Horizontal Axis Logarithmic Spiral Fluid Turbine

Abstract

The present invention is a more simplified and efficient design of a turbine. The use of a logarithmic curve pattern for blade design and an aerodynamic profile allows the present invention to not only be versatile in its uses, but also much more efficient at gathering forms of energy for different purposes.

1 . A horizontal axis logarithmic spiral fluid turbine comprises,
 a plurality of blades;   a rotary axle;   a plurality of cylindrical extensions;   a generator;   a hall;   each blade comprises of a blade surface, a center, a leading edge, a trailing edge;   each blade spiraling around the rotary axle; and   the center of each blade being attached to the rotary axle.   
     
     
         2 . The horizontal axis logarithmic spiral fluid turbine as claimed in  claim 1  comprises
 the first cylindrical extension being mounted in front of the plurality of blades; 
 the first cylindrical extension being protruded from the rotary axle; 
 the second cylindrical extension being protruded opposite of the first cylindrical extension on the rotary axle; 
 the hall traversing through the second cylindrical extension; and 
 the hall being connected to the generator. 
 
     
     
         3 . The horizontal axis logarithmic spiral fluid turbine as claimed in  claim 1  comprises,
 the leading edge being narrower than the trailing edge and therefore creating an aerodynamic profile; 
 the trailing edge being perpendicular to the rotary axle; 
 the blade surface being perpendicular to the rotary axle; and 
 the blade surface having a spiral shape with a logarithmic profile. 
 
     
     
         4 . A horizontal axis logarithmic spiral fluid turbine comprises,
 a plurality of blades;   a rotary axle;   a cylindrical extension;   a hall;   a generator;   a support bar;   a deck;   a horizontal pivot component;   the support bar being attached to the deck;   the deck being attached to the generator;   the horizontal pivot component being attached to the deck;   each blade comprises of a blade surface, a center, a leading edge, a trailing edge;   each blade spiraling around the rotary axle; and   the center of each blade being attached to the rotary axle.   
     
     
         5 . The horizontal axis logarithmic spiral fluid turbine as claimed in  claim 4  comprises,
 the cylindrical extension being mounted in front of the plurality of blades; 
 the cylindrical extension being protruded from the rotary axle; 
 the cylindrical extension being attached to the generator; 
 the hall traversing through the cylindrical extension; and 
 the hall being connected to the generator. 
 
     
     
         6 . The horizontal axis logarithmic spiral fluid turbine as claimed in  claim 4  comprises,
 the leading edge being narrower than the trailing edge and therefore creating an aerodynamic profile; 
 the trailing edge being perpendicular to the rotary axle; 
 the blade surface being perpendicular to the rotary axle; and 
 the blade surface having a spiral shape with a logarithmic profile. 
 
     
     
         7 . A horizontal axis logarithmic spiral fluid turbine comprises,
 a plurality of blades;   a rotary axle;   a cylindrical extension;   a hall;   a generator;   a plurality of cables;   each blade comprises of a blade surface, a center, a leading edge, a trailing edge;   each blade spiraling around the rotary axle; and   the center of each blade being attached to the rotary axle.   
     
     
         8 . The horizontal axis logarithmic spiral fluid turbine as claimed in  claim 7  comprises,
 the cylindrical extension being mounted in front of the plurality of blades; 
 the cylindrical extension being protruded from the rotary axle; 
 the hall traversing through the cylindrical extension; 
 the plurality of cables traversing through the hall; and 
 the plurality of cables attaching to the generator. 
 
     
     
         9 . The horizontal axis logarithmic spiral fluid turbine as claimed in  claim 7  comprises,
 the leading edge being narrower than the trailing edge and therefore creating an aerodynamic profile; 
 the trailing edge being perpendicular to the rotary axle; 
 the blade surface being perpendicular to the rotary axle; and 
 the blade surface having a spiral shape with a logarithmic profile.