FIELD: aviation.
SUBSTANCE: invention relates to a turbomachine with a gearbox of an aircraft. The aviation turbomachine with the gearbox contains first shaft (15) and second shaft (3) with one axis of rotation, wherein the second shaft is rotated by the first shaft via gearbox (7), the first shaft contains an elastically deformable means of a bellows type, and it is connected to the gearbox by a communication system also containing elastically deformable means (17) of a clamp or bellows type. The present invention also relates to a method for installation of such a turbomachine.
EFFECT: invention allows for limiting the size of a system by means of an optimized communication system between two shafts or shaft sections.
17 cl, 14 dwg
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