US2006255482A1PendingUtilityA1

Device for stirring a liquid and for injecting a gas into this liquid, suitable for shallow basins

Assignee: CHEVALIER GILBERTPriority: Apr 19, 2005Filed: Apr 19, 2006Published: Nov 16, 2006
Est. expiryApr 19, 2025(expired)· nominal 20-yr term from priority
B01F 27/80B01F 23/2331C02F 3/16Y02W10/10
50
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Claims

Abstract

The invention relates to a device for stirring a liquid in a reactor and for injecting a gas into the said liquid in order to form a gas-liquid dispersion, comprising a) a drive device ( 1 ) positioned above the reactor, provided with a vertical output shaft ( 2 ) fitted at its lower end with at least one axial flow rotor ( 4 ) immersed in the liquid, b) means for introducing gas ( 3 and 7 ) above the axial flow rotor ( 4 ), c) a deflector ( 5 ) placed above the axial flow rotor ( 4 ) preventing the gas-liquid dispersion from rising, and d) a deflector ( 6 ) placed below the axial flow rotor ( 4 ) converting the axial flow of the said axial flow rotor into a radial flow. This device may be used in shallow basins.

Claims

exact text as granted — not AI-modified
1 . A device for stirring a liquid in a reactor and for injecting a gas into the said liquid in order to form a gas-liquid dispersion, comprising: 
 a) a drive device positioned above the reactor, provided with a vertical output shaft fitted at its lower end with at least one axial flow rotor immersed in the liquid;    b) means for introducing gas above the axial flow rotor; and    c) a deflector placed above the axial flow rotor preventing the gas-liquid dispersion from rising,    wherein said device comprises a deflector placed below the axial flow rotor converting the axial flow of the said rotor into a radial flow.    
   
   
       2 . The device of  claim 1 , characterized in that the deflector placed below the axial flow rotor is a plate.  
   
   
       3 . The device of  claim 2 , characterized in that the plate is centered on the output shaft.  
   
   
       4 . The device of  claim 2 , characterized in that a deflector cone is centered on the plate.  
   
   
       5 . The device of  claim 2 , characterized in that a deflector prism is centered on the plate.  
   
   
       6 . The device of  claim 1 , characterized in that the surface area of the deflector placed below the axial flow rotor is extended to the area projected onto it by the stirring device.  
   
   
       7 . The device of  claim 1 , characterized in that the deflector placed below the axial flow rotor is fixed to the output shaft of the drive device.  
   
   
       8 . The device of  claim 1 , characterized in that the deflector ( 6 ) placed below the axial flow rotor consists of: 
 a) a central plate; and    b) surface portions distributed angularly around the central circular plate and having a progressive profile diverging outwards and towards the bottom of the reactor.    
   
   
       9 . The device of  claim 8 , characterized in that the divergent progressive profile of the surface portions is able to bring about a Coanda effect on any flow surging tangentially in the section described by the divergent progressive profile.  
   
   
       10 . The device of  claim 8 , characterized in that the central plate is fixed to the output shaft of the drive device.  
   
   
       11 . The device of  claim 8 , characterized in that a deflector cone is centered on the central plate.  
   
   
       12 . The device of  claim 1 , characterized in that: 
 a) the means for introducing gas above the axial flow rotor consists of: 
 i) a self-aspirating turbine immersed in the reactor, placed above the axial flow rotor and which can be driven by the output shaft; and  
 ii) a cylinder coaxially enveloping the output shaft, the lower end of which emerges in the turbine and the upper end of which is connected in a sealed manner to the drive device and is drilled with an opening for injecting a gas into an annular gap delimited by the shaft and the cylinder; and  
   b) the turbine consisting of two superimposed discs and an assembly of radial blades arranged between the discs and attached thereto, the upper disc being drilled with a central hole into which the lower end of the cylinder enters which delimits, with the edge of the said hole, a space that is at least partially annular, through which liquid is drawn into the turbine.

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