The present invention relates to at least one body (2) on the aircraft, at least one wing (3) that is located on the body (2), extends outwards from the body (2) and allows carrying the ammunition (M), at least one feeding unit (4) that is located inside the body (2) and allows the storage of ammunition (M), multiple launchers (5) that are located on the wing (3) and allow the ammunition (M) to be launched or released from the body (2), and multiple tubes (6) that create an opening on the launchers (5) and allow the ammunition (M) to be placed inside.

    La présente invention concerne au moins un corps (2) sur l'aéronef, au moins une aile (3) située sur le corps (2), s'étendant vers l'extérieur à partir du corps (2) et permettant de porter la munition (M), au moins une unité d'alimentation (4) située à l'intérieur du corps (2) et permettant le stockage de munitions (M), de multiples lanceurs (5) situés sur l'aile (3) et permettant le lancement ou la libération de la munition (M) à partir du corps (2), et plusieurs tubes (6) créant une ouverture sur les lanceurs (5) et permettant le placement de la munition (M) à l'intérieur.


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    Title :

    AMMUNITION TRANSFER SYSTEM


    Additional title:

    SYSTÈME DE TRANSFERT DE MUNITIONS


    Contributors:

    Publication date :

    2025-04-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F41F APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS , Vorrichtungen zum Abschießen von Geschossen oder Flugkörpern aus Rohren, z.B. Geschütze / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F41A Funktionsmerkmale oder Einzelheiten, die Handfeuerwaffen und Artillerie gemeinsam betreffen, z.B. Rohre , FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS



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