turbojet a double flow comprising an ancillaries distribution support and the ancillaries distribution support.

摘要

The present invention relates to a bypass turbojet engine, comprising a casing (11), the intermediate supported by arms (12), a sleeve (34) to the right of the casing (11) and equipment (38). In the axis of an arm (12), is provided, on the shell (34), an ancillaries distribution support (35) comprising, on the outer side of the ring (34), a first sole plate for the reception of ancillaries (36) .grâce to the invention, the longitudinal size which is connected to the ancillaries is reduced.