| 摘要 |
<p>The turbomachine has a gear system (20) comprising a power divider (26) maintaining a constant ratio between input torques of a variable pitch propeller (2) and a low pressure compressor (6), where the torques are transmitted by the system. The power divider has a planet carrier centered on longitudinal principal axis (3) of the turbomachine and integrated to an input (E) of the gear system.</p> |
