FIELD: machine building.
SUBSTANCE: invention relates to reduction gear. Gas-turbine engine includes at least one reduction gear with two peripheral tram-transmission lines. Reduction gear comprises input, output and intermediate lines, means of distributing loads between intermediate lines. Output line is the driven input line through the intermediate lines. Intermediate lines are substantially parallel. Load distribution means comprise rotary means for connection in rotation of the first end of the input line, first means of damping radial displacements of the first end of the input line and second means of damping radial displacements of the opposite, second end of the input line.
EFFECT: possibility of uniform distribution of loads and elimination of axial displacement.
11 cl, 6 dwg
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