Turbojet engine

摘要

The invention refers to a propulsion system, the tripleflux turbojet, which can be used in the aeronautical industry for aircraft propulsion.
The tripleflux turbojet having a secondary interior fan (2), a stator (1), a primary stator (3), a compressor (4), a intermediary casing (20), a exterior casing (21), a secondary interior working channel (8) and a primary working channel (9), a combustion chamber (5), a turbine (6) with three rotors 6A, 6B, 6C, independent, shafts (15 and 16) mounted in the interior casing (22) of the primary flux and the nozzle (7) having a shaft (14) mounted in the interior casing (22) which spins a fan (13) behind which is mounted a stator (12) and a secondary stator (10) which is mounted in the interior of the channel of the exterior secondary flux (11) delimitated by the body of the exterior casing (18) and the body of the intermediary casing (20).