fixed semi-a turbomachine (1, 200) of semi-bound or turbine for aircraft or aircraft, driving a receiver (2) driven so as to preserve a speed substantially constant rotation, arranging said turbomachine of a BP compressor (6) , an HP (8) compressor, an annular combustion chamber (10), a HP (12) turbine and a BP (14) turbine, dragging it, particularly via a gear system (20, 120), by said receiver (2) part and on the other hand said LP compressor (6), characterized in that the gear system (20, 120) comprises a distributor pair (26) which maintains a constant relationship between the pair of drag receiver (2) transmitted by the gear system (20, 120) and the torque of the LP compressor (6) transmitted by this same gear system (20, 120).
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