Power take-off system and gas turbine assembly including same

摘要

A power take-off system (100,400,500) for a gas turbine engine assembly (10) is provided. The gas turbine engine includes a first spool (40) and a second spool (42), the power take-off system including a starter (102) coupled to the second spool, and a clutch assembly (200) coupled between the starter and the first spool, the clutch assembly configured to couple the first spool to the starter when starting the gas turbine engine assembly.