Turbine with radial inlet and outlet rotor for use in bidirectional flows

The present invention relates to a turbine which can absorb energy from bi-directional reversing flows, as is the case of ocean wave energy converters. In the periphery of the bladed rotor (2) of the turbine there are two openings (5, 6) through which the fluid alternately enters, or exits from, the...

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Bibliographische Detailangaben
Hauptverfasser:	DE CARVALHO GATO LUIS MANUEL, FRANCO DE OLIVEIRA FALCÃO ANTÓNIO
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING 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 MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PRODUCING MECHANICAL POWER REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGYGENERATION, TRANSMISSION OR DISTRIBUTION 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
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Beschreibung
Zusammenfassung:	The present invention relates to a turbine which can absorb energy from bi-directional reversing flows, as is the case of ocean wave energy converters. In the periphery of the bladed rotor (2) of the turbine there are two openings (5, 6) through which the fluid alternately enters, or exits from, the rotor, the outward flow being radially centrifugal and the inward flow being radially centripetal. The turbine stator comprises two sets of guide vanes (7, 8) for alternately directing the bi-directional reversing flow to, and from, the rotor, and two ducts (9, 12) disposed between the rotor and the guide vanes and extending radially beyond the guide vanes. Two stator arrangements are considered. In both arrangements, the inlet guide vanes deflect the inward flow and impart a circumferential swirl component in the same direction as the normal rotational direction of the rotor. In one of the arrangements, the twin guide vane set (18, 19) is close to the rotor periphery (5, 6) and can be moved axially so that it guides the inward flow into the rotor and does not intersect the outward flow. In the other arrangement, both sets of guide vanes (7, 8) are axially fixed and are radially offset from the rotor.