Abstract: A package (100) comprising storage packaging (1) as well as a confinement canister (3) for irradiated fuel, the packaging comprising a lateral body (2) which extends around a longitudinal axis (12) of the packaging and which includes an internal surface (22) which delimits a cavity for housing the canister (3), the packaging furthermore comprising at least one assembly (15) forming a guide rail for the canister in the cavity, mounted on the lateral body (2) and protruding at least partly into the housing cavity (4). According to the invention, the assembly forming a guide rail (15) includes an impact shock absorbing element (28) designed to absorb the shock, by plastic deformation, of a lateral impact between the packaging (1) and the confinement canister (3).

Abstract: A package (100) comprising storage packaging (1) as well as a confinement canister (3) for irradiated fuel, the packaging comprising a lateral body (2) which extends around a longitudinal axis (12) of the packaging and which includes an internal surface (22) which delimits a cavity for housing the canister (3), the packaging furthermore comprising at least one assembly (15) forming a guide rail for the canister in the cavity, mounted on the lateral body (2) and protruding at least partly into the housing cavity (4). According to the invention, the assembly forming a guide rail (15) includes an impact shock absorbing element (28) designed to absorb the shock, by plastic deformation, of a lateral impact between the packaging (1) and the confinement canister (3).

Abstract: The invention relates to a method of brazing a Ti—Al alloy. According to the invention, a layer of nickel (2) is disposed between a part (1) which is made from titanium aluminide and a brazing sheet (3), such as to enable: the aforementioned part (1) to be brazed to another metallic material (4) without the aluminium diffusing from one to the other; and a stable link with good mechanical strength to be produced. The invention can be used for the assembly of aircraft engine parts which are made from titanium aluminide and nickel-based superalloy.

Abstract: The invention relates to a method of brazing a Ti—Al alloy. According to the invention, a layer of nickel (2) is disposed between a part (1) which is made from titanium aluminide and a brazing sheet (3), such as to enable: the aforementioned part (1) to be brazed to another metallic material (4) without the aluminium diffusing from one to the other; and a stable link with good mechanical strength to be produced. The invention can be used for the assembly of aircraft engine parts which are made from titanium aluminide and nickel-based superalloy.