Method of and system for destabilization and destruction of dangerous atmospheric phenomena mainly tornado.

Abstract

Method of destabilization and destruction of the dangerous atmospherical phenomena related to a rapidly rotating air masses mainly tornado and apparatus for its realization; this method consists in the delivery of normally liquid fuel-air explosive in the preferably chosen areas of this phenomena by pilotless fuel delivery means; the fuel is released, dispersed and mixed up with rotating air masses and through predeterminated time this aerosol cloud blown up, strong shock wave scatters air masses, destroys a uniform rotating flow of air and thus destroys tornado.

I claim:  
     
         1 . A method of destabilization and destruction of dangerous atmospheric phenomena caused by rapidly rotating aerial masses movement, mainly tornado, including the following steps: 
 an environment monitoring,    a monitoring information analysis and a recognition of new born said phenomenon,    a calculation of its trajectory, shape, characteristics and, at least, horizontal layer height and, at least, one local area (attack area), the most suitable for destabilization and destruction of said phenomenon and located on such height above ground to avoid any influence on ground buildings,    a preparation of necessary quantity of liquid normally non-explosive oxygen-poor fuel-air explosive (FAE),    a preparation of, at least, one fuel delivery means in waiting zone,    filling of, at least, one storage housing of said fuel delivery means with said fuel,    sending of the trajectory data to, at least, one said fuel delivery means,    a delivery of said fuel by, at least, one fuel delivery means to said attack area,    opening said storage housing, dispersing fuel-air explosive for its propagation in an ambient air media of said area and mixing with atmospheric oxygen (aerosol cloud creation),    explosion of said aerosol cloud at reaching of the predetermined fuel concentration in a range of concentration, at which the explosion is possible.    
     
     
         2 . The method according to  claim 1 , wherein said fuel delivery is performed directly to area of air stream concentration, for example, rapidly rotating air masses' area.  
     
     
         3 . The method according to  claim 1 , wherein said fuel delivery is performed in two stages: 
 a preliminary delivery of, at least, one pilotless fuel delivery means filled with said fuel to calculated point in the vicinity of said layer, using, for example, aircraft as pilotless fuel delivery means-carriers,    flying of said pilotless means from calculated point to the chosen attack area.    
     
     
         4 . The method according to  claim 1 , wherein the repeated delivery of said fuel to the chosen attack area of said layer is carried out.  
     
     
         5 . The method according to  claim 1 , wherein the repeated delivery of said fuel to the chosen layer is carried out from the different directions.  
     
     
         6 . The method according to  claim 1 , wherein the delivery of said fuel is performed simultaneously to chosen attack areas of two chosen layers, located at different heights, for example, first area located in rotating air masses, another located in reduced pressure zone.  
     
     
         7 . The method according to  claim 1 , wherein is carried out: 
 at first, delivery of said fuel to a few, at least, two said layers, located at different heights,    at second, additional delivery of said fuel after the second calculated delay time to the space between said layers.    
     
     
         8 . A system for destabilization and destruction of the dangerous atmospheric phenomena caused by rapidly rotating aerial masses movement, mainly tornado, comprising: 
 at least, one environment monitoring station,    a specified quantity of liquid normally non-explosive oxygen-poor fuel-air explosive,    at least, one fuel delivery means, including, at least, one pilotless fuel delivery means, having at least one storage housing filled with said fuel-air explosive,    a station for performing of environment monitoring information analysis, recognition these phenomena, calculation of their trajectory and having communication channels with said monitoring stations and, at least, one said delivery means,    a device to launch the engine of fuel delivery means located on its starting position,    a station for the analysis of the information, detection of the dangerous phenomenon and definition of its trajectory having communication channels with the said analysis stations and, at least, one fuel delivery means,    at least, one detonator for explosion of an aerosol cloud implemented as high brizance charge,    at least, one initiator of explosion of said detonator.    
     
     
         9 . The system according to  claim 8 , comprising also an additional means for preliminary moving pilotless fuel delivery means, for example, aircrafts.  
     
     
         10 . The system according to  claim 8 , wherein said pilotless fuel delivery means consists of, at least, 
 a body,    a rudder system and located in this body: 
 a engine chosen from group, including: 
 jet engine,  
 piston engine with external located propeller,  
 
 a device of movement control,  
   an accumulated housing, and, at least, one placed in this housing a low brizance explosive (first “opening”) charge for opening the said housing and said body and release of the said fuel, and also,    at least, one initiator of said charge explosion.    
     
     
         11 . The system according to  claim 10 , wherein said initiator of opening charge explosion is chosen from group of means including: 
 a timer, whose input at the initial moment is connected to the device to launch engine of said pilotless fuel delivery means engine,    an analyzer of a suitable parameter of external environment, whose sensor is located on the body of said pilotless fuel delivery means,    a sensor of an external control electromagnetic signal, whose source is located outside of tornado.    
     
     
         12 . The system according to  claim 8 , comprising said, at least, one pilotless grenade(rocket), whose starting position is chosen from the group including: 
 pilotless fuel delivery means,    aircrafts,    ground starting position(positions).    
     
     
         13 . The system according to  claim 8 , wherein said detonator and said initiator are located inside said pilotless fuel delivery means, the initiator contains the predetermined detaining element and the initiator's starting input is connected with a unit which is selected from: 
 opening charge(first),    device to launch the engine fuel delivery means.    
     
     
         14 . The system according to  claim 8 , comprising: 
 external fuel concentration sensor, connected with the concentration analyzer; said detonator and initiator which are located inside the body of said pilotless fuel delivery means and the analyzer output is connected with the initiator starting input and said initiator connected with said detonator.    
     
     
         15 . The system according to  claim 8 , comprising, at least, one said initiator of explosion's detonator which is chosen from the group including: 
 an analyzer of a environmental appropriate parameter, whose input is connected to a sensor control located on the body of said pilotless fuel delivery means,    an analyzer of the external control command electromagnetic signal,    a timer located in the body of said pilotless fuel delivery means, whose input is connected with the starting device of the said means' engine at the initial moment.    
     
     
         16 . The system according to  claim 12 , wherein, at least, one detonator for the aerosol cloud explosion is located inside grenade (rocket), the initiator of its explosion is also located inside this grenade together with said detonator and said grenade starting position is located outside of the tornado.  
     
     
         17 . The system according to  claim 10 , wherein said storage housing holds, at least, one container with a thin easily expanding envelope and this container is filled with said fuel.  
     
     
         18 . The system according to  claim 17 , wherein said housing comprises: 
 at least, one container of second type with has a easily expanding envelope, this container is filled with an oxygen-rich easily decomposed compound and contains an initiator of decomposition of the said compound connected with said first opening charge.    
     
     
         19 . The system according to  claim 17  or  18 , wherein said containers are chosen from group including: 
 balloons with metallized envelopes,  
 metallic boxes with walls which are made in form of bellows.  
 
     
     
         20 . The system according to  claim 18 , wherein envelopes(walls), at least, one from container types has: 
 a common site of both envelopes, dividing two internal cavity, inside one of which there is a said fuel, and inside another is oxygen-rich compound,    the second opening charge and the second connected to this charge detaining element, located on the said common site, and    the third (own) opening charge located on external safe envelope one of the said containers and the third detaining element connected with this charge, and 
 starting inputs of second and third detaining elements are connected with first opening charge,  
 a delay time of the second detaining element is less than a delay time of third detaining element, and  
 a delay time of the third detaining element is less than a delay time of the first detaining element.