PROJECTILE WITH CAPES FOR COUNTERACTING AERIAL DRONES Russian patent published in 2025 - IPC F42B12/56 F42B12/58 F42B12/66 F41H11/02 

FIELD: weapons.

SUBSTANCE: invention relates to weapons, namely to means of mechanical destruction of small-size objects by means of capes. Projectile with capes for hitting aerial drones comprises a bottom part having an imaginary longitudinal axis. Besides, it includes a cassette and a cap open at the back, which are located on an imaginary longitudinal axis. There is shaft connected with cap or being part of cap. Barrel is closed in front, barrel muzzle is directed backward. Cassette has forward-directed piston located in barrel. There is means of air blasting of burster charge and burster charge arranged in barrel. Device also includes first cape. Cassette comprises first and second cheeks perpendicular to imaginary longitudinal axis and connected to rod, wherein outer diameter of rod is smaller than outer diameters of cheeks. First jaw is located behind second jaw. First cape comprises a first ring, weights of the first cape and threads of the first cape. First cape is located between the first and second cheeks. Weights of the first cape are located around imaginary longitudinal axis. Each weight of the first cape is equipped with a thread of the first cape. Each thread of the first cape is attached to the corresponding weight of the first cape by the first end. First ring is located outside the rod. Second end of each thread of the first cape is attached to the first ring. Each thread of the first cape is compactly laid so that it can be straightened when it is pulled by the second end. Bottom part of the known projectile is additionally connected to the cartridge or is a part of the cartridge. In front of the second cheek there is a third jaw which is parallel to the second jaw and connected to the rod. Additionally introduced is the second cape located between the second and the third cheeks containing the second ring, weights of the second cape and threads of the second cape. Weights of the second cape are located around imaginary longitudinal axis. Each weight of the second cape is provided with a thread of the second cape. Each thread of the second cape is attached to the corresponding weight of the second cape with the first end. Second ring is located outside the rod. Second end of each thread of the second cape is attached to the second ring. Each thread of the second cape is compactly laid with the possibility of straightening when it is pulled by the second end. Weights of capes are located inside cap.

EFFECT: higher probability of drone hitting.

10 cl, 18 dwg