Turbojet engine must generally with a one-piece arm to the connection of the auxiliary components

摘要

The invention relates to a turbojet engine comprising an outer casing (2), connected by radial arms (3), to an annular internal device (37), downstream of which is mounted, at right angles to the outer casing (2), a ferrule (4) forming a fairing, the ancillaries on the outside of the outer casing and of the ancillaries inside the virole.elle is characterized by the fact that the turbojet engine comprises at least a monoblock arm (28) of the ancillary connection between the outside of the outer casing (2) and the inside of the ferrule (4), disposed parallel to a radial arm (3) [invention applies to the turbofan engines.