Rotor and nozzle assembly for a radial turbine and method of...

F - Mech Eng,Light,Heat,Weapons – 01 – D

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F01D 1/02 (2006.01) F01D 15/10 (2006.01)

Patent

CA 2645646

A rotor for a radial flow turbine has an impulse chamber (51) having an inlet defined in a circumferential surface of the rotor and a reaction chamber (62) having an outlet defined in the circumferential surface of the rotor. The impulse chamber is in fluid communication with the reaction chamber, and the reaction chamber outlet is axially displaced from the impulse chamber inlet.

L'invention concerne un rotor destiné à une turbine centrifuge, comprenant une chambre d'impulsion (51) pourvue d'une ouverture d'entrée définie dans la surface circonférentielle du rotor, et une chambre de réaction (62) pourvue d'une ouverture de sortie définie dans la surface circonférentielle du rotor. La chambre d'impulsion est en communication de fluide avec la chambre de réaction, et l'orifice de sortie de la chambre de réaction est déplacé axialement par rapport à l'orifice d'entrée de la chambre d'impulsion.

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