bi-directional reversing flow includes a rotor with blades 2 and a stator with guide vanes (7, 8). The rotor rotates on axis 1 and the blades 2 form flow channels from axially spaced rotor entry/exits 5, 6. The entrance of fluid into the rotor through either of the aperture...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	DE CARVALHO GATO LUIS MANUEL, FRANCO DE OLIVEIRA FALCAO ANTONIO
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING 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 RELATING TO MACHINES OR ENGINES OTHER THANNON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, TO WIND MOTORS,TO NON-POSITIVE DISPLACEMENT PUMPS, AND TO GENERATING COMBUSTIONPRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES FOR LIQUIDS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PRODUCING MECHANICAL POWER REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGYGENERATION, TRANSMISSION OR DISTRIBUTION 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 WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A turbine arrangement for bi-directional reversing flow includes a rotor with blades 2 and a stator with guide vanes (7, 8). The rotor rotates on axis 1 and the blades 2 form flow channels from axially spaced rotor entry/exits 5, 6. The entrance of fluid into the rotor through either of the apertures 5, 6 is centripetal (radially in toward the rotor axis) and the exit of the fluid from the rotor through either of the two apertures 5, 6 is centrifugal. A first set of guide vanes 7 are circumferentially disposed about the axis (1) and located at a greater radius with respect to the corresponding rotor aperture 5 in the path of the flow incoming to the rotor or out of it. A duct 9 connects the first set of guide vanes 7 with the corresponding rotor aperture 5. A second set of guide vanes 8 are circumferentially disposed about the axis 1 and located at a greater radius with respect to the corresponding rotor aperture 6 in the path of the flow incoming to the rotor or out of it. A duct 12 connects the second set of guide vanes 8 with the corresponding rotor aperture 6. The ducts are formed by walls of revolution 10, 11, 13, 14.