Methods and systems for protection from destructive dynamic vortex atmospheric structures

• US 9,708,828 B2
• Filed: 05/05/2011
• Issued: 07/18/2017
• Est. Priority Date: 05/06/2010
• Status: Active Grant

• Current Assignee: Alexey Varaksin, Arkady Rozenshteyn, Mikhail Romash, V Kopeitsev
• Original Assignee: Alexey Varaksin, Arkady Rozenshteyn, Mikhail Romash, V Kopeitsev
• Inventors: Varaksin, Alexey, Rozenshteyn, Arkady, Romash, Mikhail, Kopeitsev, V.
• Primary Examiner(s): FERENCE, JAMES M
• Application Number:
  US13/101,388
• Publication Number:
  US 20110272032A1
• Time in Patent Office: 2,266 Days
• Field of Search: 52 84, 521731, 52 29, 239 21
• CPC Class Codes: E04H 9/14 against other dangerous influences, e.g. tornadoes, floods
• CPC Class Codes: Y02A 50/00 in human health protection, e.g. against extreme weather
• CPC Class Codes: Y10T 137/0318 Processes

Abstract

Various methods and systems for protecting humans as well as individual objects from tornadoes and other naturally occurring dynamic atmospheric vortex structures are described. Active protective systems interact with such vortex structures leading to destabilization and destruction of the vortex structures. The energy required for the destabilization and destruction of the vortex structure is taken from the energy from the vortex structure itself. The method requires no external energy sources for destabilization and destruction of vortex structures such as tornadoes.

Claims

1. A method for destabilizing a dynamic atmospheric vortex structure, the method comprising:

providing a cluster of spatially oriented discrete mechanical elements at a location relative to the vortex structure to thereby produce an area of local active anisotropy, which creates a non-stationary, turbulent field with significant anisotropy that destabilizes the vortex structure, wherein the vortex structure is a tornado.

2. The method of claim 1 wherein the non-stationary turbulent field includes anisotropy of at least one of density, pressure, secondary flow velocity and turbulence parameters.

3. The method of claim 1 wherein the cluster comprises a plurality of elementary turbulent transformers.

4. The method of claim 3 wherein at least a majority of the elementary turbulent transformers are cylindrical in shape.

5. The method of claim 1 wherein the cluster is configured to exhibit a G parameter value in a range of about 0.0001 to about 10 m.

6. The method of claim 5 wherein the cluster is configured to exhibit a G parameter value in a range of about 0.001 to about 1 m.

7. The method of claim 6 wherein the cluster is configured to exhibit a G value of about 1 m.

8. The method of claim 1 wherein the height of the cluster of spatially oriented discrete mechanical elements is greater than about 4% of the height of the vortex structure.

9. The method of claim 8 wherein the height of the cluster is greater than about 6% of the height of the vortex structure.

10. The method of claim 9 wherein the height of the cluster is greater than about 10% of the height of the vortex structure.

11. The method of claim 1 wherein the cluster is in a honeycomb configuration including a plurality of hexagonal shaped modules.

12. The method of claim 1 wherein the cluster is in a saw configuration including a plurality of triangular shaped modules.

13. The method of claim 1 wherein the cluster is in a plane grid configuration including a plurality of rectangular modules.