Hydrodynamic closed loop turboset-selfbooster

Abstract

The Hydrodynamic closed loop turboset-selfbooster comprises one or more axial bispindle multistage hydrolic turbines ( 20 A, 20 B) placed into a common closed-loop tubular tunnel ( 26 B) with an axial-flow propeller pump ( 27 ) which works in self-series, as a self-booster impelling high potential operating liquid, filled inside the tunnel. The natural accumulative turbotechnology provides high energy ratio and thus profound general efficiency. The proposal leads to: (a) wide range of universal power units including perfect hydraulic turbines and effective motors for vehicles and other means instead of ineffective heat engines, (b) prospective gradual elimination of fuels for many kinds of power units, (c) ecological purity without any harm emissions and pollutions, (d) multiple high efficient design versions of different power levels, various performances and diverse purposes.

1 . A Hydrodynamic closed loop turboset-selfbooster comprising at least one of axial concentric bispindle multistage hydraulic turbines placed inside a closed loop tubular tunnel with an axial-flow propeller pump impelling operative liquid filled inside said tunnel to drive said turbines.  
   
   
       2 . The turboset of  claim 1  wherein said turbines include primary wing-blade rotating stages connected with inner turbospindle and guiding wing-blade generally rotating stages connected with outer tubular turbo-spindle, which is concentric to said inner turbo-spindle.  
   
   
       3 . The turboset of  claim 2  wherein said primary wing blades and said guiding wing-blades can be one-piece and/or multi element, and/or combined in stages, and/or spindles, and/or turbines.  
   
   
       4 . The turboset of  claim 2  wherein any of said primary and guiding wing-blade stages may include various and different numbers of wing-blades and the average adjacent blade stage step-spacing along said spindles can be different depending on turbine design.  
   
   
       5 . The turboset of  claim 2  wherein any of said guiding stages is placed between said primary stages along their said spindles and mutual orientation of primary and guiding stages provide the opposite rotations of said inner and outer spindles.  
   
   
       6 . The turboset of  claim 1  wherein said closed loop tubular tunnel is filled with a preferably high density operative liquid under definite controlled static pressure.  
   
   
       7 . The turboset of  claim 6  wherein said closed loop tunnel and its elements include flow straighteners for high potential flow turbulence limitation and flow equalization.  
   
   
       8 . The turboset of  claim 6  wherein said closed loop tunnel include a static pressure control valve device having a springed regulated piston.  
   
   
       9 . The turboset of  claim 1  wherein said closed loop tubular tunnel may include at least one controlled hydrolic bypass.  
   
   
       10 . A hydrodynamic closed loop accumulative turbotechnology includes working as self-booster in series with itself, in pressure-accumulating manner, an axial-flow propeller pump which drives a kit of axial concentric bispindle multistage turbines by high potential flow, all in common closed loop tubular tunnel filled with operative liquid.  
   
   
       11 . The turbotechnology of  claim 10  wherein any of said turbines has two concentric spindles rotating in opposite directions.  
   
   
       12 . The turbotechnology of  claim 10  wherein the possible cavitation of said high potential flow in said tunnel is limited, adjusted, and controlled by valve device and/or partly bypassing said flow, and/or combining.  
   
   
       13 . The turbotechnology of  claim 10  wherein said closed loop tubular tunnel comprises an air-cooler placed near cooling fins.  
   
   
       14 . The turbotechnology of  claim 10  wherein the power of said turbines and/or spindles can be directed preferably to electric generators, alternators and/or other various power receivers.  
   
   
       15 . The turbotechnology of  claim 14  wherein said electric generators can drive the motors of axial pump air-cooler of the tunnel said in claim using regular electric battery and charger set.  
   
   
       16 . The turbotechnology of  claim 10  wherein said in  claim 1  sets can work in series, in parallel, and/or combining in equal and/or different power levels