Projectile with snares for incapacitating flying drones
The modified projectile design with additional compartments and sequential deployment of capes enhances the probability of hitting drones by increasing the number of threaded payloads, addressing the lethality limitations of existing designs.
WO2026135496A1PCT designated stage Publication Date: 2026-06-25KUZNETSOV ANDREY LEONIDOVICH
Patent Information
- Authority / Receiving Office
- WO · WO
- Patent Type
- Applications
- Current Assignee / Owner
- KUZNETSOV ANDREY LEONIDOVICH
- Filing Date
- 2025-12-15
- Publication Date
- 2026-06-25
AI Technical Summary
Technical Problem
Existing projectiles with capes for destroying flying drones have limited lethality due to a restricted number of threaded weights, leading to a low probability of hitting the target.
Method used
The design is modified to include additional compartments between jaws on the cartridge stem, allowing the cap to open sequentially upon detonation, increasing the number of threaded payloads and enhancing the probability of hitting a drone by deploying multiple capes.
Benefits of technology
The modified design significantly increases the probability of hitting aerial drones by deploying multiple capes, improving shooting efficiency and target engagement.
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Smart Images
Figure RU2025050425_25062026_PF_FP_ABST
Abstract
The invention relates to weaponry, and more particularly to ammunition with a snare for incapacitating aerial drones. A projectile with snares for incapacitating flying drones comprises a base part having an imaginary longitudinal axis, a cassette, and a cap which is open at the back, the cassette and the cap being disposed on the imaginary longitudinal axis. An air burst means for a propelling charge is also provided. The propelling charge is disposed inside the cap between the front part of the cap and the front part of the cassette. The cassette comprises first and second fins which are perpendicular to the imaginary longitudinal axis and are connected to a shaft. The configuration of the fins is disclosed. A first snare comprises a first ring, weights of the first snare, and lines of the first snare. The positioning of the first snare and the first ring and the design of the weights and lines are also disclosed. The base part is connected to the cassette or is a part of the cassette. A third fin is positioned in front of and parallel to the second fin and is connected to the shaft. A second snare is additionally provided, said second snare being disposed between the second and third fins and comprising a second ring, weights, and lines. The positioning of the weights of the second snare and the fastening of the weights to the second snare by lines are disclosed. The technical result consists in increasing the likelihood of incapacitating a flying drone.
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