Support member for supporting shell, and method

Details Support member for supporting shell, and method Support member for supporting shell, and method

F - Mech Eng,Light,Heat,Weapons

41

F

F41F 1/06 (2006.01) F42B 30/10 (2006.01)

Patent

CA 2709791

The invention relates to a support member for supporting a shell into the barrel of a breech-loading weapon, and a method. The support member (6) comprises means for fastening a support element (8) to at least one fin (5) belonging to the tail end (4) of a shell (1). The means comprise at least one fastening piece (10), which comprises: at least one first fastening surface (14a), which may be arranged substantially parallel with a side of the fin (5), and which fastening piece (10) may be supported to the support element (8); at least one second fastening surface (14b), which second fastening surface (14b) is movably arranged so that the second fastening surface (14b) is movable in relation to the first fastening surface (14a) in a direction transverse to the longitudinal axis (L) of the shell (1); and means for pressing the fastening surfaces (14a, 14b) against the sides of the fin (5) arranged between them so as to provide friction locking between the fastening piece (10) and the fin (5).

La présente invention concerne un élément de support destiné à supporter un obus dans le canon d'une arme se chargeant par la culasse et un procédé associé. Cet élément de support (6) comprend un moyen de fixation d'une pièce de support (8) à au moins une ailette (5) appartenant à l'extrémité arrière (4) d'un obus (1). Ce moyen comprend au moins une pièce de fixation (10), laquelle comprend : au moins une première surface de fixation (14a), qui peut être agencée sensiblement parallèlement à un côté de l'ailette (5) et, cette pièce de fixation (10) peut être supportée sur la pièce de support (8), au moins une deuxième surface de fixation (14b), cette deuxième surface fixation (14b) étant mobile par rapport à la première surface de fixation (14a) dans un sens transversal à l'axe longitudinal (L) de l'obus (1) et, un moyen permettant de presser les surfaces de fixation (14a, 14b) contre les côtés de l'ailette (5) agencés entre eux de façon à offrir un verrouillage par frottement entre la pièce de fixation (10) et l'ailette (5).

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