Method for fighting aircrafts with airscrew propulsion, the element for execution of fighting aircrafts with airscrew propulsion and the transport cassette of this element

摘要

method of control of propeller driven aircraft, characterised by the fact that after locating and identifying of propeller driven aircraft, on his route of transport containers distributes elements to develop mode, depending on the particular idle position, speed and course in the area of ballistic parameters measurein which is positioned a elements to develop mode, algorithms of timing angles and times launch measure tape with components, precision distribution tapes and develop transport containers with the elements, and then at least one element is a frequency rzeliwany by the system operator to the aircraft with a propeller driven,then during free fall element is inside the vacuum that creates in the front or top of the work u015bmigu0142owego propulsion aircraft, after which element together with air is taken in the direction of propeller and due to resistance aerodynamicznyc h the individual components is wygiu0119ciu and is drawn into the propeller.usually, a central part (2), which causes a dynamic a tweak sections completed ballast (3) and the umbrella (1),a rotational propeller causes change of position wciu0105gniu0119tej central part a (2) in relation to the umbrella (1) and a ballast (3) and is effective in element in shovel arranged on both sides of the propeller and a leash (2) element is unevenly okru0119cona wo wheels, propellers, and ballast (3) element with a leash (2) remains outside the rotor and outside the propeller.by introducing dynamic unbalanced load of the propeller.