The invention relates to a device (1) for pneumatic launching of a drone (2), comprising a launch tube (3), a pressurization chamber (6) situated at the rear of the tube (3) and provided with a passage opening (63) leading into the tube (3), and means (7) for temporarily closing the passage opening (63). According to the invention, the temporary closing means (7) are arranged to change from a closed configuration to an open configuration instantaneously under the action of the gas pressure inside the chamber (6), after the latter has reached a trigger pressure, and the cross section of the passage opening (63) is sufficiently large that, instantaneously with the change to the open configuration, the gas pressure prevailing in the chamber (6) and the space located behind the drone (2), then in communication with each other, is the desired launching pressure for the drone (2).
DISPOSITIF DE LANCEMENT PNEUMATIQUE D'UN DRONE
DEVICE FOR PNEUMATIC LAUNCHING OF A DRONE
VORRICHTUNG ZUM PNEUMATISCHEN STARTEN EINER DROHNE
2025-01-08
Patent
Electronic Resource
French
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge / B64U / F41B WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE , Waffen zum Verschießen von Geschossen ohne Verwendung von Explosiv- oder Treibladungen / F41F APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS , Vorrichtungen zum Abschießen von Geschossen oder Flugkörpern aus Rohren, z.B. Geschütze |
DISPOSITIF DE LANCEMENT D'UN PROJECTILE ET PROCÉDÉ DE LANCEMENT D'UN PROJECTILE
European Patent Office | 2024
|European Patent Office | 2024
|European Patent Office | 2025
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