Mix-in structure for gas or the like in pressurization...

F - Mech Eng,Light,Heat,Weapons – 04 – D

Patent

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Details

F04D 29/44 (2006.01) F04D 5/00 (2006.01) F04D 15/00 (2006.01) F04D 29/66 (2006.01) F04D 31/00 (2006.01)

Patent

CA 2493419

A mix-in structure for a gas or the like in a pressurization centrifugal pump, capable of mix-discharging liquid and gas or the like to prevent cavitation and of suppressing gas residence in the pump chamber at the time of operation stoppage or the like. It comprises a drum-like case (4) having a suction port (2) and a delivery port (3), in which opposedly disposed are a vane wheel (5) radially formed with a plurality of vanes (19), a pressurization surface (36) formed with a compression chamber (33) opposed to the vane wheel (5) and converging from the suction port (2) toward the vanes (19), and pressurization section (16) formed with a pressurization partition wall (35) disposed close to the side surfaces of the vanes (19) to prevent leakage of the fluid in the vane chamber (27), wherein a gas supply device (6) is installed for supplying a gas into the suction port (2) by an increase in the liquid pressure in the delivery port (3) by using a pressurization centrifugal pump for pressurizing the liquid taken in from the suction port (2) in a pump chamber (9) defined by the vane wheel (5) and the pressurization section (16) and delivering it through the delivery port (3).

L'invention concerne une structure de mélange de gaz, ou analogue, dans une pompe centrifuge de surpression, pouvant refouler un mélange de liquide et de gaz, ou analogue, afin d'empêcher un phénomène de cavitation, et de supprimer la présence de gaz dans le corps de pompe au moment de l'arrêt de la pompe, ou analogue. Cette structure comprend un carter de type tambour (4) équipé d'un orifice d'aspiration (2) et d'un orifice de refoulement (3), dans lequel sont disposés en opposition une turbine radiale à ailettes (5), dotée de plusieurs ailettes (19), une surface de surpression (36) formée par une enceinte de compression (33), opposée à la turbine à ailettes (5), et convergeant de l'orifice d'aspiration vers les ailettes (19), et une section de surpression (16) formée par une paroi de séparation de surpression (35) disposée à proximité des surfaces latérales des ailettes (19) afin d'empêcher une fuite de liquide dans la chambre des ailettes (27). Un dispositif d'alimentation en gaz (6) est installé dans cette structure afin d'introduire un gaz par l'orifice d'aspiration (2) par augmentation de la pression du liquide dans l'orifice de refoulement (3) au moyen d'une pompe centrifuge de surpression pressurisant le liquide entrant par l'orifice d'aspiration (2) dans le corps de pompe (9), défini par la roue à ailettes (5) et la section de surpression (16), et le refoulant par l'orifice de refoulement (3).

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