Wind powered energy amplification system and method

Abstract

The present invention is comprised of a wind powered energy amplification method and systems for capturing wind power and harvesting tangentially amplified energy. The harvested tangentially amplified energy is converted, processed and stored for use for generating continuous, on demand and stand by electricity to supply electricity. The present invention is further comprised of methods and systems for extracting, processing and storing water and carbon dioxide to supply water and supply carbon dioxide.

1 . A wind powered energy amplification system to harvest, convert and store energy and extract, process and store water and carbon dioxide from air, comprising:
 cantilevered support structure modules coupled to wind powered energy amplification modules;   bearing attachment modules coupled to the cantilevered support structure modules and to a mounting apparatus, wherein the bearing attachment modules are configured to allow rotation of the cantilevered support structure modules;   energy harvest and conversion modules coupled to the cantilevered support structure modules and configured to harvest and convert tangentially amplified kinetic energy;   forced rotation modules configured to control the speed of rotation and orientation of the cantilevered support structure modules from the converted tangentially amplified kinetic energy; and   extraction modules configured to extract and process water and carbon dioxide from the air.   
     
     
         2 . The wind powered energy amplification system of  claim 1 , further comprising wind capture modules coupled to the cantilevered support structure modules and configured to create rotation using captured wind power. 
     
     
         3 . The wind powered energy amplification system of  claim 1 , further comprising tube frame support structure modules configured to support the cantilevered support structure modules. 
     
     
         4 . The wind powered energy amplification system of  claim 3 , further comprising drive shaft systems modules coupled to the tube frame support structure modules and configured to transfer wind power rotation to modules that are not attached to the tube frame support structure modules. 
     
     
         5 . The wind powered energy amplification system of  claim 4  further comprising forced rotation modules coupled to the drive shaft systems and configured to allow transfer of a mechanically forced rotation. 
     
     
         6 . The wind powered energy amplification system of  claim 1 , further comprising:
 a bearing platform configured to allow rotation of the cantilevered support structure modules and coupled to the mounting apparatus, bearings and the cantilevered support structure modules;   a tube frame mounting bracket coupled to a mounting block and the tube frame support structure modules; and   a mounting block lock configured coupled to the tube frame mounting bracket and the mounting block and configured to prevent separation and lateral displacement.   
     
     
         7 . The wind powered energy amplification system of  claim 6 , further comprising a convection cooled bearing system configured to create a low friction bearing with fluid lubricant cooling convection flow channels. 
     
     
         8 . The wind powered energy amplification system of  claim 7 , further comprising;
 a convex sliding rotating section configured to slide a convex surface on a fluid lubricant and to mate with an asymmetrical concave surface to form a convection flow channel;   an asymmetrical concave convection ring channel configured to mate with the convex sliding rotating section to form the convection flow channel, to connect to a mounting base and fluid cooling reservoir to form cooling channels;   a non uniform convection flow channel formed by the permanent separation of the mated opposing surfaces of the convex sliding rotating section and the asymmetrical concave convection ring channel and configured to create circulation of the fluid lubricant by convection; and   a stationary section mounting base and fluid cooling reservoir coupled to an object, the asymmetrical concave convection ring channel and configured to allow rotation, to form cooling channels, to act as a heat sink and to accumulate fluid lubricant in a fluid reservoir for supplying the convection flow channel.   
     
     
         9 . The wind powered energy amplification system of  claim 2 , further comprising;
 drive panel systems modules configured to form wind capture modules to capture the power of the wind;   drive panel furling systems modules coupled to the drive panel systems and configured to rotate drive panels in various degrees of rotation; and   an automated furling control system coupled to the drive panel furling systems modules and configured to control degrees of rotation of the drive panel systems modules.   
     
     
         10 . The wind powered energy amplification system of  claim 1 , further comprising monitor and control modules configured to measure, control, record and transmit operating conditions and levels of the modules. 
     
     
         11 . The wind powered energy amplification system of  claim 1 , further comprising extraction storage modules for storing and supplying extracted water and carbon dioxide. 
     
     
         12 . The wind powered energy amplification system of  claim 1 , further comprising;
 flutter vane amplification energy harvest modules configured to harvest and convert the energy of the air encountered at tangentially amplified speeds;   propeller amplification energy harvest modules configured to harvest and convert the energy of the air encountered at tangentially amplified speeds.   
     
     
         13 . The wind powered energy amplification system of  claim 6 , further comprising:
 a flutter vane including a blade configured to rotate, wherein the flutter vane is coupled to the cantilevered support structure modules for harvesting energy of the air flow moving at speeds amplified by tangential speed;   a curved elongated panel including a Venturi wing coupled to a flutter vane axle hub and configured to allow rotation of blade;   a Venturi wing configured to form a Venturi constriction with an outer edge of the blade and configured to accelerate a speed of moving air by the Venturi effect to add force to the rotation of the flutter vane amplification energy harvest modules;   wherein the flutter vane axle hub is coupled to energy converting modules and the cantilevered support structure modules to position the flutter vane amplification energy harvest modules at a radial distance from the axis of rotation of the cantilevered support structure modules and configured to allow the flutter vane amplification energy harvest modules to rotate at tangential speeds; and   energy converting modules coupled to the flutter vane axle hub and configured to convert the energy harvested by the flutter vane transferred by connection to the flutter vane axle hub.   
     
     
         14 . The wind powered energy amplification system of  claim 6 , further comprising:
 a propeller coupled to a propeller shaft and rotation transfer modules and configured to allow the propeller to rotate for harvesting the energy of the air flow moving at speeds amplified by tangential speed and Venturi effect by rotating;   a propeller shaft and rotation transfer modules coupled to a nacelle to allow the propeller shaft and rotation transfer modules to connect to energy converting modules;   a nacelle coupled to an air scoop Venturi to provide a stable structure to hold the propeller in position;   an air scoop Venturi coupled to a housing to accelerate the speed of air encountered at tangentially amplified speeds;   a housing coupled to cantilevered support structure modules to position the propeller amplification energy harvest modules at a radial distance from the axis of rotation of the cantilevered support structure modules to allow the propeller amplification energy harvest modules to rotate at tangential speeds; and   energy converting modules coupled to the housing for converting the energy harvested by the propeller transferred by connection to the propeller shaft and rotation transfer modules.   
     
     
         15 . The extraction modules of  claim 1 , further comprising circular receiver assembly modules configured to form transitional connection devices to allow the collection systems used to convey the converted energy and extracted water to transition from a rotating state to a stationary state to convey the converted energy and extracted water to the converted energy process and storage modules. 
     
     
         16 . A method for treating a hollow interior of a part comprising:
 pumping an acrylic based liquid into the hollow interior of the part;   forming the acrylic based bubbles by injecting a compressed gas into the acrylic based liquid;   projecting the ultra violet light into the hollow interior of the part;   exposing the acrylic based bubbles to the ultra violet light for a predetermined period of curing time; and   creating a light weight rigid three dimensional interlocking structure from the cured acrylic based bubbles filling within the hollow interior of the part.   
     
     
         17 . The method of  claim 16 , further comprising controlling sizes of the acrylic based bubbles and wall thickness of the acrylic based bubbles by adjusting the viscosity and volume of the acrylic based liquid used to form the bubbles, controlling the formation of the acrylic based bubbles by adjusting the pressure level and volume of compressed gas used for injecting the acrylic based liquid with the compressed gas to cause the bubble formation and controlling the curing time by adjusting the wavelength and intensity of the ultra violet light exposing the acrylic based bubbles. 
     
     
         18 . The method of  claim 16 , further comprising inserting a tool inside the hollow interior for injecting the acrylic based liquid and compressed gas into the part. 
     
     
         19 . The method of  claim 16 , further comprising using an extruder to inject the acrylic based liquid and compressed gas into the part. 
     
     
         20 . A honeycomb chamber storage system of component section modules to allow adaptable sizing and installations of compressed gas storage below ground, comprising:
 a honeycomb chamber storage tank assembly of interconnecting storage chamber section component modules configured to an extended hexagonal form to form a system of stable stackable interconnecting storage chambers;   a chamber section configured to include one or more interconnect fittings to allow the interconnection of stacked units to form a free flow compressed gas storage containment;   a chamber extension configured to allow the lengthening of the honeycomb chamber storage tank assembly to increase storage volume capacity;   a chamber end cap female configured to seal one end of the honeycomb chamber storage tank assembly;   a chamber end cap male configured to seal one end of the honeycomb chamber storage tank assembly;   a chamber spacer configured to support the angled recessed sections of the bottom layer of the stacked honeycomb chamber storage tank assemblies;   a storage system inlet configured to be attached to the chamber interconnect fittings to allow compressed gas to enter the honeycomb chamber storage system; and   a storage system outlet configured to be attached to the chamber interconnect fittings to allow compressed gas to be released from the honeycomb chamber storage system.