FIELD: machine building.
SUBSTANCE: invention relates to the machine building. Reduction gear with two intermediate transmission lines, in particular, for gas turbine engine, comprises inlet line (12) and output line rotated by inlet line through said intermediate lines, wherein intermediate lines are parallel. Reduction gear also comprises means of distributing loads between said intermediate lines, wherein said load distribution means comprises rotary means (30) damping to engage rotation of inlet line end and oil means (40, 50) to radially displace radially opposite ends of said inlet line.
EFFECT: higher reliability of the reduction gear, improved design and reduced weight.
10 cl, 7 dwg
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